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1

Gudín de la Lama, Enrique. "Emilio Herrera Linares, artífice de la ingeniería aeronáutica española." Llull Revista de la Sociedad Española de Historia de las Ciencias y de las Técnicas 46, no. 92 (November 25, 2023): 39–67. http://dx.doi.org/10.47101/llull.2023.46.92.gudin.

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The beginnings of Spanish aeronautics are linked to the biography of Emilio Herrera, a leading figure among the pioneers of aviation in Spain. Despite the research that has been done on him, his role in the genesis of aeronautical engineering as an area of knowledge with its own identity remained to be explored. Herrera’s work in this field took place at the same time as the birth and growth of this speciality and was oriented —as the subsequent evolution of the decisions he had taken showed— in the right direction. His management work in the Aerodynamic Laboratory, in the commission for the homologation of aeronautical engineering degrees, in the creation of the School of Engineers and in the Association of Aeronautical Engineers were key to the birth and consolidation of Spanish aeronautical engineering. This article highlights the initiatives and decisions taken, and to what extent they contributed to institutionalizing Spanish aeronautical engineering.
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Ackroyd, J. A. D. "The Victoria University of Manchester’s contributions to the development of aeronautics." Aeronautical Journal 111, no. 1122 (August 2007): 473–93. http://dx.doi.org/10.1017/s0001924000004735.

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This issue of the Aeronautical Journal celebrates the 50th anniversary of the foundation of the Honours Degree Course in Aeronautical Engineering at the Victoria University of Manchester. The following article therefore describes the aeronautical research and teaching activities of that university up to its recent amalgamation with the University of Manchester Institute of Science and Technology (UMIST) to form the present-day University of Manchester. This juncture provides a further justification for recording the Victoria University’s achievements.Both the Victoria University and UMIST had their roots in the nineteenth century although, apart from the relatively brief period of the First World War, neither of them was particularly involved in aeronautics until after the Second World War. However, as Sections 6.0-10.0 seek to demonstrate, thereafter the Victoria University’s involvement became considerable. The preceding Sections describe the origins of the Victoria University and UMIST and, in the case of the former institution, the subsequent activities of its staff and graduates in engineering and mathematics which, although not always specifically aeronautical in content, nonetheless had a profound influence on the development of the aeronautical sciences.
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3

Ackroyd, J. A. D., L. Bernstein, and F. W. Armstrong. "One hundred years of aeronautics in East London." Aeronautical Journal 112, no. 1133 (July 2008): 357–80. http://dx.doi.org/10.1017/s0001924000002335.

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This paper celebrates the centenary of Queen Mary College’s involvement in aeronautics, a celebration with a unique distinction since it was this College’s immediate forebear which was the first British higher education institution to begin teaching and research in this subject. Thus the emphasis is on the early years from 1907 until the 1950s, a period ripe for recording before it recedes beyond living memory, but also the period during which the degree course in aeronautical engineering became firmly established and its parent Department acquired its reputation for research. Section 2.0 gives a brief history of the College’s origins in the East London College. Subsequent sections deal with the foundation of the aeronautical laboratory there, from which the aeronautical department grew, and the activities of the two men who led these developments, A.P. Thurston and N.A.V. Tonnstein who changed his name to Piercy.
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Allen, J. E. "Aeronautics-1903; aerospace-2003; ? ? 2103." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 219, no. 3 (March 1, 2005): 235–60. http://dx.doi.org/10.1243/095441005x30252.

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The centenary of the first manned flight was a unique occasion permitting a rare opportunity to range far into both the past and the future. Most of aeronautics must inevitably be focussed on the near future and immediate actions. However, there are some very long-term underlying issues which are invisible from a day-to-day perspective, but which should not be overlooked as they can be used very often to guide decisions that might otherwise be unsound. In Part 1, the paper reviews the major breakthroughs that have impelled aeronautics along a startling trajectory of success, with some mention of the uncertain beginnings, when even Wilbur Wright considered that all his aerodynamic theories were in a muddle. In that spirit, in Part 2, some attempts are made to anticipate possible breakthroughs that might happen in the 21st century. However, aeronautics does not stand alone. Considerations, such as other transport modes, energy substitution, non-vehicular transport, and the consequences of major global political alignments, will be reviewed in order to seek new aeronautical challenges of the future. Some other long-term, but non-aeronautical engineering, initiatives relevant to the IMechE are introduced and discussed in the appendix
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5

Lemco, Ian. "Wittgenstein's aeronautical investigation." Notes and Records of the Royal Society 61, no. 1 (December 22, 2006): 39–51. http://dx.doi.org/10.1098/rsnr.2006.0163.

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After a rigorous German education in the physical sciences, young Ludwig Wittgenstein entered Manchester University as an aeronautical engineering research student. There he devised and patented a novel aero-engine employing an airscrew propeller driven by blade tip-jets. Within the context of the growth of English aviation during the first half of the twentieth century (including the contributions of many Fellows of the Royal Society) and taking into account related aspects of his life, this paper examines an unfulfilled engineering aspiration. In enlarging upon what Wittgenstein might have accomplished during his stay at Manchester, it contrasts his invention with later comparable proven designs, albeit applied to hybrid rotorcraft. His engine employed centrifugal flow compression and arguably was a precursor of Sir Frank Whittle's gas turbine. In conclusion, reasons are given for Wittgenstein's departure from Manchester.
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Bearman, Peter. "Special Issue of The Aeronautical Journal, marking the 150th Anniversary of the Founding of the Royal Aeronautical Society." Aeronautical Journal 120, no. 1223 (January 2016): 1–2. http://dx.doi.org/10.1017/aer.2015.1.

