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Littérature scientifique sur le sujet « Aerospace engineers »

Auteur : Grafiati
Publié le 4 juin 2021
Mis à jour le 1 août 2024

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Articles de revues sur le sujet "Aerospace engineers"

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Knyazeva, M. D., et E. M. Mitrofanov. « School of aerospace engineers ». Geodesy and Cartography 955, no 1 (20 février 2020) : 59–64. http://dx.doi.org/10.22389/0016-7126-2020-955-1-59-64.

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The authors discuss the project of creating a school of aerospace engineers, as well as the need to take additional measures to expand the opportunities of space education for children. These are promotion of schoolchildren’ s career guidance in the aerospace sphere, popularization of cosmonautics and involvement of young people in engineering and space activities, as well as developing the motivation of the younger generation to choose technical professions related to Cosmonautics, space research and the use of space technologies. Space activities are necessary as a significant incentive for the developing technologies and basic science. The authors propose to promote the intellectual development of students through competitions, research, scientific and project activities. The implementation of the project is a systematic, consistent work of the project team and is to contribute to solving the problem of the students’ career guidance in aerospace education to perform the tasks. Today, the relevance of technical education is very high and there is a need to improve the level of the students’ knowledge in the field of exact Sciences, to emphasize the importance of technical education.
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Lastovenko, Daria, et Alena Aleksandrovna Muzalevskaya. « Expert assessment of the important professional competencies of aerospace engineers ». Психология и Психотехника, no 1 (janvier 2021) : 42–50. http://dx.doi.org/10.7256/2454-0722.2021.1.34924.

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This article is dedicated to examination of the important professional competencies of aerospace engineers and specificity of their professional activity. The study represents an expert assessment of the activity and important professional competencies of aerospace engineers. The research program consisted of several stages. The first stage includes the formation of the relevant expert group and assessment of the characteristics of activity and important professional competencies based on the methodology of expert assessment of I. L. Solomin. The second stage implies the expert ranking of the important psychological characteristics in the activity of aerospace, and determination of psychological factors that affect the solution of professional tasks. Based on the acquired results, the author reveals the socioeconomic, industrial-technical, and psychological characteristics of the activity of aerospace engineers. The most important professional competencies of aerospace engineers include: attention span, ability to predict, psychic stability, memory, imagination, and distress tolerance. The effective solution of professional tasks by aerospace engineers requires psychological resilience to external influences, ability to maintain attention control, etc. The acquired data can be valuable in assessment of the important professional competencies of young specialists, as well as carrying out a set of measures aimed at developing attention span, ability to predict, and psychic stability.
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Swift, Douglas Keith. « MISCONCEPTIONS CONCERNING THE VALUE OF SYSTEMS ENGINEERS ». INCOSE International Symposium 3, no 1 (juillet 1993) : 795–800. http://dx.doi.org/10.1002/j.2334-5837.1993.tb01662.x.

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AbstractIn the community of professional engineers, the Systems Engineer is often perceived as an inferior engineer. Misconceptions are especially prevalent among technical design engineers for whom up‐front Systems Engineering should be considered absolutely essential. The Systems Engineer often works in an environment where his engineering peers, and sometimes even management, considers his contribution to be subordinate, of second‐class value, and at times, a nuisance. This paper examines this critical problem from the perspective of an aerospace engineer who spent five years working as a flight controls design engineer (where Systems Engineering was treated with considerable bias), and men transferred into Systems Engineering and has since been working on the opposite side of the fence. An exploration into the causes of the phenomena is detailed in the paper, with special emphasis on the factors perpetuating these misconceptions. A set of practical recommendations (some applicable for working Systems Engineers and some applicable for Managers) is then presented for use in mitigating and eventually dissolving these non‐productive barriers.
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Haghighattalab, Sakineh, An Chen et Mohammadreza Saghamanesh. « Is Engineering Ethics Important for Aerospace Engineers ? » MATEC Web of Conferences 179 (2018) : 03009. http://dx.doi.org/10.1051/matecconf/201817903009.

