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Journal articles on the topic 'Aeronautic engineering'

Author: Grafiati

Published: 30 May 2022

Last updated: 31 July 2025

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1

Zhao, Yan Ling, Chun Yu Che, Hong Bo Wang, Zi Yan Yun, and Guan Hong Xu. "Application of Knowledge Based Engineering in Aeronautics Mold Parts Parametric Design." Advanced Materials Research 765-767 (September 2013): 47–50. http://dx.doi.org/10.4028/www.scientific.net/amr.765-767.47.

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In the process of designing aeronautic composite mold parts, previous designing knowledge and expertise cant be well used, the cycle of parts modeling is long and its production efficiency is low. According to the classification and characteristics of aeronautic mold parts and the knowledge engineering technology, based on the fusion module in UG6.0, we establish its repository by the knowledge acquisition, knowledge representation and knowledge reasoning of aeronautic mold parts. With the UG secondary development tools, UG/Open Menuscript and UG/Open Uistyler, we develop user menu and paramet

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Qian, Hao Han, Yuan Ming Ding, and Jia Cheng. "Research in Thermo-Physical Property Testing System of Aeronautic PMMA Based on Temperature-Pressure Parameters." Advanced Materials Research 647 (January 2013): 828–32. http://dx.doi.org/10.4028/www.scientific.net/amr.647.828.

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Because of the differences in physical properties, the aeronautic PMMA for porthole may easily craze, crack and even explode in flight. In this paper, the operating conditions for porthole were analyzed and testing methods of PMMA’s thermo-physical properties were studied considering the two main factors, temperature and pressure, which affects porthole’s operating life. At last a thermo-physical property testing system of aeronautic PMMA based on temperature-pressure parameters was designed. This device could preferably simulate the operating conditions and conduct continuous fatigue test for

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Brito-Acuña, Guillermo. "Aeronautic maturity cybersecurity: a framework." DYNA 90, no. 227 (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 th

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Boulos, Federico, Georg Frederik Riemschneider, and Stefano Caizzone. "3D Phased Array Enabling Extended Field of View in Mobile Satcom Applications." Electronics 13, no. 2 (2024): 310. http://dx.doi.org/10.3390/electronics13020310.

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Satellite communication (satcom) is experiencing increased interest to cover the connectivity gaps of terrestrial networks. To ensure high performance and throughput for the user—and even more so in Communications-On-The-Move(COTM) systems, e.g., in aeronautics—steerable antennas such as phased arrays are required to adjust the beam so as to follow the satellite’s trajectory. The mutual movement of terminals and satellite in COTM systems calls for a broad Field of View (FoV) and, hence, poses a challenge to common planar systems. For improving the FoV, common solutions require ad hoc designs,

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Deque, R., and P. Bachelier. "Future aeronautic environment FMS/ATC/Pilot." Aeronautical Journal 94, no. 940 (1990): 341–43. http://dx.doi.org/10.1017/s0001924000023290.

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Abstract The scope of the air-ground data links, which have been developed over the last ten years to meet the airlines' operational requirements, will be extended in future years.Air traffic control is one of the fields which will certainly make extensive use of this type of link. Indeed, it appears to be necessary to deal with the problem of traffic saturation globally by taking account of the navigation capabilities of modern aircraft as regards precision and the considerable automated flight/ground exchange possibilities which will be provided by future telecommunication networks.The conte

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Tommasino, Domenico, Federico Moro, Bruno Bernay, Thibault De Lumley Woodyear, Enrique de Pablo Corona, and Alberto Doria. "Vibration Energy Harvesting by Means of Piezoelectric Patches: Application to Aircrafts." Sensors 22, no. 1 (2022): 363. http://dx.doi.org/10.3390/s22010363.

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Vibration energy harvesters in industrial applications usually take the form of cantilever oscillators covered by a layer of piezoelectric material and exploit the resonance phenomenon to improve the generated power. In many aeronautical applications, the installation of cantilever harvesters is not possible owing to the lack of room and/or safety and durability requirements. In these cases, strain piezoelectric harvesters can be adopted, which directly exploit the strain of a vibrating aeronautic component. In this research, a mathematical model of a vibrating slat is developed with the modal

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Füchter, Simone Keller, Mário Sérgio Schlichting, and George Salazar. "Aeronautic pilot training and augmented reality." ACTA IMEKO 10, no. 3 (2021): 66. http://dx.doi.org/10.21014/acta_imeko.v10i3.1038.