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This special issue is one of a number of activities taking place this year to celebrate the founding of the Royal Aeronautical Society in 1866. The decision to form the Society was taken on 12 January 1866 at a meeting of distinguished people held in London and chaired by the Duke of Argyll. One of those present, James Glaisher, addressed the gathering and it is interesting to revisit an extract from his statement: “The first application of the balloon as a means of ascending into the upper regions of the atmosphere has been almost within the recollection of men now living but with the exception of some of the early experimenters it has scarcely occupied the attention of scientific men, nor has the subject of aeronautics been properly recognised as a distinct branch of science. . .”. The meeting resolved “that it is desirable to form a Society for the purpose of increasing by experiments our knowledge of Aeronautics and for other purposes incidental thereto and that a Society be now formed under the title of the ‘Aeronautical Society of Great Britain’ to be supported by annual subscriptions and donations.”
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7

Goetzendorf-Grabowski, Tomasz. "Multi-disciplinary optimization in aeronautical engineering." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 231, no. 12 (May 12, 2017): 2305–13. http://dx.doi.org/10.1177/0954410017706994.

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Nowadays, optimization is a very popular tool used to improve existing projects. The optimization covers different disciplines by linking them into multidisciplinary process of design. Existing software tools allow to very effectively solve particular problems giving high quality solutions which were previously very hard to achieve. Aeronautical engineering is a domain/field which links many disciplines: aerodynamics, stability, control, structural analysis, materials, propulsion systems, avionics, etc. Therefore, the multidisciplinary optimization results in very significant progress not only in aircraft design but also in air transport, which links technical aspects with economical questions. The paper presents selected aspects of using the multidisciplinary optimization in aeronautical engineering with special focus on multidisciplinary aircraft design.
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8

Klemin, Alexander. "TRAINING AND RESEARCH IN AERONAUTICAL ENGINEERING." Journal of the American Society for Naval Engineers 46, no. 4 (March 18, 2009): 527–30. http://dx.doi.org/10.1111/j.1559-3584.1934.tb02575.x.

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9

Arti, Endang Sugih, Elfi Amir, Dini Wagini, Togi Adnan Maruli, Ferry Budi Cahyono, Agustono Agustono, and Rini Sadiatmi. "Sosialisasi Program Studi Penerangan Aeronautika Di SMA Negeri 3 Kabupaten Tangerang." Jurnal Pengabdian Kepada Masyarakat (JPKM) Langit Biru 5, no. 01 (March 1, 2024): 1–5. http://dx.doi.org/10.54147/jpkm.v5i01.866.

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Kegiatan Pengabdian Kepada Masyarakat (PKM) ini didasarkan pada UU No. 20 Tahun 2003 tentang Sistem Pendidikan Nasional dan PERPRES No. 68 tahun 2022 tentang Revitalisasi Pendidikan Vokasi. PPI Curug merupakan salah satu perguruan tinggi vokasi dibawah Kementerian Perhubungan yang dekat /mudah aksesnya, biaya relatif terjangkau, jangka waktu pendidikan relative cepat dengan menghasilkan lulusan siap kerja dengan pemberian bekal kompetensi / keterampilan lapangan. PKM ini dilaksanakan dalam bentuk sosialiasi dan bertujuan untuk lebih mengenalkan program studi D.III Penerangan Aeronautika di PPI Curug yang lulusannya akan bekerja di dunia penerbangan dan bertugas menyampaikan informasi penerbangan dalam bentuk self-briefing, Notam (Notice To Airmen), AIP (Aeronautical Information Publication, Aeronautical chart/peta) kepada siswa SMAN 3 Tangerang. Diharapkan dengan penjelasan ini peserta PKM akan termotivasi dan tumbuh minatnya untuk memilih melanjutkan pendidikannya di PPI Curug, terutama pada Prodi D.III Penerangan Aeronautika. Kegiatan berjalan lancar dan animo siswa SMAN 3 Kabupaten Tangerang sangat tertarik dengan PPI Curug terbukti dengan banyaknya pertanyaan yang diajukan.
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10

Pertiwi, Dewanti Ratna. "Needs Analysis of English for Aeronautical Engineering Purposes at STT Adisutjipto Yogyakarta." LLT Journal: A Journal on Language and Language Teaching 19, no. 2 (January 9, 2017): 105–14. http://dx.doi.org/10.24071/llt.v19i2.304.

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In the context of ESP, needs analysis is the first step to develop a program. Needs analysis is conducted to investigate the present students mastery and the need of the future work field. This study aims to investigate the needs analysis of English for aeronautical engineering. The study employed a survey technique in the form of distributing questionnaires and interview for the lecturers, and centre of quality insurance. Indonesian qualification framework to standardize the graduate of aeronautical engineering with the national criteria is used as the source of developing the research instruments. The result of the study is expected to be able to build the foundation of developing better English course for aeronautical engineering students.DOI: https://doi.org/10.24071/llt.2016.190205
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11

Yang, Guowei. "Transonic aeroelastic numerical simulation in aeronautical engineering." International Journal of Computational Fluid Dynamics 20, no. 5 (June 2006): 339–47. http://dx.doi.org/10.1080/10618560600916973.

