Thematische Bibliographien / Aircraf

Inhaltsverzeichnis

  1. Zeitschriftenartikel
  2. Dissertationen
  3. Bücher
  4. Buchteile
  5. Konferenzberichte
  6. Berichte der Organisationen

Auswahl der wissenschaftlichen Literatur zum Thema „Aircraf“

Autor: Grafiati
Veröffentlicht am 28. Juni 2021
Zuletzt aktualisiert am 29. Juli 2025

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Zeitschriftenartikel zum Thema "Aircraf"

1

Serenko, Irina. "RUSSIA INCLUSION IN «PAKISTAN STREAM» IN COURSE OF MUTUALLY BENEFICIAL ECONOMIC COOPERATION." Eastern Analytics 13, no. 1 (2022) (2022): 36–47. http://dx.doi.org/10.31696/2227-5568-2022-01-036-047.

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Air transport has become the most dynamic segment of the PRC's transport services market. As a necessary conditon for the country's territorial integrity and the unity of its economic space, regular air lines connect all parts of the huge state, ensure the expansion of China's foreign economic relatons and its integraton into the system of world economic relatons. Despite the losses incurred by the industry in 2020 due to the COVID‑19 epidemic, China contnues to explode its air travel market. Moreover, the Chinese airlines were the fastest to restore the previous, «dock‑like» indicators. At th
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Tomberg, Igor. "THE AIR TRANSPORT OF CHINA." Eastern Analytics 13, no. 1 (2022) (2022): 24–35. http://dx.doi.org/10.31696/2227-5568-2022-01-024-035.

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Air transport has become the most dynamic segment of the PRC's transport services market. As a necessary conditon for the country's territorial integrity and the unity of its economic space, regular air lines connect all parts of the huge state, ensure the expansion of China's foreign economic relatons and its integraton into the system of world economic relatons. Despite the losses incurred by the industry in 2020 due to the COVID‑19 epidemic, China contnues to explode its air travel market. Moreover, the Chinese airlines were the fastest to restore the previous, «dock‑like» indicators. At th
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Suharyadi, Suharyadi, and Yudhistira Tri Nurteisa. "Teknologi Pesawat Tanpa Awak untuk Pemetaan Skala Detail Rencana Jaringan Pipa Sanitasi Komunal bagi Masyarakat Dusun Kepek 1, Kepek, Wonosari, Gunungkidul." Jurnal Pengabdian kepada Masyarakat (Indonesian Journal of Community Engagement) 2, no. 1 (2017): 1–13. http://dx.doi.org/10.22146/jpkm.22081.

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Human settlements can not be separated from the emergence of waste generated by human activity. Waste will give a negative efect on health and the environment if not handled and managed properly. Hamlet Kepek 1, Kepek, Wonosari have realized the impact that arises when household waste is not managed properly. For that, some residents have initiated a communal waste management and manufacture of communal sanitation pipelines. Conventionally, communal sanitary pipe network planning and data requires a huge cost, for it takes breakthrough of utilization of appropriate technology to facilitate the
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Mikhailov, E. A., and V. B. Fedorov. "Study of the design parameters of the onboard system for changing the massinertia characteristics of the aircraf." Bulletin of the South Ural State University series "Mechanical engineering industry" 23, no. 1 (2023): 50–62. http://dx.doi.org/10.14529/engin230105.

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The paper presents the results of a study of a new concept of a system for changing the mass-inertial characteristics of nominally axisymmetric rotor structures, in particular, aircraft of an axisymmetric shape. This system can be used for static and dynamic balancing of the product directly during operation and is a balancing weight installed on the movable platform of the mechanism with parallel kinematics of the hexapod type. It can be applied, including for nominally axisymmetric aircraft, to parry disturbances from asymmetries of various kinds by purposefully creating a mass-inertial asym
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Al Wardi, Yousuf, Sasirajan Jeevarathinam, and Saleh Al Sabei. "A Cross-Cultural Anthropometric Analysis in Military Aviation." Aerospace Medicine and Human Performance 91, no. 4 (2020): 358–62. http://dx.doi.org/10.3357/amhp.5530.2020.