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<p class="Abstract">A pre-flight checklist requires in-depth technical knowledge of the aircraft and its dashboard, avionics, instruments, functions, and cabin layout. The student in training to be a pilot or advanced pilot, to obtain an updated certification, must know very thoroughly each instrument and its position on the flight panel. Every second spent searching for the location of an instrument, switch or indicator can waste time, resulting in a poor start-up procedure and possibly a safety hazard. The objective of this research was to obtain preliminary data to determine if the us

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González Ojeda, Itzel De Jesús, Pablo Bengoa, Aitor Ibarguren, et al. "Robot Coordination: Aeronautic Use Cases Handling Large Parts." Designs 6, no. 6 (2022): 116. http://dx.doi.org/10.3390/designs6060116.

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The coordination of two collaborative robots to handle and hold huge parts is the main topic of this research. This study shows how flexible systems may accommodate large-volume components while situating components with a displacement precision between robots of no more than 10 mm into the parts, with the assistance of a single operator. The robots must be able to keep the parts in place while coordinating their movements to handle the parts and reducing external stressors. This paper suggests using collaborative robots to integrate flexible tools for adaptability to various elements in order

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9

Xia, Qianshan, Zhichun Zhang, Yanju Liu, and Jinsong Leng. "Buckypaper and its composites for aeronautic applications." Composites Part B: Engineering 199 (October 2020): 108231. http://dx.doi.org/10.1016/j.compositesb.2020.108231.

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10

Vietri, U., L. Guadagno, M. Raimondo, L. Vertuccio, and K. Lafdi. "Nanofilled epoxy adhesive for structural aeronautic materials." Composites Part B: Engineering 61 (May 2014): 73–83. http://dx.doi.org/10.1016/j.compositesb.2014.01.032.

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11

Geyer, Fabien, and Georg Carle. "Network engineering for real-time networks: comparison of automotive and aeronautic industries approaches." IEEE Communications Magazine 54, no. 2 (2016): 106–12. http://dx.doi.org/10.1109/mcom.2016.7402269.

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12

Jäckel, R., G. L. Gutiérrez Urueta, F. Tapia Rodríguez, and C. Monreal Jiménez. "Numerical and experimental characterisation of an aeronautic Pitot probe." Aeronautical Journal 123, no. 1264 (2019): 890–911. http://dx.doi.org/10.1017/aer.2019.33.

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AbstractAeronautic Pitot probes (PPs) are extremely important for airspeed and altitude measurements in aviation. Failure of the instrument due to clogging caused by ice formation can lead to dangerous situations. In this work, a commercial aeronautic PP was characterised experimentally regarding its inner composition, material properties and its thermal performance in a climatic wind tunnel. Performance runs were taken out in order to analyse the thermal response of the PP under various operating conditions with a particular emphasis on the cooling process in the case of a heating element fai

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Dal Santo, Philippe, Guénaël Germain, Serge Boude, and Eliane Giraud. "Cold forming by stretching of aeronautic sheet metal parts." International Journal of Computer Integrated Manufacturing 27, no. 2 (2013): 129–38. http://dx.doi.org/10.1080/0951192x.2013.800641.

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14

Loukopoulos, Andreas, Christos Vasilios Katsiropoulos, and Spiros G. Pantelakis. "Carbon footprint and financial evaluation of an aeronautic component production using different manufacturing processes." International Journal of Structural Integrity 10, no. 3 (2019): 425–35. http://dx.doi.org/10.1108/ijsi-07-2018-0043.