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12

Zheng, Zheng, Kemao Peng, Wenbo Du, and Guangquan Zhang. "Modeling, Control, and Optimization in Aeronautical Engineering." Scientific World Journal 2015 (2015): 1–2. http://dx.doi.org/10.1155/2015/979107.

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13

Duggins, R. K. "Aeronautical Engineering Education for the Armed Forces." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 206, no. 2 (July 1992): 137–42. http://dx.doi.org/10.1243/pime_proc_1992_206_250_02.

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A discussion is given of the arrangements that have been made for aeronautical and aerospace engineering education of members of the armed forces in the United Kingdom, the United States of America, West Germany and Australia. A striking feature of the comparisons is shown to be the extent of the differences in the arrangements in the various countries. A less detailed and less rigorous version of the paper was presented at the Aerotech 92 conference (1).
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14

Uzule, Kristine, and Irina Kuzmina-Merlino. "THE CONNECTION BETWEEN AN AIRPORT TYPE AND REVENUE STRUCTURE AT BALTIC STATES AIRPORTS." Aviation 26, no. 4 (November 28, 2022): 183–94. http://dx.doi.org/10.3846/aviation.2022.17854.

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Airports are not only engines of transportation of passengers and cargo, but also commercial enterprises offering services far beyond transportation, which is why their revenues are formed by both aeronautical and non-aeronautical sales. Aeronautical revenues of some large European airports are higher than non-aeronautical revenues, whereas some regional and secondary European airports demonstrate the opposite trend. The aim of this research was to determine if there is a connection between an airport type and the ratio of aeronautical and non-aeronautical revenues at Baltic States airports in way that is consistent with the previous research. The aim was attained in three stages. The first, the definitions of the main and secondary airports were constructed via discourse analysis. The second, the structure of airport revenues of the selected Baltic States airports was analysed. The third, conclusions were made regarding a connection between an airport type and the revenue structure of these Baltic States airports. On the one hand, the research results suggested there might be a connection between an airport type and the revenue structure although this question requires further research, and on the other hand, the financial analysis showed that airports with a higher share of non-aeronautical revenues than aeronautical revenues were more resilient to crises.
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15

Li, Zhao, Na Lu, Yuanyuan Lu, Jing Cao, and Wei Hou. "Research on the Construction of Aviation Materials Industry College under the Background of New Engineering." Journal of Education, Humanities and Social Sciences 4 (November 17, 2022): 21–23. http://dx.doi.org/10.54097/ehss.v4i.2716.

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The construction of new engineering is the direction of my country engineering education reform based on the new requirements of my country's strategic development, the new situation of international competition and the new requirements of Lide Shuren. An important carrier of the docking industry chain, aviation materials are an indispensable part of the aviation industry. This paper takes the College of Aeronautical Materials Industry under the background of new engineering as the object, and takes the College of Materials Engineering of Xi'an Aeronautical University as an example to study its construction content such as talent training mode, in order to provide reference and reference for the school to carry out the construction of new engineering.
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16

Huang, Guo Qing, Cheng Gen Zhang, and Hong Bo Yuan. "Recognition of MQAM Signals in the Aeronautical Communication." Advanced Materials Research 765-767 (September 2013): 2647–52. http://dx.doi.org/10.4028/www.scientific.net/amr.765-767.2647.

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For the complex recognition of signals in the aeronautical communication, the recognition of the star-type MQAM signals is studied under the aeronautical channel. The different scenarios of the aeronautical channel are analyzed and the reasonable channel model is established. The high order cumulant recognition algorithm which applies to the aeronautical channel is proposed, the invariant classification characteristics of modulation signals are constructed by this algorithm, and this algorithm is improved by using the receive diversity technique. Simulation results show that this algorithm significantly improves the correct recognition rate of the received signals has the good anti-fading and anti-noise performance and meets the requirements of the modulation recognition of MQAM signals under the aeronautical channel.
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17

McManus, Hugh L. "Revised Mechanics Curriculum in the Department of Aeronautics and Astronautics at MIT." Applied Mechanics Reviews 47, no. 6S (June 1, 1994): S305—S309. http://dx.doi.org/10.1115/1.3124430.

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The mechanics curriculum in the Department of Aeronautics and Astronautics at MIT is being revised as part of a broad revision of the entire research and teaching program of the department. The traditional MIT approach of fundamental engineering science taught with an emphasis on its practical application has not changed, but it has been complemented by some important innovations. The mechanics curriculum has been revised and updated from the ground up. It has been coordinated with the rest of the aeronautical engineering curriculum, assuring that students understand the place of mechanics in the overall engineering of an aerospace system. Material science has been integrated throughout the mechanics curriculum. Finally, mechanics education plays a large role in teaching the “implicit curriculum”, a formalization of the skills and knowledge that a student is expected to gain outside of the stated curriculum.
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18

Tatzl, Dietmar. "Design-Build-Write: Increasing The Impact Of English For Specific Purposes Learning And Teaching In Aeronautical Engineering Education Through Multiple Intelligences Task Design." American Journal of Engineering Education (AJEE) 2, no. 2 (November 23, 2011): 55–66. http://dx.doi.org/10.19030/ajee.v2i2.6638.