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BACKGROUND: Aircrew-aircraft compatibility is important in military aviation for flight safety. Anthropometric aircrew selection standards in RAFO were embedded from the selection standards of western defense forces as the aircrafts were imported from there. Henceforth efforts were made to fit local native aviators into aircrafts not initially designed for them. In view of this, this study was carried out to obtain the anthropometric data of Oman aircrew recruits and compare these with published western and eastern data with a hope to understand and highlight the aircrew-aircraft mismatch issu
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Biswal, P., and YS Dahiya. "Principal component analysis: The path ahead for aircrew-aircraft compatibility at the Institute of Aerospace Medicine." Indian Journal of Aerospace Medicine 63 (November 7, 2019): 8–15. http://dx.doi.org/10.25259/ijasm_2019_3.

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Introduction: The Institute of Aerospace Medicine provides design consultancy on aircraft-aircrew compatibility on a number of fixed-wing as well as rotary-wing aircrafts during various stages of development. Till date, the cockpit compatibility of aircrew has been determined based on the percentile concept. Percentiles, though useful when dealing with a single parameter, pose major design and fitment problems when considering multiple parameters simultaneously as in aircraft cockpit design. The concept of multivariate analysis has been the solution which the aviation industry the world over h
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Ponomarev, Artyom I., and Mikhail Y. Sorokin. "INTEGRATION OF THE MEASURED ALTITUDE-SPEED PERFORMANCES IN THE SYSTEM." Автоматизация процессов управления 2, no. 64 (2021): 18–22. http://dx.doi.org/10.35752/1991-2927-2021-2-64-18-22.

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The air data system used by modern aircrafts is a soft hardware designed to measure, compute, and display the altitude-speed performances as well as other parameters such as air temperature, angles of attack and slip; and to provide to aircrew and consumers (various on-board systems) with this information. The speed and altitude are one of the most important flight parameters of an aircraft. The operating principle of modern onboard equipment for measuring the aircraft movement parameters while in flight is based on an aerometric method. This article deals with a method for increasing the accu
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Yao, Xinchi. "Differences in large aircraft design between military and civil perspectives." Theoretical and Natural Science 14, no. 1 (2023): 112–16. http://dx.doi.org/10.54254/2753-8818/14/20240908.

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Military transport aircrafts and civil aircrafts are important parts of the aviation field. With the development of aviation technology and the specificity of aircraft functions, the design of military transport aircraft and civil aircraft gradually differs according to application scenarios. However, in the aircraft design, military transport aircrafts and civil aircrafts still have a lot of mutual references. Analyzing the differences between them and the reasons for the differences may contribute to the design and development of military transport aircraft and civil aircraft in the future,
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Lewitowicz, Jerzy, and Stefan Rutkowski. "Research of the Reliability of an Air Combat Manoeuvere – Nosedive of a Jet Powered Aircraft / Badanie Niezawodności Lotniczego Manewru Bojowego – Lotu Nurkowego Samolotu Odrzutowego." Journal of KONBiN 31, no. 1 (2014): 13–22. http://dx.doi.org/10.2478/jok-2014-0019.

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Abstract This paper considered a problem of: the reliability of performance of a nosedive of a jet powered aircraft in the context of the ability of pilots trained on a simulator to reliably accomplish a combat mission. For research purposes, the manoeuvre of attack of a target with the nosedive, which is most commonly used by the pilots performing flights on different types of modern aircrafts, and the basic manoeuvre during aircrew training, both basic and advanced were assumed. The research was conducted on a flight simulator.
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Fujita, Etsushi, Taichi Higashioka, Manabu Sugiura, and Osamu Kohashi. "Evaluation method of military aircraft noise using AI analysis of aircraft images." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 263, no. 6 (2021): 854–62. http://dx.doi.org/10.3397/in-2021-1668.