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Purpose The purpose of this paper is to quantify the environmental footprint and cost and thus compare different manufacturing scenarios associated with the production of aeronautical structural components. Design/methodology/approach A representative helicopter canopy, i.e., canopy of the EUROCOPTER EC Twin Star helicopter described in Pantelakis et al. (2009), has been considered for the carbon footprint (life cycle energy and climate change impact analysis) along with the life cycle costing analysis. Four scenarios – combinations of different manufacturing technologies (autoclave and resin

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15

Salah, Mostefa, Farouk B. Boukhoulda, Mohamed Nouari, and Kouider Bendine. "Temperature Variation Effect on the Active Vibration Control of Smart Composite Beam." Acta Mechanica et Automatica 14, no. 3 (2020): 166–74. http://dx.doi.org/10.2478/ama-2020-0024.

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Abstract Due to their impressive capacity of sensing and actuating, piezoelectric materials have been widely merged in different industrial fields, especially aeronautic and aerospace area. However, in the aeronautic industry, the structures are operating under critical environmental loads such as high and very low temperature, which made the investigation of the effect of thermal forces on the piezoelectric structures indispensable to reach the high functionality and performance. The present paper focuses on the effect of thermal loads on the active vibration control (AVC) of structures like

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Irez, Alaeddin Burak, Emin Bayraktar, and Ibrahim Miskioglu. "Fracture Toughness Analysis of Epoxy-Recycled Rubber-Based Composite Reinforced with Graphene Nanoplatelets for Structural Applications in Automotive and Aeronautics." Polymers 12, no. 2 (2020): 448. http://dx.doi.org/10.3390/polym12020448.

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This study proposes a new design of lightweight and cost-efficient composite materials for the aeronautic industry utilizing recycled fresh scrap rubber, epoxy resin, and graphene nanoplatelets (GnPs). After manufacturing the composites, their bending strength and fracture characteristics were investigated by three-point bending (3PB) tests. Halpin–Tsai homogenization adapted to composites containing GnPs was used to estimate the moduli of the composites, and satisfactory agreement with the 3PB test results was observed. In addition, 3PB tests were simulated by finite element method incorporat

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Dyantyi, Noluntu, Adrian Parsons, Cordellia Sita, and Sivakumar Pasupathi. "PEMFC for aeronautic applications: A review on the durability aspects." Open Engineering 7, no. 1 (2017): 287–302. http://dx.doi.org/10.1515/eng-2017-0035.

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AbstractProton exchange membrane fuel cells (PEMFC) not only offer more efficient electrical energy conversion, relative to on-ground/backup turbines but generate by-products useful in aircraft such as heat for ice prevention, deoxygenated air for fire retardation and drinkable water for use on-board. Consequently, several projects (e.g. DLR-H2 Antares and RAPID2000) have successfully tested PEMFC-powered auxiliary unit (APU) for manned/unmanned aircraft. Despite the progress from flying PEMFC-powered small aircraft with 20 kW power output as high as 1 000 m at 100 km/h to 33 kW at 2 558 m, 17

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18

Liu, Jin Hui, Yan Yan Guo, and Guang Bin Bu. "Research on Cutting Force of Milling Aviation Aluminum Alloy." Advanced Materials Research 299-300 (July 2011): 1032–35. http://dx.doi.org/10.4028/www.scientific.net/amr.299-300.1032.

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In this paper, a milling test for aeronautic aluminum alloy 7050-T7451 was carried out and the cutting force was measured. The least square method was used to make a regression analysis on testing data and the experiential formula for milling was established. The influencing laws of cutting parameters on cutting force were educed, which can offer an important reference for optimizing cutting parameters.

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19

Langat, Rogers K., Emmanuel De Luycker, Arthur Cantarel, and Micky Rakotondrabe. "Integration Technology with Thin Films Co-Fabricated in Laminated Composite Structures for Defect Detection and Damage Monitoring." Micromachines 15, no. 2 (2024): 274. http://dx.doi.org/10.3390/mi15020274.

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Despite the well-established nature of non-destructive testing (NDT) technologies, autonomous monitoring systems are still in high demand. The solution lies in harnessing the potential of intelligent structures, particularly in industries like aeronautics. Substantial downtime occurs due to routine maintenance, leading to lost revenue when aircraft are grounded for inspection and repairs. This article explores an innovative approach using intelligent materials to enhance condition-based maintenance, ultimately cutting life-cycle costs. The study emphasizes a paradigm shift toward structural he

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20

Citarella, R. "MSD crack propagation by DBEM on a repaired aeronautic panel." Advances in Engineering Software 42, no. 10 (2011): 887–901. http://dx.doi.org/10.1016/j.advengsoft.2011.02.014.