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This article presents an English for Specific Purposes (ESP) task developed for teaching aeronautical engineering students. The task Design-Build-Write rests on the assumption that engineering students are skilled at mathematical reasoning, problem solving, drawing and constructing. In Gardner’s 1983 Multiple Intelligences (MI) theory, these skills strongly correspond to the logical-mathematical, bodily-kinesthetic and spatial intelligences. The current task combines creativity, innovation and problem solving with the description of technical concepts. An enthusiastic learner response in class suggests that the target group of aeronautical engineering students could be engaged and captivated by this assignment.
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19

Arias-Montano, Alfredo, Carlos A. Coello Coello, and Efrén Mezura-Montes. "Multiobjective Evolutionary Algorithms in Aeronautical and Aerospace Engineering." IEEE Transactions on Evolutionary Computation 16, no. 5 (October 2012): 662–94. http://dx.doi.org/10.1109/tevc.2011.2169968.

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20

Staack, I., K. Amadori, and C. Jouannet. "A holistic engineering approach to aeronautical product development." Aeronautical Journal 123, no. 1268 (August 5, 2019): 1545–60. http://dx.doi.org/10.1017/aer.2019.51.

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ABSTRACTProduct development, especially in aerospace, has become more and more interconnected with its operational environment. In a constant changing world, the operational environment will be subjected to changes during the life cycle of the product. The operational environment will be affected by not only technical and non-technical perturbations, but also economical, managerial and regulatory decisions, thus requiring a more global product development approach. One way to try tackling such complex and intertwined problem advocates studying the envisioned product or system in the context of system of systems (SoS) engineering. SoSs are all around us, probably in any field of engineering, ranging from integrated transport systems, public infrastructure systems to modern homes equipped with sensors and smart appliances; from cities filling with autonomous vehicle to defence systems.Since also aerospace systems are certainly affected, this work will present a holistic approach to aerospace product development that tries spanning from needs to technology assessment. The proposed approach will be presented and analysed and key enablers and future research directions will be highlighted from an interdisciplinary point of view. Consideration of the surrounding world will require to look beyond classical engineering disciplines.
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21

SUZUKI, Shinji, Kenji KARASAWA, and Daiichirou MATSUNAGA. "Pilot Modeling and Intelligent Interface for Aeronautical Engineering." Proceedings of the Conference on Information, Intelligence and Precision Equipment : IIP 2002 (2002): 9–12. http://dx.doi.org/10.1299/jsmeiip.2002.9.

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22

Duggins, R. K., and J. P. Baird. "An Aeronautical Engineering Degree Course Designed For Prospective Pilots." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 209, no. 2 (April 1995): 161–63. http://dx.doi.org/10.1243/pime_proc_1995_209_283_02.

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A new aeronautical engineering degree course has been designed and introduced at the Australian Defence Force Academy for prospective pilots. It is a three-year Bachelor of Technology course leading to engineering technologist status.
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23

Jenab, Kouroush, Nikita Ottosen, and Saeid Moslehpour. "Application of scenario-driven hazard analysis in the solid rocket booster." International Journal of Engineering & Technology 5, no. 1 (January 7, 2016): 16. http://dx.doi.org/10.14419/ijet.v5i1.4673.

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Bibliographical Notes: Kouroush Jenab is a senior member of IEEE, received the B.Sc. degree from the IE Department at Isfahan University of Technology (1989), the M.Sc. degree from the IE Department at Tehran Polytechnic (1992), and the Ph.D. degree from the Department of Mechanical Engineering at the University of Ottawa (2005). He served as a senior engineer/manager in auto, and high-tech industries for 18 years. He joined the National Research Council Canada as a research officer where he participated in several international research projects. In 2006, he joined the Department of Mechanical and Industrial Engineering at Ryerson University, Toronto as assistant professor. Currently, Dr. Jenab is Faculty of the College of Aeronautics at Embry-riddle Aeronautical University, FL, USA. He has published over 110 papers in international scientific journals based on his experiences in industries.Nikita Ottosen is a current Systems Engineering graduate student at Embry-Riddle Aeronautical University. She received her undergraduate degree from ERAU in Aeronautics and is currently working as an Assistant Campus Director at the Crestview, FL campus. She gained valuable knowledge previously working for the Boeing Company and Seattle-Tacoma International Airport, known as The Port of Seattle, in Seattle, Washington. During her time at The Port of Seattle she worked alongside the Wildlife Management department to conduct a study on effective wildlife management strategies. Her study will become a part of a future Airport Cooperative Research Program (ACRP) publication, sponsored by the FAA’s Transportation Research Board of the National Academies.Saeid Moslehpour is a full professor and department chair in the Electrical and Computer Engineering Department in the College of Engineering, Technology, and Architecture at the University of Hartford. He holds Ph.D. (1993) from Iowa State University and Bachelor of Science (1989) and Master of Science (1990) degrees from University of Central Missouri. His research interests include failure analysis, logic design, CPLDs, FPGAs, Embedded electronic system testing and distance learning.
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Yadav, Devinder K., and Hamid Nikraz. "AN INSIGHT INTO PROFESSIONAL REGISTRATION OF TECHNICAL PERSONNEL IN AERONAUTICAL ENGINEERING INDUSTRY." Aviation 16, no. 2 (June 29, 2012): 51–55. http://dx.doi.org/10.3846/16487788.2012.701854.