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Engineering as a profession has a direct effect on society and the environment. Engineering ethics is a part of the essence of engineering. One of the important branches of engineering profession is aerospace engineering. Furthermore, aerospace industry achievements play an undeniable role in our lives. Research and development in the aerospace domain have contributed to the progress of some new technologies in the last decades. The purpose of this study is to emphasize the importance of engineering ethics as an essential part of aerospace engineering. Engineering ethics examines professional responsibilities and ethical decision making of engineers. Moreover, codes of ethics help the engineers to apply ethical principles in critical conditions. The poor ethical decision-making of engineers leads to engineering failures which jeopardized human life and the environment. This paper by examining two case studies related to the field of aerospace engineering (Challenger and Columbia disasters) describes the role of the negligence of engineering ethics on the occurrence of engineering disasters.
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English, Lyn D., Donna T. King, Peter Hudson et Les Dawes. « The Aerospace Engineering Challenge ». Teaching Children Mathematics 21, no 2 (septembre 2014) : 122–26. http://dx.doi.org/10.5951/teacchilmath.21.2.0122.

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Integrating Science, Technology, and Engineering in Mathematics authors share ideas and activities that stimulate student interest in the integrated fields of science, technology, engineering, and mathematics (STEM) in K—grade 6 classrooms. This article describes an activity that introduced fourth-grade students to the work of aerospace engineers and to the science, technology, and mathematics principles associated with flight.
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Kuznetsova, Elena, Victoria Kindinova et Oleg Krinetsky. « Numerical methods in the training of aerospace engineers ». MATEC Web of Conferences 362 (2022) : 01013. http://dx.doi.org/10.1051/matecconf/202236201013.

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The paper analyzes the experience of teaching numerical methods in the preparation of engineering students at the Moscow Aviation Institute (National Research University). The necessity of linking the numerical methods studied in the basic course with the topic of a particular specialty is substantiated. The disadvantages of using Ms Excel spreadsheets in the implementation of numerical methods are explained. The necessity of teaching software implementation of numerical methods on a computer is shown. The new American Strategic Computer Initiative is analyzed, as well as the current state of computing power in Russia. The need for the development and implementation of specialized courses in engineering areas for teaching complex methods of numerical analysis is shown. Such learning is recommended to be carried out within the framework of profile physical tasks. It is proposed to acquaint future engineers with the problem of parallelizing numerical algorithms for solving them on a superecomputer. The essence of the engineering approach to the parallelization of numerical algorithms is presented.
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van Velzen, Eric, et Alison Olechowski. « Investigation of Remote Work for Aerospace Systems Engineers ». INCOSE International Symposium 31, no 1 (juillet 2021) : 816–31. http://dx.doi.org/10.1002/j.2334-5837.2021.00872.x.

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Vroman, Gary J. « Sharpening the problem‐solving skills of aerospace engineers ». Aircraft Engineering and Aerospace Technology 71, no 3 (juin 1999) : 255–58. http://dx.doi.org/10.1108/00022669910270754.

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Campos, Luis M. B. C. « On the education of aerospace engineers in Portugal ». Air & ; Space Europe 2, no 1 (janvier 2000) : 105–8. http://dx.doi.org/10.1016/s1290-0958(00)80020-9.

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Wolcott, Barbara. « Renaissance Technologist ». Mechanical Engineering 122, no 08 (1 août 2000) : 46–50. http://dx.doi.org/10.1115/1.2000-aug-1.

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This article observes that in the present competitive world, it is important for an engineer to be adaptable, entrepreneurial, and versatile. According to a private marketing consultant in Cambria, CA, Vicki Clift, ‘Engineers must consider themselves self-employed no matter where they work, or for whom.’ Clift strongly urges engineers to develop cross-industry interests, suggesting that a space engineer can move to medical instruments. Clift recommends that people ‘cross pollinate,’ for instance, by taking ideas from the medical industry that could apply to aerospace. He suggests compiling a list of five or so people and meeting with them on a regular basis. One large contributing factor for the change in employment is the result of an even greater change in the way large contracts are bid today. The state of Oregon recognized the importance of teaming when it established a grant program called Flexible Networks to help businesses form alliances for new markets and opportunities for growth.
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Thèses sur le sujet "Aerospace engineers"

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Conlon, Craig Fertig. « A study of ergonomic risk factors and interventions among aerospace engineers ». Diss., Restricted to subscribing institutions, 2008. http://proquest.umi.com/pqdweb?did=1568065861&sid=1&Fmt=2&clientId=1564&RQT=309&VName=PQD.

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Sales, Hazel Eneida. « Engineering texts : a study of a community of aerospace engineers, their writing practices, and technical proposals ». Thesis, University of Birmingham, 2002. http://etheses.bham.ac.uk//id/eprint/241/.