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21

Riveiro, A., F. Quintero, F. Lusquiños, J. Pou, and M. Pérez-Amor. "Laser cutting of 2024-T3 aeronautic aluminum alloy." Journal of Laser Applications 20, no. 4 (2008): 230–35. http://dx.doi.org/10.2351/1.2995769.

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22

Guo, Bi Xin, Jian Xia Li, and Yun Kui Gao. "Study on the Spraying Technique of Ultra-High Strength Parts Made by 30CrMnSiNi2A Steel." Advanced Materials Research 154-155 (October 2010): 1110–13. http://dx.doi.org/10.4028/www.scientific.net/amr.154-155.1110.

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The oxy-acetylene flame spraying is a new kind of the spraying technology which is developed in recent years. The ultra-high strength is the pivotal structural material in aviation. The oxy-acetylene flame spraying method that is used to mend aeronautic parts made by ultra-high strength steel is studied in this article. The spraying technology of ultra-high strength parts made by 30CrMnSiNi2A steel is introduced.

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23

Keshkar, Miziya, Raja Muthalagu, Abdul Rajak, and Libin K. Mathew. "GAE and OBE Enhanced Interference Mitigation Techniques in LDACS." Aerospace 9, no. 1 (2022): 45. http://dx.doi.org/10.3390/aerospace9010045.

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Interference mitigation in L-band digital aeronautic communication systems from legacy users is vital due to stringent safety requirements and steady-state increase in air traffic. This paper proposes an L-band digital aeronautic communication systems receiver prototype that employs nonlinear operations to reduce the interference from the prime interference contributor distance measuring equipment. The knowledge of genie-aided estimator and optimum Bayesian estimator is utilized to propose improved and low complexity nonlinear devices, such as a genie-aided estimator enhanced pulse peak attenu

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24

Ndongo Diaw, El Hadji, Severine Le Roy, Gilbert Teyssedre, and Eddy Aubert. "Current Measurements in High Performance Polymers Used in Aeronautic Cables." IEEE Transactions on Dielectrics and Electrical Insulation 27, no. 6 (2020): 2195–202. http://dx.doi.org/10.1109/tdei.2020.008796.

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25

Opran, Constantin, Diana Cotoros, Nadinne Roman, Angela Repanovici, and Roxana Miclaus. "Research Regarding the Impact Behaviour of Some Polymeric Bio-composite Products for Orthopedic Use." Materiale Plastice 54, no. 3 (2017): 438–42. http://dx.doi.org/10.37358/mp.17.3.4867.

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Polymeric bio-composites have special characteristics and use in various areas such as: automotive, aviation and aeronautic industries, civil engineering and for medical devices manufacturing. This paper presents the evaluation of impact behaviour of some types of materials suitable for orthopaedic use. As composites behave very differently at different rates of loading, static strength tests cannot be used to predict impact behaviour in the perspective of prosthetic medical devices study and manufacture. The used testing machine is Instron Dynatup Impact System with Data Acquisition and Contr

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26

Corrado, Andrea, and Wilma Polini. "Assembly design in aeronautic field: From assembly jigs to tolerance analysis." Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture 231, no. 14 (2016): 2652–63. http://dx.doi.org/10.1177/0954405416635033.

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Tolerance analysis represents the best way to solve assembly problems in order to improve the quality and to reduce the costs. It is a critical step to design and to build a product such as an aircraft and its importance is grown up in the past years. This work presents a method for the tolerance analysis of an assembly involving free-form surfaces with large dimensions. The assembly is a tail beam, a structural component of an aircraft that is constituted by five parts of large dimensions. The influence of the tolerances applied to the five components of the tail beam on the value of the gap

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27

Ridel, M., P. Savi, and J. P. Parmantier. "Characterization of Complex Aeronautic Harness—Numerical and Experimental Validations." Electromagnetics 33, no. 5 (2013): 341–52. http://dx.doi.org/10.1080/02726343.2013.792718.