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The aeronautical industry is a powerful force for progress in our modern global society. Industrial activities in this industry started to accelerate in the beginning of the 20th century, and the number of aircraft in airspace for civil purposes started increasing. Consequently, the industry and the personnel associated with aircraft were required to be regulated to ensure the safety and reliability of the product. Currently, various categories of personnel related to operations, airworthiness, and maintenance of aircraft are licensed by statute. Government authorities consider registration or licensing an instrument for controlling and regulating the professionals. This paper is primarily focused on licensing and approval of different categories of aeronautical engineers. It discusses the importance of the licensing of engineers in the aeronautical industry and presents a critical review of various licensing standards and practices, including the standard recommended by the International Civil Aviation Organisation (ICAO). This paper also argues that the license issued by a contracting state of the ICAO must be fully convertible in another state, because it is granted by a member state in conformance with the standards recommended by the ICAO.
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AGAN, MARTIN J., DANIEL I. NAKAMURA, ALAN D. CAMPBELL, ROBERT H. STERNOWSKI, WENDY A. WHITING, and LEON SHAMESON. "ACTS AERONAUTICAL EXPERIMENTS." International Journal of Satellite Communications 14, no. 3 (May 1996): 233–47. http://dx.doi.org/10.1002/(sici)1099-1247(199605)14:3<233::aid-sat544>3.0.co;2-5.

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26

Evdokimenkov, V. N., N. B. Toporov, M. N. Krasilshchikov, K. S. Anisimov, and K. I. Sypalo. "PROCEDURE OF MULTIDISCIPLINARY AERONAUTICAL ENGINEERING BASED ON AUTOMATED INFORMATION – ANALYTICAL SUPPORT SYSTEM." Vestnik komp'iuternykh i informatsionnykh tekhnologii, no. 229 (July 2023): 35–43. http://dx.doi.org/10.14489/vkit.2023.07.pp.035-043.

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The article demonstrates both architecture and software of the automated information – analytical support system, intended for implementation of multidisciplinary aeronautical engineering procedure. The system discussed should generate as a first approximation the design of the prospective aircraft, which could be implemented, considering actual scientific and technical level of aeronautical engineering. In case of impossibility to develop aircraft according to corresponding multidisciplinary requirements, basing on accumulated scientific and technical groundwork, it is necessary to determine priority solutions, which could provide development of discussed prospective aircraft. Implementation of described above opportunities is provided due to utilization of three problem-oriented blocks (DSS – decision support systems): DSS1 provides generation of the so called conceptual model of aircraft design problem, DSS2 generates analytical model of aircraft design problem and controls calculation procedures by generation of alternative versions of requirements applying to prospective aircraft, being developed, DSS3 provides automated support of generated aeronautical engineering solutions estimation in order to select most acceptable one. The article contains description of software, which is basis for solution of all above discussed problems, as well as approach of these problems solution as optimization ones. The article contains also result of developed both methods and software utilization applying to prospective transport aircraft design.
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27

Goraj, Zdobyslaw, Jonas Stankunas, Martinsh Kleinhofs, Villu Mikita, and Antonin Pištek. "A SHORT HISTORY OF SEMINARS ON “RECENT RESEARCH AND DESIGN PROGRESS IN AERONAUTICAL ENGINEERING AND ITS INFLUENCE ON EDUCATION”." Aviation 11, no. 1 (March 31, 2007): 3–5. http://dx.doi.org/10.3846/16487788.2007.9635948.

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The aeronautical sciences and aerospace industry are by nature international. Coming from this thesis, we decided in 1994 to organise an international meeting, further called the Seminar, devoted to “RECENT RESEARCH AND DESIGN PROGRESS IN AERONAUTICAL ENGINEERING AND ITS INFLUENCE ON EDUCATION”. The objective of that first Seminar and following ones was to organise a multinational forum for discussion and interchange of aeronautical issues and subjects, focusing on their influence on university education. Other goals included promoting international co-operation in the study of the problems in aeronautical science and technology in which there was a common interest and facilitating personal contacts between scientists, university lecturers, and industrial engineers. Our area of interest was aeronautical technology, as it is widely understood. The special focus of our Seminars was concentrated on Aircraft Design, Aircraft Oriented Aerodynamics, Flight Dynamics, Helicopter Dynamics, Computational Fluid Dynamics, Materials and Structures, Control and Flight Tests. All these topics and their influence on the teaching process at a technical university were considered — what we believe is a specific feature of our Seminars. We notice a mutual influence between contemporary research and education; it is impossible to deliver a modern university lecture without conducting one’s own serious research or design, and it is almost impossible to become a serious, successful researcher or designer without being a graduate of a good, contemporary university. The other specific feature of our Seminars is a student session. An international jury of professors and deans from aerospace faculties all over the world observes the sessions and awarded the best student papers diplomas (sometimes with small prizes contributed by different institutions). We believe that the student sessions promote personal contacts between students and foreign lecturers and encourage students to work harder in the future. For all of us, it is the promise of a new generation of engineers, designers and scientists.
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Murman, E. M., M. Walton, and E. Rebentisch. "Challenges in the better, faster, cheaper era of aeronautical design, engineering and manufacturing." Aeronautical Journal 104, no. 1040 (October 2000): 481–89. http://dx.doi.org/10.1017/s0001924000091983.