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In recent aircraft noise survey in Japan, noise data is associated with each aircraft by flight log or by radio information including transponder signals. Especially, above Tokyo metropolitan area, flight tracks are tangled extremely each other, therefore assessments from various perspectives such as departure / arrival airport, used runway, aircraft model, and operator have been demanded for determining noise policies. However, for military aircrafts, it is not easy to identify their information with the same way as commercial aircrafts, because their flight logs are not disclosed and many of
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Dissertationen zum Thema "Aircraf"

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Torres, Calderon Rosa Maria. "Multi-objective environmentally-friendly departure procedures for civil aircraf : modeling, optimization and robustness assessment." Toulouse 3, 2011. http://www.theses.fr/2011TOU30320.

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Cette thèse présente le concept MCDP (Multi-Criteria Departure Procedure), qui a comme objectif l’optimisation des procédures de départ afin de minimiser l’impact environnemental des avions. Ces impacts portent essentiellement sur les nuisances acoustiques, la qualité de l’air et l’émission des gaz d’effet de serre. Il n’existe pas une seule procédure capable de minimiser les trois critères simultanément. Le concept MCDP est donc modélisé par un problème d’optimisation multi-objectif sous contraintes. La technique de recherche directe MADS est utilisée pour obtenir les trajectoires Pareto opti
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Urbano, Simone. "Detection and diagnostic of freeplay induced limit cycle oscillation in the flight control system of a civil aircraf." Thesis, Toulouse, INPT, 2019. http://www.theses.fr/2019INPT0023/document.

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Cette étude est le résultat d’une thèse CIFRE de trois ans entre le bureau d’étude d’Airbus (domaine du contrôle de l’avion) et le laboratoire TéSA à Toulouse. L’objectif principal est de proposer, développer et valider une solution logicielle pour la détection et le diagnostic d’un type spécifique de vibrations des gouvernes de profondeur et direction, appelée oscillation en cycle limite (limit cycle oscillation ou LCO en anglais), basée sur les signaux existants dans les avions civils. LCO est un terme mathématique générique définissant un mode périodique indépendant de conditions initiales
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Dvořáček, Zdeněk. "Návrh hlavního podvozku pro letouny řady Zlín 40." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-442850.

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This master thesis deals with the modernization of the main landing gear of the Z 143 LSi aircraft. The main emphasis is placed on optimizing of the landing gear shape and its deformation characteristics. Along with this change, variants made of different materials are examined. The landing load is calculated analytically and the load-bearing capacity of the structure is verified using the numerical FEM method. This work brings a possible replacement of the current chassis, which is production-intensive not only in time and money, but also in terms of cooperation with external companies. The o
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Bauer, David O. "A historical perspective of aircrew systems effects on aircraft design." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1996. http://handle.dtic.mil/100.2/ADA320281.

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Thesis (M.S. in Aeronautical Engineering) Naval Postgraduate School, September 1996.<br>Thesis advisor(s): Conrad F. Newberry. "September 1996." Includes bibliographical references (p. 99-100). Also available online.
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Megas, Vasileios. "Aircraft to Aircraft Connectivity Analysis." Thesis, KTH, Skolan för elektroteknik och datavetenskap (EECS), 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-254887.

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It is very common to feel the need to be connected, especially in cases where we are idle, such as in airplanes. Aircraft connectivity has already been implemented by using direct air-to-ground communication and satellite communication. However, since the current solutions are not satisfying, more ways to provide connectivity to aircraft are being researched. One solution is to use aircraft as relay nodes and forward signals to aircraft which are out of range of the ground base stations, creating an ad-hoc network.This thesis aims in evaluating the performance of such networks over the North A
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Federico, Claudio Antonio. "Dosimetria da radiação cósmica no interior de aeronaves no espaço aéreo Brasileiro." Universidade de São Paulo, 2011. http://www.teses.usp.br/teses/disponiveis/85/85131/tde-26012012-104504/.