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This is a report of a six-year study of working and writing practices in an engineering environment. It is an investigation into a distinctive discourse community of design engineers conducted from an ethnographic perspective. It surveys the engineers’ attitudes towards writing and texts, and describes their distinctive writing practices, including collaborative writing. It shows them to have been acculturated into work attitudes, procedures, and a writing style which are at odds with actual demands made of them in the workplace. The engineering-lore about engineers being generally incompetent or indifferent writers is explored and, for the most part, debunked. The texts that design engineers write are identified, and it is shown that product design, the type of work activity that most engages and concerns the engineers, provides a common thread throughout all the documents considered. Particular attention is paid to proposals and executive summaries, since they give rise to specifications and requirements, all of which give most cause for concern to the engineers and the company. It is shown that proposals are ultimately persuasive in intent, in which engineers must convince the Customer of the superiority of their ‘solution’ over the proposal submissions from other companies. Pragmatism and problem-solving underpin the approach taken to proposal documents, the description and analysis of which is intended to be useful to the engineer writers themselves, and intended to reflect their collaborative writing practices. An analytical approach has been devised, based on information content, which is of potential use for diagnostic or evaluative purposes. Findings arising out the analysis suggest that the proposals and executive summaries written by design engineers comprise a selection of Information Components (ICs) drawn from a finite set of thirty-nine ICs. They indicate the existence of four major foci for proposal texts: three information-based, and one metadiscoursal. The results also seem to indicate that proposal writers may be focusing too much on product design in proposals to the detriment of other key information, which also contributes to the overall ‘solution’.
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Bethune, Mary. « Save That Thought| A Case Study of How Knowledge Is Transferred between Baby Boomers and Generation-X Aerospace Engineers ». Thesis, City University of Seattle, 2018. http://pqdtopen.proquest.com/#viewpdf?dispub=10828846.

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The current American workforce is at a crossroads due to the number of Baby Boomers either retiring or on the cusp of retirement. For many organizations, this cohort possesses knowledge and experiences that can be lost if this knowledge is not transferred before their departure from the organization. This ability to share knowledge is increasingly recognized both as a valuable asset for organizations and as a modern-day challenge for leaders. The purpose of this research was to explore the process of organizational knowledge sharing resulting from the Baby Boomers’ retirement. Using case study methodology and a single-stage sampling procedure, twelve participants were recruited to participate, and research questions were designed, to address how two generations of aerospace engineers describe their experiences with knowledge transfer and the strategies used to support such a transfer. Sources of information for this study were face-to-face, semi-structured interviews, organizational documents, and artifacts. Data were analyzed, generating codes and conceptual categories that eventually led to the emergence of the three themes of organizational knowledge transfer, promote knowledge sharing, and tacit and explicit knowledge. An analysis of these three themes resulted in three specific recommendations for action which were: (a) turning tacit knowledge into explicit knowledge, (b) creating knowledge sharing activities, and (c) developing purposeful leadership. Future researchers could explore management views of knowledge sharing and the impact on the organization.

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Ekman, Marcus. « Design Study of a Wing Rudder : Exploring the Possibility to Implement Additive Manufacturing ». Thesis, Luleå tekniska universitet, Institutionen för ekonomi, teknik och samhälle, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-64522.