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Abstract 'Better, faster, cheaper’ (BFC) emerged in the 1990s as a new paradigm for aerospace products. In this paper, we examine some of the underlying reasons for BFC and offer some thoughts to help frame the thinking and action of aerospace industry professionals in this new era. Examination of literature on industrial innovation indicates that aeronautical products have evolved to a ‘dominant design’ and entered the ‘specific phase’ of their product life cycle. Innovation in this phase centers on: incremental product improvement, especially for productivity and quality; process technology; technological innovations that offer superior substitutes. The first two of these are aligned with BFC objectives. The concepts of ‘value’ and ‘best lifecycle value’ are introduced as conceptual frameworks. Value is offered as a metric for BFC. Risk management is intimately tied to achieving value and needs to be integrated into aeronautical processes. The process technology area is addressed by considering ‘lean’ practices for design, engineering and manufacturing. Illustrative results of process improvements from the seven-year Lean Aerospace Initiative research programme at MIT indicate opportunities to achieve BFC. Concluding remarks offer some challenges to industry, government and academics in aeronautical design, engineering and manufacturing.
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Brito-Acuña, Guillermo. "Aeronautic maturity cybersecurity: a framework." DYNA 90, no. 227 (July 13, 2023): 24–34. http://dx.doi.org/10.15446/dyna.v90n227.107420.

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This article presents the results of a systematic review of the methods to implement cybersecurity maturity. Based on them, it proposes a framework for excellence in aeronautical cybersecurity that integrates the objectives of aeronautical cybersecurity with capabilities and requirements, which contributes to increasing the maturity of aeronautical cybersecurity. It exposes 13 objectives with 120 capabilities and 5 functional maturity levels to gradually meet up to 600 aeronautical cybersecurity requirements. Which were taken from articles with good practices associated with publications of the last 5 years and the criteria resulting from the collaboration of managers and the validation of experts in the industry, which allowed it to be enriched with good practices associated with the management of cybersecurity and the resilience of these infrastructures.
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Zhang Guihua, 张桂华, 王菲 Wang Fei, 陈斅恔 Chen Xiaoxiao, 王琳 Wang Lin, 李丽 Li Li, 蔡伟 Cai Wei, and 张珊 Zhang Shan. "The Application of Precision Laser Welding in Aeronautical Engineering." Applied laser 30, no. 2 (2010): 111–14. http://dx.doi.org/10.3788/al20103002.0111.

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31

Sharma, S. "Adaptation of modelling and identification: an aeronautical engineering perspective." International Journal of Modelling, Identification and Control 6, no. 2 (2009): 104. http://dx.doi.org/10.1504/ijmic.2009.024326.

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32

Gil-Sanchez, Luis, Rafael Masot, and Miguel Alcaniz. "Teaching Electronics to Aeronautical Engineering Students by Developing Projects." IEEE Revista Iberoamericana de Tecnologias del Aprendizaje 10, no. 4 (November 2015): 282–89. http://dx.doi.org/10.1109/rita.2015.2486398.

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33

McDougall, N. "BAE Systems/EPSRC integrated research programme in aeronautical engineering." Aeronautical Journal 110, no. 1104 (February 2006): 121–24. http://dx.doi.org/10.1017/s000192400000107x.

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Abstract BAE Systems and the Engineering and Physical Sciences Research Council (EPSRC) have recently formed a partnership to invest in strategic research in aerospace and defence. The framework which has been developed as part of this new alliance places a strong emphasis on collaboration. This contrasts with the conventional approach to industry led research which is normally based on the establishment of ‘centres of excellence’ in specific subject areas. By using a collaborative approach, the funding partners aim to benefit from inter-disciplinary collaboration which will take place during the project, giving rise to a more effective use of the invested funds. The objective of the research programme is to develop technologies which would support the design of low cost (both to acquire and operate) flapless unmanned aerial vehicles (UAVs). This work includes fundamental aerodynamic research to provide control forces without the use of conventional flaps, coupled with developments in the areas of control systems, manufacturing engineering, structural engineering, the electromagnetic behaviour of these structures and design optimisation. The output from the research has been extended to include the design, manufacture, assembly and flight of a demonstrator vehicle, which will provide the research teams with a platform on which to evaluate the performance of their technology in a realistic flight environment. A total of fourteen research groups at ten universities are involved in the five year programme, which has a total value of £6·5M (€9·75M).
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Bravo-Mosquera, Pedro David, Nelson David Cisneros-Insuasti, Fabiola Mosquera-Rivadeneira, and Bryann Avendaño-Uribe. "STEM Learning Based on Aircraft Design: An Interdisciplinary Strategy Developed to Science Clubs Colombia." Ciencia y Poder Aéreo 14, no. 1 (June 30, 2019): 204–27. http://dx.doi.org/10.18667/cienciaypoderaereo.629.