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Neste trabalho, cujo objetivo foi fornecer subsídios que permitam estabelecer um sistema de dosimetria para as tripulações de aeronaves que operam no território nacional, foi desenvolvida uma técnica para realizar medições do equivalente de dose ambiente em aeronaves. Foi testado um detector ativo, para uso embarcado em aeronaves, avaliando-se sua adequação a este tipo específico de medição, assim como sua suscetibilidade às interferências magnética e eletromagnética. O equipamento foi calibrado em campos metrologicamente rastreados e foi verificado em um campo especial do laboratório europeu
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Serrano, Ignacio. "Unmanned Aircraft System (UAS) vs. Manned Aircraft System (MAS): A Military Aircraft Study." Digital Commons at Loyola Marymount University and Loyola Law School, 2015. https://digitalcommons.lmu.edu/etd/430.

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Unmanned Aerial Vehicles (UAVs) are common place in the 21st century, whether they are small to medium sized remotely piloted vehicles (aka drones) or large advanced Unmanned Aerial Systems with a preprogrammed flight path. There is anticipation that these Unmanned Systems will, in the future assume the roles of their traditional manned aircraft counterparts. There is also the perception that these Unmanned Systems should be developed partly because they would be less expensive when compared to their manned aircraft. This integrative paper asserts that this perception is not reality with regar
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Iskender, Hani. "Aircraft Simulator." Thesis, Linköping University, Department of Electrical Engineering, 2005. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-2936.

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<p>At Saab Bofors Dynamics there are projects running which purpose are to develop simulators for various weapon systems like RBS 70. In order to manage creating real working simulators Saab Bofors Dynamics has to do more research and this final thesis is a part of this process.</p><p>This final thesis has been performed at Saab Bofors Dynamics in the department of modelling and simulation, RTRKM, in Karlskoga. The purpose was to develop a control algorithm which makes it possible for an aircraft to behave real when controlling through a joystick.</p><p>The conclusions show that further improv
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Sychova, I. U., and E. I. Zolotova. "Supersonic aircraft." Thesis, Вид-во СумДУ, 2011. http://essuir.sumdu.edu.ua/handle/123456789/22211.

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Thompson, Brian G. "Aircraft agility." Thesis, This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-09192009-040436/.

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Bücher zum Thema "Aircraf"

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Bauer, David O. A historical perspective of aircrew systems effects on aircraft design. Naval Postgraduate School, 1996.

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Kershaw, Andrew. Aircraft. Derrydale Books, 1992.

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Buydos, John F. Aircraft. Science Reference Section, Science, Technology and Business Division, Library of Congress, 2000.

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Schaefer, Lola M. Aircraft. Raintree, 2004.

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Parker, Steve. Aircraft. Mason Crest, 2011.

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Gunston, Bill. Aircraft. F. Watts, 1986.

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Langley, Andrew. Aircraft. Puffin, 1991.

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Ian, Graham. Aircraft. Belitha, 1997.

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Hawes, Alison. Aircraft. Oxford University Press, 2010.

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Bill, Gunston. Aircraft. Franklin Watts/Aladdin, 1985.

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Buchteile zum Thema "Aircraf"

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Paluszek, Michael, and Stephanie Thomas. "Aircraft." In MATLAB Recipes. Apress, 2015. http://dx.doi.org/10.1007/978-1-4842-0559-4_11.

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Juson, Adam, and Catherine Juson. "Aircraft." In Advances in the Biology and Management of Modern Bed Bugs. John Wiley & Sons, Ltd, 2018. http://dx.doi.org/10.1002/9781119171539.ch38.

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Pleter, Octavian Thor. "Aircraft." In Air Navigation. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-52994-8_7.

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Kalić, Milica, Slavica Dožić, and Danica Babić. "Aircraft." In Introduction to the Air Transport System. CRC Press, 2022. http://dx.doi.org/10.1201/9781003102533-2.

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Paluszek, Michael, and Stephanie Thomas. "Aircraft." In MATLAB Recipes. Apress, 2020. http://dx.doi.org/10.1007/978-1-4842-6124-8_12.

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Kearns, Suzanne K. "Aircraft." In Fundamentals of International Aviation, 2nd ed. Routledge, 2021. http://dx.doi.org/10.4324/9781003031154-2.

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Henke, Rolf. "Aircraft." In Technology Guide. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-88546-7_58.