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Subtractive manufacturing are the most common methods in the aerospace industry to manufacture components. In these parts the buy to fly ratio is low and it needs accurate strengths analyses to static and dynamic loads especially were the different parts relate to each other with fasteners in the assembly work. Additive manufacturing has now been developed to be of such quality that the aerospace industry see the potential to use the technology in their production of parts. It has been possible to make them lighter, stronger and reduce the total amount of parts in an assembly. This mean probably some changes to the stakeholders in the process of their product development. Engineers who are working on the products will need to face the design aspects and restrictions with AM to choose the right component/sub-assemblies to convert to AM parts. This thesis will address the possibility to redesign a wing rudder and to get some knowledge about the engineer’s point of view of AM and how it may affect them. Today there are several aerospace industries adopting AM and get airworthy components to less critical parts as brackets but also parts in the engines as the fuel nozzle in an Airbus (Trimble, 2016). For larger parts, there have also been studies to use AM for example internal galley partition but the result is it will take too long time to print by todays machines. There are several different methods for AM and Powder Bed System is popular in the aerospace industry according to its geometrical correctness to the CAD model (Dordlofva, Lindwall, & Törlind, 2016). Commercial aircrafts industry starts to get harder regulations for their emissions to get lighter planes and less air resistance. AM open up the possibilities to meet these requirements by producing parts which was impossible to produce before. The design process for AM design today are not fully known yet, which leave a lot to imagination. There are general design rules on how to design for AM build but it does not necessary mean the part will be correctly built. There are several cost driven aspects with AM, the most expensive part is the print time but there are different aspects to. For example, CNC machining may be needed after the AM build and add cost for subtractive manufacturing. Interviews with engineer’s groups have been made to conduct their thoughts and knowledge of AM and how it may affect their work. Some uncertainties were mentioned and it was most focused on the process and the reliability of the finished part. The engineers think the design process will be almost the same and only change boundary conditions. To get ideas, a workshop was made with some design guidelines for development of different designs on the wing rudder and to bring positive and negative aspects to the design. An overall cost calculation was made for a few parts and the result shows that it is hard to compete with the design of the wing rudder today. The most important aspects for a success of AM is the print speed, qualified manufacturing processes and CAD software support for the engineers.
Flygindustrin använder sig främst av subtraktiv bearbetning i sin framställning av de olika komponenterna till ett flygplan. Det blir då ofta en väldigt låg grad av materialutnyttjande, endast några procent återstår av det inköpta utgångsmaterialet. Till det tillkommer monteringsarbete och noggranna hållfasthetsanalyser, både statisk och utmatningshållfasthet av sammanbyggda skarvar där fästelement är en del. Den additiva tillverkningen har nu utvecklats och visat sig inneha kvalitéer för att klara kraven som ställs i flygindustrin. Det kan göra detaljerna lättare, starkare och minska antalet komponenter i monteringsarbetet. Det kan innebära en hel del förändringar för olika intressenter som får börja tänka annorlunda. Ingenjörer som arbetar med produktframtagning kommer att ställas inför utmaningen att applicera denna teknik på lämpliga delar/delkonstruktioner. Detta examensarbetet undersöker möjligheten att designa ett vingroder till ett flygplan och bilda en uppfattning om ingenjörernas förtroende för additiv tillverkning samt hur det kommer påverka dem. Det finns idag flera flygindustrier som har påbörjat att ta fram flygvärdiga komponenter, framförallt mindre kritiska fästelement men även en del artiklar i motorer så som bränslemunstycke hos Airbus (Trimble, 2016). De har analyserat möjligheten att använda additiv tillverkning på större artiklar såsom inre kabinstruktur men har kommit fram till att det tar för lång tid att tillverka med dagens maskiner. Det finns flertalet olika additiva tillverkningsmetoder men den som står ut är pulverbäddskrivaren då den har en bättre geometrisk korrekthet gentemot CAD modellen (Dordlofva, Lindwall, & Törlind, 2016). Nya reglementen för utsläpp i den komersiella flygindustrin pressar företagen att bygga bättre flygplan som är lättare och därmed får mindre luftmotstånd. Designprocessen för additiv tillverkning är inte given då det inte finns några givna processer som täcker hela processen. Det finns generella design-riktlinjer i vad de olika maskinerna klarar av att bygga, men samtidigt är det ingen garanti att genom att följa dessa riktlinjer skapa en fungerande design. Det finns flera olika kostnadsdrivande aspekter med additiv tillverkning. Det som mest driver kostnaden idag är den låga skrivarhastigheten. Andra kosnadsdrivare är om det tillkommer efterarbete för att uppfylla toleranser eller få en korrekt / plan sammanfogningsyta. Arbetet har utförts med intervjuer av ingenjörsgrupper för att skapa en uppfatting om deras syn på additiv tillverkning och hur det skulle ändra deras arbete. En viss osäkerhet förekom men det berodde framförallt på osäkerheten för säkring av processen, dvs tillverkningsprocessen och att kunna vara säker på att detaljen håller måttet. De ansåg att designprocessen inte skulle förändras så mycket, utan bara att randvillkoren skulle ändras. Utifrån workshops och designriktlinjer har koncept tagits fram och utvärderats med för och nackdelar. En översiktlig kostnadskalkyl har gjorts som visar på att det blir svårt att designa roder som en större enhet för additiv tillvekning som är ekonomiskt jämförbart med dagens tillverkingsmetoder. De viktigaste framgångsfaktorerna för additiv tillverkning är ökad skrivarhastighet, kvalificering av tillverkningsprocesserna och CAD stöd för ingenjörerna.
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Collins, Michelle Louise. « Surface treatment for new engineered aerospace systems ». Thesis, University of Manchester, 2012. https://www.research.manchester.ac.uk/portal/en/theses/surface-treatment-for-new-engineered-aerospace-systems(79c66e05-aaea-4dc3-bb8f-4d281ea1ea78).html.