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This article describes a STEM learning strategy based on aircraft design in order to promote the development of aeronautical science in Colombia. This teaching strategy was developed by specialized instructors from the Science Clubs Colombia program, seeking to stimulate in young Colombian students their passion for science, technology, and innovation, and in the process, create an international network of academic collaborations. Bloom’s taxonomy was used to classify and select both the educational objectives, as well as the teaching plan of the science club. STEM activities that encourage students to perform hands-on learning experiences were the basis of this framework. Essentially, interdisciplinary activities involving aeronautics, electronics, computational simulations, and technical drawing; characterized this science club. As a result, the students were able to design, manufacture and test their own hand-launched air-model, applying all steps of the scientific method: the conception of ideas, design, execution of experiments, and communication of results. After the first flight tests of the air-models, the students disclosed an ability to apply their mathematics knowledge in conjunction with their science learning on the forces of flight, in order to improve their launching technique. Therefore, both the time and range of the air-models were enhanced. Finally, both students and instructors benefited throughout the learning interaction, since it was the first time that a rural community is the scenario of an aeronautical engineering training process. It is expected that the dissemination of this material will contribute to the Colombian aeronautical community, giving outlooks for new research proposals and cooperation frameworks between government entities and universities.
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Cummings, D., and C. G. Wildey. "Military aeronautical satellite communications." IEE Proceedings F Communications, Radar and Signal Processing 133, no. 4 (1986): 411. http://dx.doi.org/10.1049/ip-f-1.1986.0066.

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36

Sobieszczanski-Sobieski, Jaroslaw, and Inderjit Chopra. "Multidisciplinary Optimization of Aeronautical Systems." Journal of Aircraft 27, no. 12 (December 1990): 977–78. http://dx.doi.org/10.2514/3.56840.

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37

Perrins, Erik. "FEC Systems for Aeronautical Telemetry." IEEE Transactions on Aerospace and Electronic Systems 49, no. 4 (October 2014): 2340–52. http://dx.doi.org/10.1109/taes.2014.6619932.

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38

Caetano, Mauro. "AVIATION ACCIDENT AND INCIDENT FORECASTING COMBINING OCCURRENCE INVESTIGATION AND METEOROLOGICAL DATA USING MACHINE LEARNING." Aviation 27, no. 1 (March 23, 2023): 47–56. http://dx.doi.org/10.3846/aviation.2023.18641.

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Studies on safety in aviation are necessary for the development of new technologies to forecast and prevent aeronautical accidents and incidents. When predicting these occurrences, the literature frequently considers the internal characteristics of aeronautical operations, such as aircraft telemetry and flight procedures, or external characteristics, such as meteorological conditions, with only few relationships being identified between the two. In this study, data from 6,188 aeronautical occurrences involving accidents, incidents, and serious incidents, in Brazil between January 2010 and October 2021, as well as meteorological data from two automatic weather stations, totaling more than 2.8 million observations, were investigated using machine learning tools. For data analysis, decision tree, extra trees, Gaussian naive Bayes, gradient boosting, and k-nearest neighbor classifiers with a high identification accuracy of 96.20% were used. Consequently, the developed algorithm can predict occurrences as functions of operational and meteorological patterns. Variables such as maximum take-off weight, aircraft registration and model, and wind direction are among the main forecasters of aeronautical accidents or incidents. This study provides insight into the development of new technologies and measures to prevent such occurrences.
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Ropp, Timothy, Jay Hedden, Philip Mick, J. Michael Davis, and S. Wesley Austin Jr. "Incorporating Advanced Aircraft Technologies into an Aeronautical Engineering Technology Curriculum." Journal of Aviation Technology and Engineering 2, no. 1 (October 2012): 116–24. http://dx.doi.org/10.5703/1288284314863.

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40

Shishkin, S. V., and S. S. Shishkin. "The application of rivets with shape memory in aeronautical engineering." Journal of Machinery Manufacture and Reliability 39, no. 2 (April 2010): 179–84. http://dx.doi.org/10.3103/s1052618810020135.

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41

Viscardi, Massimo, Maurizio Arena, Liberata Guadagno, Luigi Vertuccio, and Giuseppina Barra. "Multi-functional nanotechnology integration for aeronautical structures performance enhancement." International Journal of Structural Integrity 9, no. 6 (December 3, 2018): 737–52. http://dx.doi.org/10.1108/ijsi-11-2017-0060.

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Purpose The purpose of this paper is to evaluate the applicative potentiality of functional/self-responsive materials in aeronautics. In particular, the study aims to experimentally validate the enhancement of structural performances of carbon fibers samples in the presence of nanofillers, as multi-walled carbon nanontubes or microcapsules for the self-healing functionality. Design/methodology/approach The paper opted for a mechanical study. Experimental static and dynamic tests on “blank” and modified formulations were performed in order to estimate both strength and damping parameters. A cantilever beam test set-up has been proposed. As a parallel activity, a numerical FE approach has been introduced to assess the correct modeling of the system. Findings The paper provides practical and empirical insights about how self-responsive materials react to mechanical solicitations. It suggests that reinforcing a sample positively affects the samples properties since they, de facto, improve the global structural performance. This work highlights that the addition of carbon nanotubes strongly improves the mechanical properties with a simultaneous slight enhancement in the damping performance. Damping properties are, instead, strongly enhanced by the addition of self-healing components. A balanced combination of both fillers could be adopted to increase electrical conductivity and to improve global performance in damping and auto-repairing properties. Practical implications The paper includes implications for the use of lightweight composite materials in aeronautics. Originality/value This paper fulfills an identified need to study new lightweight self-responsive smart materials for aeronautical structural application.
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Kurosawa, Masahiro. "Obstruction Marking and Aeronautical Lighting." JOURNAL OF THE ILLUMINATING ENGINEERING INSTITUTE OF JAPAN 73, no. 3 (1989): 151–54. http://dx.doi.org/10.2150/jieij1980.73.3_151.