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Yu, David. "Introduction." In Aircraft Valuation. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-6743-8_1.

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Yu, David. "Background Concepts and Definitions." In Aircraft Valuation. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-6743-8_2.

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Yu, David. "Global Aircraft Leasing Industry Characteristics." In Aircraft Valuation. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-6743-8_3.

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Konferenzberichte zum Thema "Aircraf"

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Shields, Paul. "Additive Manufacturing of Simulator Parts." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12097.

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The DARPA Aircrew Labor In-Cockpit Automation System (ALIAS) program aims to develop custom, tailorable kits that can be implemented into existing aircraft to provide autonomous and optionally piloted vehicle capabilities. In support of this program, Sikorsky Aircraft has developed kits for both fixed wing and rotary wing aircraft. During the development of ALIAS kits, Sikorsky used Additive Manufacturing for prototyping and to meet critical program milestones. Additive Manufacturing was shown to be a viable solution for producing simulator and demonstrator parts required for various aspects o
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Chen, Yong, Sebastien Ghinet, Andrew Price, Viresh Wickramasinghe, and Anant Grewal. "Evaluation of Aircrew Whole-Body Vibration Exposure Levels on a Canadian CH-147F Chinook Helicopter." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11418.

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Flight testing has been performed on a Royal Canadian Air Force (RCAF) CH-147F Chinook helicopter to investigate aircrew whole-body vibration (WBV) exposure levels in accordance with ISO 2631-1 or MIL-STD-1472G standard. Results showed that the helicopter cabin vibration was dominated at the N/rev harmonics of the three-bladed tandem rotor speed. The aircrew WBV levels varied significantly depending on flight conditions and aircraft load configurations while the highest levels of WBV occurred at high speed level flight maneuver conditions. With reference to the guidelines in the standards, the
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Aylworth, Warren. "The Evolving Threat and Operational Environment's Impact on Aircraft Vulnerability Reduction." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12843.

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This paper examines how the evolving threat and the Operational Environment (OE) have challenged the effectiveness of our current aircraft and aircrew vulnerability reduction methods. It provides specific examples of the how Threat weapon systems have evolved, and nominates specific representative weapon systems as the new benchmark for future vulnerability reduction efforts. Additionally this paper examines how the changing OE directly impacts the overall vulnerability equation by highlighting that legacy vulnerability reduction will prove insufficient to sustain expeditionary warfare. Recogn
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Finckenor, Jeff, Terry Baker, Christopher Wallace, Michael Chandler, and Scott Engelmeyer. "Establishing Rotorcraft Component Fatigue Lives using SUMS Data and a Partial Usage Spectrum Approach for the MH-47G Chinook." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11472.

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Lives of fatigue critical components for Army aircraft are typically established based on component strength from ground test, loads for each regime from flight test, and aircraft usage in each regime from engineering and aircrew judgement. This paper documents the first time that an Army platform has had component fatigue lives defined with usage monitored by the Structural Usage Monitoring System (SUMS). SUMS uses aircraft parameters to identify the regime at any given time. The time in recognized regimes is summed up to generate a spectrum of time spent in each regime. The Partial Regime Re
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Finckenor, Jeff, Terry Baker, Mark Davis, et al. "Establishing Rotorcraft Component Fatigue Lives using SUMS Data and a Partial Usage Spectrum Approach for the UH-60 L/M Blackhawk." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12769.

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Lives of fatigue critical components for Army aircraft are typically established based on component strength from ground test, loads for each regime from flight test, and aircraft usage in each regime from engineering and aircrew judgement. This paper documents the updates to the spectrum for the large Army UH-60 fleet based on usage monitored by the Integrated Vehicle Health Management System (IVHMS). IVHMS and subsequent post processing uses aircraft parameters to identify the regime at any given time. The recognized regimes are summed to generate a spectrum of time or occurrences in each re
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McGrath, Braden, Jeffrey Cox, Joe McKay, and Angus Rupert. "Mission Utility of a Tactile Display in Rotary Wing Operations." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10152.