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28

Charruau, S., F. Guerin, J. Hernández Dominguez, and J. Berthon. "Reliability estimation of aeronautic component by accelerated tests." Microelectronics Reliability 46, no. 9-11 (2006): 1451–57. http://dx.doi.org/10.1016/j.microrel.2006.07.009.

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29

Dai, Yu, Xi Chen, Duan Yang, Lanjin Xu, and Xiang Zhu. "Performance of a New Aeronautic Oil-Guiding Splash Lubrication System." Lubricants 10, no. 6 (2022): 130. http://dx.doi.org/10.3390/lubricants10060130.

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Among ever-increasing demands for low power consumption, low weight, and compact reducer systems, an oil-guiding splash lubrication method integrating the oil-guiding cylinder and pipes is suggested to be more suitable for light helicopters, instead of conventional splash or oil jet lubrication. Aiming at improving the lubrication and cooling performance of this special lubrication method, this paper introduces an oil-guiding channel to increase oil quantity reaching the driving gear, bearings, and spline. Firstly, the lubrication and cooling effect of the oil-guiding channel in the main gearb

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Yu, Wentao, Shijun Liu, Wenbo Xu, and Dongfei Wang. "Modal Analysis of Aeronautic Spiral Bevel Gear in the Temperature Field." Journal of Sensors 2022 (September 13, 2022): 1–13. http://dx.doi.org/10.1155/2022/1707808.

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The temperature of the bevel gear tooth surface will increase greatly because of its special structure. Modal is the characteristic of reaction structure. In order to design and manufacture higher quality aerial bevel gears, it is necessary to study the modal of aerial bevel gears under the action of the temperature field. Firstly, a temperature field calculation model is established according to heat transfer theory. Then, based on the traditional linear modal theory, the modal analysis model under the influence of temperature was established considering the influence of rotational speed and

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Lin, Guo Min, Li Xia Peng, and Yu Feng Zhao. "Analysis of Latest Application Movement of Laser Surface Heat Treatment Technologies." Advanced Materials Research 291-294 (July 2011): 2199–204. http://dx.doi.org/10.4028/www.scientific.net/amr.291-294.2199.

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The application of two representative laser surface treatments technologies which are laser shock processing technology and laser coating treatment technology are described. The application of laser shock processing in the fields of aero engine disc, wing panel formation, structural welding and strengthening, nuclear power station pressure container strengthening etc and also evaluates the effects are analyzed. The applications of laser coating treatment in the field of aeronautic manufacturing are analyzed in detail. The development direction of laser shock processing and laser coating treatm

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32

Potnuru, Sandeep, and C. V. S. Rajesh. "Modeling and Simulation of Bevel Gearboxes in AutoCAD." International Journal of Trend in Scientific Research and Development 2, no. 5 (2018): 1937–39. https://doi.org/10.31142/ijtsrd18200.

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Designing and developed of aeronautic bevel gearboxes is a complex and time consuming method. A gear or cogwheel is a rotating machine part having cut like teeth, or cogs, which mesh with another toothed part to transmit torque. Geared devices can change the speed, torque, and direction of a power source. Gears almost always produce a change in torque, creating a mechanical advantage, through their gear ratio, and thus may be considered a simple machine. The teeth on the two meshing gears all have the same shape. Two or more meshing gears, working in a sequence, are called a gear train or a tr

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De Moura, Jose Dos Reis Vieira, and Valder Steffen. "Impedance-based Health Monitoring for Aeronautic Structures using Statistical Meta-modeling." Journal of Intelligent Material Systems and Structures 17, no. 11 (2006): 1023–36. http://dx.doi.org/10.1177/1045389x06063087.

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34

FLOREA, Mihai, Vlad-Stefan CONSTANTIN, Andrei-Christian BUCUR, Raluca FAUR, Denis PREDU, and Alexandru CAZACU. "Materials and Structures Used in Aeronautics: Present and Future Perspectives." INCAS BULLETIN 16, no. 4 (2024): 57–72. https://doi.org/10.13111/2066-8201.2024.16.4.6.