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43

Novák, Andrej. "MODERN TELECOMMUNICATION NETWORKS IN THE AERONAUTICAL TELECOMMUNICATION NETWORK (ATN)." Aviation 10, no. 4 (December 31, 2006): 14–17. http://dx.doi.org/10.3846/16487788.2006.9635942.

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This paper summarizes the results of a study of modern telecommunication technology in the Aeronautical Telecommunication Network. The ATN is a data communications inter‐network that provides its users a robust and reliable Air/Ground and Ground/Ground communications service. The Air Telecommunication Network is build on a ring of fixed telecommunication networks. The article deals with the integration of modern telecommunication technology into the still developing sector of aeronautical telecommunication.
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44

Haines, A. B. "High lift and separation control, an introductory review paper." Aeronautical Journal 99, no. 989 (November 1995): 359–60. http://dx.doi.org/10.1017/s0001924000028669.

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The Royal Aeronautical Society Aerodynamics Group organised a CEAS European Forum on High Lift and Separation Control which was held at the University of Bath on 29-31 March 1995. This paper gives an idea of the scope of the Forum and of the main conclusions that emerged and it is followed in this special issue of The Aeronautical Journalby four papers that were invited for the Forum.
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45

Samkov, Alexei, and Valeriy Silkov. "SOME PARTICULAR INDICES OF EFFECTIVENESS OF UNMANNED AERIAL VEHICLE APPLICATION." Aviation 16, no. 3 (October 2, 2012): 57–62. http://dx.doi.org/10.3846/16487788.2012.732302.

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In this article, a methodological approach based on a complex indicator (productivity – cost – efficiency) to evaluate the efficiency of using unmanned aeronautical systems is presented as a solution to the problem of searching for objects on the ground. This methodological approach can be used as a substantiation of decisions taken during the act of searching for specific objects and as a comparative evaluation of unmanned aeronautical systems by taking into account their characteristics.
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BARAN, Daniela, Romeo MARIN, Mihaela PETRE, and Radu BOGATEANU. "A comparative study evaluating the hybrid composite-metal aviation structure." INCAS BULLETIN 13, no. 2 (June 4, 2021): 3–9. http://dx.doi.org/10.13111/2066-8201.2021.13.2.1.

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The main purpose of this paper is to develop some numerical experiences based on mechanical tests performed on a hybrid composite metal aeronautical structure using finite element commercial codes (here NASTRAN). The results of the numerical simulations are consistent with the laboratory tests and encourage us to continue to improve the models using NASTRAN capabilities to obtain a realistic simulation of aeronautical structures made of such composites, taking into account their special properties.
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Samkov, Alexei, Galyna Suslova, Vladimir Litvinenko, and Yurii Zakharchenko. "METHODOLOGICAL ASPECTS OF AERONAUTICAL SYSTEM UPGRADE." Aviation 14, no. 4 (December 31, 2010): 104–11. http://dx.doi.org/10.3846/aviation.2010.16.

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This article is devoted to the methodological aspects of upgrading aircraft, including the complex of mathematical methods, algorithms and criteria which allow the objective of the assigned research problem to be met. Santrauka Šiame straipsnyje nagrinejami metodologiniai orlaiviu modernizavimo aspektai, iskaitant matematiniu metodu, algoritmu ir kriteriju kompleksa, kuris leidžia priimti tam tikra mokslini sprendima.
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Hernández-Ramírez, Carlos Arturo, Diana Marcela Rodríguez-Toro, Oscar Andrés Rivera-Ramirez, and Sebastian Camilo Medina-Montero. "Development of a HTS application for the Colombian aircraft manufacturing industry." DYNA 90, no. 229 (October 26, 2023): 25–34. http://dx.doi.org/10.15446/dyna.v90n229.108947.

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The Colombian manufacturing industry's diversity and capacity for high-quality production are creating opportunities for increased participation in the aeronautical market. To tap into this potential, companies must adapt processes to adhere to global quality and safety standards. This research led to the creation of a specialized software tool capable of managing documents and risks linked to safety analysis during aeronautical product certification and manufacturing. By identifying local industry needs and essential risk-tracking features, the software was tailored to suit Colombian practices. This tool enables data management and risk monitoring throughout the manufacturing process, promoting standardization and centralization of risk-related information while meeting certification requirements and alleviating constraints tied to implementing a new risk monitoring system. Despite possessing the necessary potential, the Colombian manufacturing industry has yet to adopt the essential tools for certifying products under international standards in the aeronautical sector.
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ISHIDE, Akira, Mitsuhiro FUJITA, Hideomi NASU, Kazuaki HOSHINOO, Minoru ITO, Kenji NIIMI, Tatsuto YAMADA, and Shuji NISHI. "Aeronautical Data Communication Experiment Using Engineering Test Satellite V (ETS-V)." Journal of Japan Institute of Navigation 82 (1990): 113–19. http://dx.doi.org/10.9749/jin.82.113.

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Skvortsov, Evgueny Borisovich, and Anna Sergeevna Shelekhova. "METHOD FOR ANALYSIS OF ALTERNATIVES IN CONCEPTUAL DESIGN IN AERONAUTICAL ENGINEERING." TsAGI Science Journal 48, no. 5 (2017): 459–68. http://dx.doi.org/10.1615/tsagiscij.2017025106.

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