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During this EngD project, two pigmented, anti-corrosion polymer/sol-gel hybrid coatings were developed with the aim of producing an eco-friendly alternative to conventional, toxic hexavalent chromate conversion and anodized anti-corrosion alloy treatments for the aircraft manufacturer; Airbus S.A.S. The polymer/sol-gel hybrid coatings were then tested and validated as anti-corrosion coatings on the AA2024-T3 aluminium aerospace alloy and in certain cases, their performance was compared against that of the hexavalent chromate benchmark (Alocrom 1200). The mechanisms of corrosion inhibition exhibited by the coatings were also studied in depth. The polymer/sol-gel hybrid coatings that were developed in this project are silane based and the first, designated as B2, has polyester-methacrylic functionality and the second, designated as CA/MM, has polyester-amide functionality. Certain inhibitor compounds which were incorporated in the polymer/sol-gel hybrid coatings were chosen by the split-cell technique. The microstructure and elemental compositions of the polymer/sol-gel hybrid coatings and of the AA2024-T3 aluminium alloy were determined by Scanning Electron Microscopy - Energy Dispersive X-ray Spectroscopic (SEM-EDS) analysis of the specimens. The anti-corrosion performance and the corrosion protection mechanisms of the polymer/sol-gel hybrid coatings were determined by salt-water and electrochemical testing of the coated alloy specimens. The thermal resistance of the polymer/sol-gel hybrid coatings was ascertained by thermogravimetric analysis (TGA) of the coatings. The polymer/sol-gel hybrid coatings were also analysed by Fourier Transform Infrared (FTIR), Micro-Raman and X-ray Photoelectron (XPS) spectroscopic techniques to determine whether the desired polymer and silane coating networks formed during coating processing. Anti-corrosion performance test results revealed that both polymer/sol-gel hybrid coatings are self-healing due to their ability to implement a precipitation mechanism of corrosion inhibition. Analysis of the polymer/sol-gel hybrid coatings by X-ray Diffraction (XRD) and X-ray Fluorescence (XRF) after salt-water exposure suggested that the B2 coating precipitated the compound tungsten pyrophosphate, W(P2O7), within defects and that the CA/MM coating precipitated the compound iron carbide, Fe2C, within defects. However, anti-corrosion test results also shown that the anti-corrosion performance of the polymer/sol-gel hybrid coatings does not satisfy aerospace industry requirements. Therefore, it can be concluded that although the achievements of this project have not enabled Airbus to eliminate toxic chromium (VI) species from their operations, further optimisation of the polymer/sol-gel hybrid coatings developed during this project could potentially lead to a solution being found.
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Ling, Jack C. L. « Compressors for miniature unmanned aerospace propulsion systems ». Phd thesis, School of Aerospace, Mechanical and Mechatronic Engineering, 2009. http://hdl.handle.net/2123/6430.

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Korak, Ghosh. « Model predictive control for civil aerospace gas turbine engines ». Thesis, University of Sheffield, 2013. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.595827.

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Kiker, Adam Paul. « Experimental Investigations of Mini-Pulsejet Engines ». NCSU, 2005. http://www.lib.ncsu.edu/theses/available/etd-08112005-134914/.

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An experimental 8 cm pulsejet was developed using scaling laws from research on both 50 and 15 cm pulsejets. The 8 cm jet operates in three different inlet configurations?conventional, perpendicular, and rearward. The rearward configuration features inlets facing in the opposite direction of the flight path and develops the maximum net thrust. Using a high frequency pressure transducer, the operational frequency of the pulsejet was obtained by monitoring the combustion chamber pressure. It was found that in the rearward configuration, the operational frequency of the jet decreases with increasing inlet length. In addition, the combustion chamber peak pressure rise per cycle increases significantly if the exhaust diameter is reduced. Using information from the 8 cm pulsejet, a 4.5 cm pulsejet was developed and is operational.
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OVERMAN, NICHOLAS. « FLAMELESS COMBUSTION APPLICATION FOR GAS TURBINE ENGINES IN THE AEROSPACE INDUSTRY ». University of Cincinnati / OhioLINK, 2006. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1163776616.