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Over the last decade, the foremost helicopter issue reported by the military operating in desert environments is the inability to maintain control of the aircraft in degraded visual environments (DVE). A DVE mishap is a special subset of the Spatial Disorientation (SD) mishap. SD is defined as the inability of the pilot to correctly perceive the position, motion or attitude of the aircraft relative to the earth or other significant objects. The US military organization has been developing improved man-machine interfaces that increase pilots’ awareness of spatial orientation, including the use
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Stanzione, Kaydon, Michael Baiada, and Richard Ruff. "An Investigation of Emergency Flight Operations with Vertical Flight Aircraft in Class B Airspace." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12215.

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This paper investigates how vertical flight aircraft operations can more efficiently mesh with airline arrival and departure flows in both emergency and non-emergency conditions within Class B airspace. Specifically, Helicopter Air Ambulance Operations (HAAO) are merged with the results of FAA studies addressing Aircraft Arrival Management Systems. The unique flight capabilities of vertical flight aircraft must be optimized to provide rapid emergency response while permitting queued airlines to land with minimal to no delay. FAA's NextGen and specific HAAO procedural and equipment mandates off
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Horton, Ira D., and Allen N. Budge. "Electronic Corrosion in Aerospace Equipment." In CORROSION 1985. NACE International, 1985. https://doi.org/10.5006/c1985-85330.

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Abstract Corrosion of electronics, especially on printed circuit boards (PCBs) in the missile and aircraft industries have been a major problem for years. The causes and treatment of this corrosion is much the same as for many other types of corrosion on other systems. Some environments in certain locations, cause unique kinds corrosion. The corrosion of electronics found in launch facilities (LF), launch control facilities (LCF) and sealed components of many types of aircrafts is a major problem in the Air Force. Some require special treatment. Conformal coatings as a means of protection of t
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Xiao, Kun, Yuxin Chen, Wuyao Jiang, Chenyao Wang, and Longfei Zhao. "Modeling, Simulation and Implementation of a Bird-Inspired Morphing Wing Aircraf." In 2019 3rd International Conference on Robotics and Automation Sciences (ICRAS). IEEE, 2019. http://dx.doi.org/10.1109/icras.2019.8808959.

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Lou, Bin. "Preliminary Design of Several New Kinds of Martian Aircrafts." In Vertical Flight Society 77th Annual Forum & Technology Display. The Vertical Flight Society, 2021. http://dx.doi.org/10.4050/f-0077-2021-16736.

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The low-altitude Martian aircraft has become an important research direction in the field of Mars exploration recently. The traditional Martian aircrafts including floating balloons, fixed-wing aircrafts, rotorcrafts, flapping-wing aircrafts and tilt-rotor aircrafts, have been proposed and studied for decades. In this paper, several new kinds of Martian aircraft were proposed, maybe enlightening other researchers. Compressed-air jet aircraft makes use of the CO2 for airjet to control the flight. Coaxial tri-rotor autogyro is designed with three rotors, modified from "Ingenuity" with light weig
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Berichte der Organisationen zum Thema "Aircraf"

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Reason, William. Helicopter Aircrew Integrated Life Support System (HAILSS) Aircraft Integration Tests. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada377892.

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Anderson, Jay, Dan Bowman, Douglas Burke, Edward Campbell, and Barry Coble. Aircraft. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada424435.

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3

Yoel, David, Tina Sicilia, Matthew Bogaart, and Jeremy Fernandes. PR-417-203902-R02 Remote Sensing and Leak Detection Platform that Can Deploy Multiple Sensor Types. Pipeline Research Council International, Inc. (PRCI), 2024. http://dx.doi.org/10.55274/r0000055.