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In recent years, significant advancements have been made in the development of novel materials for aeronautic applications. This effort aims to reduce costs by extending the operational life of structural and engine components, improving fuel economy, load capacity, and flight range. This paper investigates metallic materials such as aluminum alloys, titanium alloys, magnesium alloys, steels, nickel superalloys, and metal matrix composites (MMCs), providing an overview of recent advancements and highlighting current challenges and future perspectives in aeronautic metals. Several crucial facto

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35

Cacciola, Matteo, Aimé Lay-Ekuakille, and Giuseppe Megali. "Incremental Bayesian learning for in-service analysis of aeronautic composites." IET Science, Measurement & Technology 7, no. 6 (2013): 334–42. http://dx.doi.org/10.1049/iet-smt.2012.0151.

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36

Chimakurthi, Venkata Naga Satya Surendra. "Risks of Multi-Cloud Environment: Micro Services Based Architecture and Potential Challenges." ABC Research Alert 5, no. 3 (2017): 33—xx. http://dx.doi.org/10.18034/abcra.v5i3.590.

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Over the most recent couple of years, a modified programming engineering style has been created to plan new programming applications. This engineering style is especially appropriate for use cases in the avionic business, from an autonomously deployable programming administration. These administrations are worked around business and mission capacities and are freely deployable by completely computerized apparatus. With microservices, a few sorts of uses become simpler to construct and keep up with when they are separated into more modest, composable pieces that cooperate. This is rather than a

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Chimakurthi, Venkata Naga Satya Surendra. "Risks of Multi-Cloud Environment: Micro Services Based Architecture and Potential Challenges." ABC Research Alert 5, no. 3 (2017): States. http://dx.doi.org/10.18034/ra.v5i3.590.

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Over the most recent couple of years, a modified programming engineering style has been created to plan new programming applications. This engineering style is especially appropriate for use cases in the avionic business, from an autonomously deployable programming administration. These administrations are worked around business and mission capacities and are freely deployable by completely computerized apparatus. With microservices, a few sorts of uses become simpler to construct and keep up with when they are separated into more modest, composable pieces that cooperate. This is rather than a

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38

Citarella, R. "Non-linear MSD crack growth by DBEM for a riveted aeronautic reinforcement." Advances in Engineering Software 40, no. 4 (2009): 253–59. http://dx.doi.org/10.1016/j.advengsoft.2008.04.007.

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39

Frosina, Emma, Adolfo Senatore, Luka Palumbo, Giuseppe Di Lorenzo, and Ciro Pascarella. "Development of a Lumped Parameter Model for an Aeronautic Hybrid Electric Propulsion System." Aerospace 5, no. 4 (2018): 105. http://dx.doi.org/10.3390/aerospace5040105.

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This paper describes a case study for applying a hybrid electric propulsion system for general aviation aircraft. The work was performed by a joint team from the Centro Italiano Ricerche Aerospaziali (CIRA) and the Department of Industrial Engineering of the University of Naples Federico II. The use of electric and hybrid electric propulsion for aircraft has gained widespread and significant attention over the past decade. The driver of industry interest has principally been the need to reduce the emissions of combustion engine exhaust products and noise; however, studies have revealed the pot

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40

Sensors, Journal of. "Retracted: Modal Analysis of Aeronautic Spiral Bevel Gear in the Temperature Field." Journal of Sensors 2023 (December 20, 2023): 1. http://dx.doi.org/10.1155/2023/9825321.

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41

Doraghi, Qusay, Alina Żabnieńska-Góra, Gabriele Voto, et al. "Experimental and computational thermoelectric generator for waste heat recovery for aeronautic application." Energy 297 (June 2024): 131286. http://dx.doi.org/10.1016/j.energy.2024.131286.

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42

Russo, Antonio, and Alberto Cavallo. "Stability and Control for Buck–Boost Converter for Aeronautic Power Management." Energies 16, no. 2 (2023): 988. http://dx.doi.org/10.3390/en16020988.