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Schoen, Michael Alexander. « Experimental Investigations in 15 Centimeter Class Pulsejet Engines ». NCSU, 2005. http://www.lib.ncsu.edu/theses/available/etd-08082005-095911/.

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Testing is performed on the 15 centimeter class pulsejet engine in order to develop, study, and explore the operational characteristics. Valved and valveless operation, hydrogen and propane fuels, various fuel injection methods, and a range of geometric configurations are investigated for operational feasibility. The scaling capabilities of a valveless 15 centimeter class pulsejet of conventional design are studied by methodically varying inlet length, exit length, exit geometry, and inlet area to combustor area ratio (Ai/Ac). Engine performance is defined by measuring chamber pressure, internal gas temperatures, time-resolved thrust, operational frequency, and fuel flow rate. The scaling capability is characterized by the success of self-sustained combustion for each corresponding geometric configuration. Tail pipe length is found to be a function of valveless inlet length and may be further minimized by the addition of a diverging exit nozzle. Chemical kinetic times and Ai/Ac prove to be the two prominent controlling parameters in determining scaling behavior.
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Livres sur le sujet "Aerospace engineers"

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American Institute of Aeronautics and Astronautics., dir. AIAA aerospace design engineers guide. 3e éd. Washington, DC : American Institute of Aeronautics and Astronautics, 1993.

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American Institute of Aeronautics and Astronautics. AIAA aerospace design engineers guide. 6e éd. Reston, VA : American Institute of Aeronautics and Astronautics, 2012.

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American Institute of Aeronautics and Astronautics., dir. AIAA aerospace design engineers guide. 4e éd. Reston, VA : American Institute of Aeronautics and Astronautics, 1998.

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American Institute of Aeronautics and Astronautics., dir. AIAA aerospace design engineers guide. 5e éd. Reston, VA : AIAA, 2003.

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Research, Institute for Career. Careers in aerospace engineering : Aeronautics - astronautics. [Chicago, Ill.] : Institute for Career Research, 2003.

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Habibie, B. J. Habibie, from Pare-Pare via Aachen and other articles. Sous la direction de Makka A. Makmur 1945-. 3e éd. [Jakarta] : Swakarya, 1989.

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United States. Civil Air Patrol. Aerospace, the flight of discovery. Maxwell AFB, Ala : National Headquarters, Civil Air Patrol, 1992.

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Yuanguang, Shi, dir. Zhongguo hang kong shi ye xian qu Wang Shizhuo. Beijing Shi : Hang kong gong ye chu ban she, 2007.

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Mayūra, Bi Es. Bi. Raṅganāyakaṃṃa : Prathama mahiḷā ēronāṭikal iñjiniyar. Beṅgaḷūru : Navakarnāṭaka Prakāśana, 2010.

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Volkov, L. I. Zhiznʹ moi︠a︡--. Moskva : Izd-vo "SIP RIA", 2000.

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Chapitres de livres sur le sujet "Aerospace engineers"

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Guruprasad, R., Khaiser Nikam et P. Marimuthu. « Use Patterns of Aerospace E-Indexing, Abstracting and Citation Services : A Research Study of Aerospace Scientists and Engineers of Bangalore ». Dans The Outreach of Digital Libraries : A Globalized Resource Network, 67–72. Berlin, Heidelberg : Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-34752-8_9.

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Middleton, James A. « Simple Linear Regression ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 271–314. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-10.

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Middleton, James A. « Introduction to Probability ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 85–110. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-4.

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Middleton, James A. « Data Reduction : Principal Components Analysis ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 515–50. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-16.

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Middleton, James A. « Sampling Distribution of the Proportion ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 163–92. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-7.

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Middleton, James A. « Dealing with Variation ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 15–54. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-2.

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Middleton, James A. « The Ten Building Blocks of Experimental Design ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 143–62. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-6.

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Middleton, James A. « The Bootstrap ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 481–514. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-15.

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Middleton, James A. « Types of Data ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 55–84. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-3.