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American Aerospace Technologies, Inc. has conducted a pilot project for the Pipeline Research Council, International to evaluate the performance of an automated threat detection system onboard a medium alti-tude, long endurance unmanned aircraft capable of beyond visual line of sight flight that can be used in the pipeline industry for routine patrol and surveillance as a risk reduction solution. The unmanned aircraft system test program evaluation was conducted at Test Site(s) in Pendleton, Oregon, Woodbine, New Jersey, and San Joaquin Valley, California using American Aerospace sensors, unma
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Haubrich, Julia, Sarah Benz, Ullrich Isermann, et al. Leq+X - Lärmexposition, Ereignishäufigkeiten und Belästigung: Re-Analyse von Daten zur Belästigung und Schlafstörung durch Fluglärm an deutschen und Schweizer Flughäfen. Universitätsbibliothek der Ruhr-Universität Bochum, 2020. http://dx.doi.org/10.46586/rub.164.139.

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In this study, part of the data sets from 4 large Swiss and German aircraft noise impact studies are re-analysed using logistic multi-level regression models. The aim is to investigate the assumptions that the prediction of a) the percentage of persons highly annoyed by aircraft noise or b) the percentage of persons highly sleep disturbed by aircraft noise can be improved if (i) instead of the energy-equivalent continuous noise level alone, either additional or alternative, more frequency-based aircraft noise metrics and (ii) also airport-specific characteristics are used as predictors. The re
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Stache, Jeremiah. A dynamic aircraft response model for determining roughness limits. Engineer Research and Development Center (U.S.), 2024. http://dx.doi.org/10.21079/11681/48513.

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Runway roughness poses significant risks to aircraft and aircraft personnel. Roughness irregularities can be found in both civilian and military airfields, from rutting to bomb-damaged repairs. Various methods exist for determining roughness criteria, such as discrete surface deviation evaluation and dynamic response models. Although validated dynamic response models such as TAXI-G were used extensively in the HAVE BOUNCE program from the 1970s up to the late 1990s, modern military aircraft have not undergone the same formal analysis. This paper presents the mathematical formulation and valida
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Cook, Stephen, and Anna Dietrich. Regulatory Barriers to Autonomy in Aviation. ASTM International, 2022. http://dx.doi.org/10.1520/tr3-eb.

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As technology advances and increased automation and autonomy in aviation become ever more within reach, it makes sense to turn our attention to the operational regulatory landscape within which these aircraft will be flown. Technical standards that could be part of the means of compliance for the airworthiness certification of these aircraft are receiving attention within a variety of standards development organizations (SDOs). The operational rules and their implications for autonomous aircraft, however, remain largely unexplored.
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Lee, E. U., R. Taylor, C. Lei, and H. C. Sander. Aircraft Steels. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada494348.

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Spicer, John, Fadel M. Al Garni, Deborah Bereda, et al. Aircraft Industry. Defense Technical Information Center, 2007. http://dx.doi.org/10.21236/ada475111.

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Fernandez, Ruben, Hernando Lugo, and Georfe Dulikravich. Aerodynamic Shape Multi-Objective Optimization for SAE Aero Design Competition Aircraft. Florida International University, 2021. http://dx.doi.org/10.25148/mmeurs.009778.

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The SAE Regular Class Aero Design Competition requires students to design a radio-controlled aircraft with limits to the aircraft power consumption, take-off distance, and wingspan, while maximizing the amount of payload it can carry. As a result, the aircraft should be designed subject to these simultaneous and contradicting objectives: 1) minimize the aerodynamic drag force, 2) minimize the aerodynamic pitching moment, and 3) maximize the aerodynamic lift force. In this study, we optimized the geometric design variables of a biplane configuration using 3D aerodynamic analysis using the ANSYS
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Heymsfield, Ernie, and Jeb Tingle. State of the practice in pavement structural design/analysis codes relevant to airfield pavement design. Engineer Research and Development Center (U.S.), 2021. http://dx.doi.org/10.21079/11681/40542.

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An airfield pavement structure is designed to support aircraft live loads for a specified pavement design life. Computer codes are available to assist the engineer in designing an airfield pavement structure. Pavement structural design is generally a function of five criteria: the pavement structural configuration, materials, the applied loading, ambient conditions, and how pavement failure is defined. The two typical types of pavement structures, rigid and flexible, provide load support in fundamentally different ways and develop different stress distributions at the pavement – base interface
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