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The need for greener and cleaner aviation has accelerated the transition towards more electric systems on the More Electric Aircraft. One of the key challenges related to the increasing number of electrical devices onboard is the control of bidirectional power converters. In this work, stability analysis and control of a buck–boost converter for aeronautic applications are presented. Firstly, stability of the buck–boost converter in the Lyapunov sense is proven by resorting to input-to-state stability notions. Then, a novel control design based on second order sliding mode control and uniting

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43

El Bayda, H., F. Valensi, M. Masquere, and A. Gleizes. "Energy losses from an arc tracking in aeronautic cables in DC circuits." IEEE Transactions on Dielectrics and Electrical Insulation 20, no. 1 (2013): 19–27. http://dx.doi.org/10.1109/tdei.2013.6451337.

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Bonora, R. G., H. J. C. Voorwald, M. O. H. Cioffi, G. S. Junior, and L. F. V. Santos. "Fatigue in AISI 4340 steel thermal spray coating by HVOF for aeronautic application." Procedia Engineering 2, no. 1 (2010): 1617–23. http://dx.doi.org/10.1016/j.proeng.2010.03.174.

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45

Fei, Tang, Zhao Xiaolu, and Xu Jianzhong. "The Application of Counter-Rotating Turbine in Rocket Turbopump." International Journal of Rotating Machinery 2008 (2008): 1–7. http://dx.doi.org/10.1155/2008/426023.

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Counter rotating turbine offers advantages on weight, volume, efficiency, and maneuverability relative to the conventional turbine because of its special architecture. Nowadays, it has been a worldwide research emphasis and has been used widely in the aeronautic field, while its application in the astronautic field is seldom investigated. Researches of counter rotating turbine for rocket turbopump are reviewed in this paper. A primary analysis of a vaneless counter rotating-turbine configuration with rotors of different diameters and rotational speeds is presented. This unconventional configur

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46

Lamicq, Pierre. "Main features of thermostructural composites for space, aeronautic and industrial applications." Advanced Composite Materials 8, no. 1 (1999): 47–53. http://dx.doi.org/10.1163/156855199x00065.

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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 (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 h

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Liu, Lei, Qiumin Jing, Hua Y. Geng та ін. "Revisiting the High-Pressure Behaviors of Zirconium: Nonhydrostaticity Promoting the Phase Transitions and Absence of the Isostructural Phase Transition in β-Zirconium". Materials 16, № 14 (2023): 5157. http://dx.doi.org/10.3390/ma16145157.

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Zirconium (Zr) is an important industrial metal that is widely used in nuclear engineering, chemical engineering, and space and aeronautic engineering because of its unique properties. The high-pressure behaviors of Zr have been widely investigated in the past several decades. However, the controversies still remain in terms of the phase transition (PT) pressures and the isostructural PT in β-Zr: why the PT pressure in Zr is so scattered, and whether the β to β’ PT exists. In the present study, to address these two issues, the Zr sample with ultra-high purity (>99.99%) was quasi-hydrostatic

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Aperador Chaparro, William, Andres Felipe Escobar Mosquera, and Fabian Andrés Pérez Londoño. "Evaluating protection systems against marine corrosion of aeronautic alloy Alclad 2024-T3." Ingeniería e Investigación 31, no. 1 (2011): 224–32. http://dx.doi.org/10.15446/ing.investig.v31n1.20558.

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This paper shows how two coating systems were obtained as an alternative for protection against corrosion of al clad 2024-T3which is used in battery compartment manufacture for T-41 aircraft. Such systems consist of three types of organic resin: a first layer of P-115 polyester resin as the first coating on both systems, and a second layer of Hetron 197-3 polyester resin in the first system and vinylester resin in the second one. Scanning electron microscopy (SEM) was used for surface morphology analysis, showing the roughness produced by surface treatment. The coatings were electrochemically

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Laurenzi, S., A. Grilli, M. Pinna, F. De Nicola, G. Cattaneo, and M. Marchetti. "Process simulation for a large composite aeronautic beam by resin transfer molding." Composites Part B: Engineering 57 (February 2014): 47–55. http://dx.doi.org/10.1016/j.compositesb.2013.09.039.

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