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Middleton, James A. « Hypothesis Testing Using 1-Sample Statistics ». Dans Experimental Statistics and Data Analysis for Mechanical and Aerospace Engineers, 193–232. Boca Raton : Chapman and Hall/CRC, 2021. http://dx.doi.org/10.1201/9781003094227-8.

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Actes de conférences sur le sujet "Aerospace engineers"

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Peris, Rafael Masot, Miguel Alcaniz Fillol et Luis Gil Sanchez. « Discovering electronics to aerospace engineers ». Dans 2014 XI Tecnologias Aplicadas a la Ensenanza de la Electronica (Technologies Applied to Electronics Teaching) (TAEE). IEEE, 2014. http://dx.doi.org/10.1109/taee.2014.6900139.

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Komerath, Narayanan, Marilyn Smith, Brian German et Dolores Krausche. « Helping Aerospace Engineers Innovate Across Disciplines ». Dans 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-887.

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Gonzalez Lozano, Alma Arcelia. « Educating Aerospace Engineers for Industry 4.0 ». Dans International Conference on Advanced Research in Education. Acavent, 2019. http://dx.doi.org/10.33422/educationconf.2019.03.130.

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Driesman, Andrew S. « Developing Young Space System Engineers ». Dans 2011 IEEE Aerospace Conference. IEEE, 2011. http://dx.doi.org/10.1109/aero.2011.5747665.

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Fidel, Raya, et Efthimis N. Efthimiadis. « Web searching behavior of aerospace engineers (poster abstract) ». Dans the 22nd annual international ACM SIGIR conference. New York, New York, USA : ACM Press, 1999. http://dx.doi.org/10.1145/312624.312751.

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Mignot, J. « Helping engineers and scientists avoid PowerPoint phluff ». Dans 2005 IEEE Aerospace Conference. IEEE, 2005. http://dx.doi.org/10.1109/aero.2005.1559758.

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RODMAN, LAURA, et DAVID NIXON. « An intelligent technology transfer system for development engineers ». Dans 31st Aerospace Sciences Meeting. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-327.

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Williams, C. R., et A. M. Reyes. « NASA's system behind the system : Developing systems engineers ». Dans 2012 IEEE Aerospace Conference. IEEE, 2012. http://dx.doi.org/10.1109/aero.2012.6187445.

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de Maine, P. A. D., et M. M. de Maine. « Computer Aids For Scientists And Engineers ». Dans SPIE 1989 Technical Symposium on Aerospace Sensing, sous la direction de Mohan M. Trivedi. SPIE, 1989. http://dx.doi.org/10.1117/12.969271.

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Derro, Mary Ellen, et Christine R. Williams. « Behavioral competencies of highly regarded systems engineers at NASA ». Dans 2009 IEEE Aerospace conference. IEEE, 2009. http://dx.doi.org/10.1109/aero.2009.4839712.

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Rapports d'organisations sur le sujet "Aerospace engineers"

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Barclay, Rebecca O., Thomas E. Pinelli, David Elazar et John M. Kennedy. NASA/DoD Aerospace Knowledge Diffusion Research Project, Paper Fourteen : An Analysis of the Technical Communications Practices Reported by Israeli and U.S. Aerospace Engineers and Scientists. Fort Belvoir, VA : Defense Technical Information Center, novembre 1991. http://dx.doi.org/10.21236/ada252564.

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Barkan, Terrance. The Role of Graphene in Achieving e-Mobility in Aerospace Applications. 400 Commonwealth Drive, Warrendale, PA, United States : SAE International, décembre 2022. http://dx.doi.org/10.4271/epr2022030.

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<div class="section abstract"><div class="htmlview paragraph">Advanced two-dimensional (2D) materials discovered in the last two decades are now being produced at scale and are contributing to a wide range of performance enhancements in engineering applications. The most well-known of these novel materials is graphene, a nearly transparent nanomaterial comprising a single layer of bonded carbon atoms. In relative terms, it has the highest level of heat and electrical conductivity, protects against ultraviolet rays, and is strongest material ever measured. These properties have made graphene an attractive potential material for a variety of applications, particularly for transportation related uses, and especially for aerospace engineering. </div><div class="htmlview paragraph"><b>The Role of Graphene in Achieving e-Mobility in Aerospace Applications</b> reviews the current state of graphene-related aerospace applications and identifies the technological challenges facing engineers that look to benefit from graphene’s attractive properties.</div><div class="htmlview paragraph"><a href="https://www.sae.org/publications/edge-research-reports" target="_blank">Click here to access the full SAE EDGE</a><sup>TM</sup><a href="https://www.sae.org/publications/edge-research-reports" target="_blank"> Research Report portfolio.</a></div></div>
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Pinelli, Thomas E., Rebecca O. Barclay, Myron Glassman et Walter E. Oliu. NASA/DoD Aerospace Knowledge Diffusion Research Project, Paper One : The Value of Scientific and Technical Information (STI), Its Relationship to Research and Development (R and D), and Its Use by U.S. Aerospace Engineers and Scientists. Fort Belvoir, VA : Defense Technical Information Center, janvier 1990. http://dx.doi.org/10.21236/ada252565.

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Roye, Thorsten. The Right Level of Automation for Industry 4.0. SAE International, mai 2022. http://dx.doi.org/10.4271/epr2022013.

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In its entirety, automation is part of an integrated, multi-disciplinary product development process including the design, process, production, logistics, and systems approach—it depends on all these areas, but it also influences them as well. Automation in aerospace manufacturing is present throughout the entire supply chain, from elementary part manufacturing at suppliers up to final assembly, and a clear understanding of all the benefits (and drawbacks) of automation would help designers and engineers select the right designs for and levels of automation. The Right Level of Automation Within Industry 4.0 examines all impacts of automation that should be known by designers, manufacturers, and companies before investments in automation-related decisions are made—regardless of the which industry they work in. The process and the set of criteria discussed in this report will help decision makers select the right level of automation.
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Eley, T. C., John Leslie King, Kalle Lyytinen et Jeffrey Nickerson. Implications of Off-road Automation for On-road Automated Driving Systems. 400 Commonwealth Drive, Warrendale, PA, United States : SAE International, décembre 2023. http://dx.doi.org/10.4271/epr2023029.

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<div class="section abstract"><div class="htmlview paragraph">Automated vehicles, in the form we see today, started off-road. Ideas, technologies, and engineers came from agriculture, aerospace, and other off-road domains. While there are cases when only on-road experience will provide the necessary learning to advance automated driving systems, there is much relevant activity in off-road domains that receives less attention.</div><div class="htmlview paragraph"><b>Implications of Off-road Automation for On-road Automated Driving Systems</b> argues that one way to accelerate on-road ADS development is to look at similar experiences off-road. There are plenty of people who see this connection, but there is no formalized system for exchanging knowledge.</div><div class="htmlview paragraph"><a href="https://www.sae.org/publications/edge-research-reports" target="_blank">Click here to access the full SAE EDGE</a><sup>TM</sup><a href="https://www.sae.org/publications/edge-research-reports" target="_blank"> Research Report portfolio.</a></div></div>
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Qian, Yuping, Yangjun Zhang et WEILIN ZHUGE. Key Technology Challenges of Electric Ducted Fan Propulsion Systems for eVTOL. 400 Commonwealth Drive, Warrendale, PA, United States : SAE International, novembre 2023. http://dx.doi.org/10.4271/epr2023027.

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<div class="section abstract"><div class="htmlview paragraph">Electrical vertical takeoff and landing (eVTOL) vehicles for urban air mobility (UAM) are garnering increased attention from both the automotive and aerospace industries, with use cases ranging from individual transportation, public service, cargo delivery, and more. Distributed electric propulsion systems are their main technical feature; they determine vehicle size and propulsion efficiency and provide distributed thrust to achieve attitude control. Considering the intended role of eVTOL vehicles, ducted-fan systems are ideal choice for the propulsor, as the duct provides a physical barrier between the rotating blades and the human, especially during the take-off and landing phases.</div><div class="htmlview paragraph"><b>Key Technology Challenges of Electric Ducted Fan Propulsion Systems for eVTOL</b> introduces the main bottlenecks and key enablers of ducted-fan propulsion systems for eVTOL applications. Based on the introduction and discussion of these important issues, this report will help eVTOL engineers understand the key technical issues and inspire them to develop the ideal solutions that will enable eVTOL vehicle deployment for UAM operations.</div><div class="htmlview paragraph"><a href="https://www.sae.org/publications/edge-research-reports" target="_blank">Click here to access the full SAE EDGE</a><sup>TM</sup><a href="https://www.sae.org/publications/edge-research-reports" target="_blank"> Research Report portfolio.</a></div></div>
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