Relevant bibliographies by topics / Aircraf

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Aircraf'

Author: Grafiati
Published: 28 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Aircraf"

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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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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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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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Zhang, Yuhang, Hao Sun, Jiawei Zuo, Hongqi Wang, Guangluan Xu, and Xian Sun. "Aircraft Type Recognition in Remote Sensing Images Based on Feature Learning with Conditional Generative Adversarial Networks." Remote Sensing 10, no. 7 (2018): 1123. http://dx.doi.org/10.3390/rs10071123.

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Aircraft type recognition plays an important role in remote sensing image interpretation. Traditional methods suffer from bad generalization performance, while deep learning methods require large amounts of data with type labels, which are quite expensive and time-consuming to obtain. To overcome the aforementioned problems, in this paper, we propose an aircraft type recognition framework based on conditional generative adversarial networks (GANs). First, we design a new method to precisely detect aircrafts’ keypoints, which are used to generate aircraft masks and locate the positions of the a
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Zuo, Yu Yu. "Analysis of Gas Turbine Engines Auxiliary Power Units." Applied Mechanics and Materials 533 (February 2014): 13–16. http://dx.doi.org/10.4028/www.scientific.net/amm.533.13.

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As aircraft became more complex a need was created for a power source to operate the aircraft systems on the ground without the necessity for operating the aircrafts main engines. This became the task of the Auxiliary Power Unit (APU). The use of an APU on an aircraft also meant that the aircraft was not dependant on ground support equipment at an airfield. It can provide the necessary power for operation of the aircrafts Electrical, Hydraulic and Pneumatic systems. It should come as no surprise that the power unit selected to do this task is a Gas Turbine Engine.
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Wang, Hong Yong, Rui Ying Wen, and Yi Fei Zhao. "Empirical Research on Topological Characteristics of Air Traffic Situation Network." Applied Mechanics and Materials 744-746 (March 2015): 1975–79. http://dx.doi.org/10.4028/www.scientific.net/amm.744-746.1975.

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A method for description of structural characteristics of air traffic situation based on the theory of complex network was proposed. This method characterizes the air traffic situation from three dimensions, including single aircraft, local sector, and overall sector. We selected the routinely-recorded flight data in an air traffic control sector within China's airspace in 2013. With the aircrafts in the sector regarded as nodes, and with the between-aircraft proximity relations as edges, we constructed an undirected and unweighted aircraft network. The results show that network node degree ca
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Yao, Man. "Water Impact Analysis for Aircraft over Sea." Applied Mechanics and Materials 341-342 (July 2013): 563–66. http://dx.doi.org/10.4028/www.scientific.net/amm.341-342.563.

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The modern aircrafts flying height is strictly limited by the conditions on the sea. Terrible conditions may lead overturning or dropping into the water to the aircraft. Whats more, the structure of the aircraft may be broken by water-impact force. The affection of the water impact must be considered to promise the safety of the aircraft. This paper focuses on the water impact to a typical symmetrical aircraft flying above sea. The water impact force related to the trajectory angle and equivalent pitch angle is researched based on the water impact force model of a two-dimensional wedge. In add
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Zhao, Chang Jun, Yue Bai, Xun Gong, Dong Fu Xu, and Zhi Jun Xu. "Control System Design of a Hex-Rotor Aircraft Based on the Neural Network Sliding Mode Method." Advanced Materials Research 971-973 (June 2014): 418–21. http://dx.doi.org/10.4028/www.scientific.net/amr.971-973.418.

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For the existing Multi-rotor aircrafts, the under-actuation and strong coupling characteristics have a remarkable influence on their flight performance. In order to overcome this effect, a novel Hex-Rotor aircraft is proposed in this paper. Based on the unique configuration of its six driving rotors, the Hex-Rotor aircraft has the ability to achieve the real independent control on the space 6-DOF channels. An autonomous flight control system with neural network sliding mode is designed. The simulation proved that the novel Hex-Rotor aircraft has desired maneuvering capability,and thehe control
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Dissertations / Theses on the topic "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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Thompson, Brian G. "Aircraft agility." Thesis, This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-09192009-040436/.

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Hacker, Earl W. "One-year UDP: a cost/benefit analysis of a proposed alternative to the Marine Corps' Unit Deployment Program for fighter aviation." Thesis, Monterey, California. Naval Postgraduate School, 1988. http://hdl.handle.net/10945/23337.

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Approved for public release; distribution is unlimited<br>The author examines the incremental costs and benefits associated with a change from six-month unit deployments to one-year unit deployments. The analysis is based primarily on five fighter squadrons participating in the Marine Corps' Unit Deployment Program and takes in the period July 1976 to October 1988. Regression analysis is used to project transportation cost savings of $4 million in real terms from FY 1989 through FY 1993. With a change to a one-year Unit Deployment Program, fighter squadrons should experience net increases
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Books on the topic "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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Parker, Steve. Aircraft. Mason Crest, 2011.

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Aircraft. Universe, 1988.

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Maynard, Christopher. Aircraft. Lerner Publications, 1999.

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Langley, Andrew. Aircraft. Bookwright Press, 1989.

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Aircraft. Reaktion, 2003.

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1928-, Roffe Michael, ed. Aircraft. Piccolo, 1985.

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Langley, Andrew. Aircraft. Puffin, 1991.

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Santos, Julie Dos. Aircraft. Marshall Cavendish Benchmark, 2010.

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Aircraft. Trefoil, 1987.

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Book chapters on the topic "Aircraf"

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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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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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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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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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Joslin, Robert E. "Certification of Aircraft and Aircraft Systems." In Handbook of Human Factors in Air Transportation Systems. CRC Press, 2017. http://dx.doi.org/10.1201/9781315116549-8.

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Hadcock, Richard N. "Aircraft Applications." In Handbook of Composites. Springer US, 1998. http://dx.doi.org/10.1007/978-1-4615-6389-1_49.

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Isaksson, Marléne. "Aircraft Industry." In Kanerva's Occupational Dermatology. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-02035-3_116.

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Isaksson, Marléne. "Aircraft Industry." In Kanerva’s Occupational Dermatology. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-68617-2_116.

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Howe, Denis. "Aircraft Configuration." In Aircraft Conceptual Design Synthesis. John Wiley & Sons, Ltd, 2014. http://dx.doi.org/10.1002/9781118903094.ch2.

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Conference papers on the topic "Aircraf"

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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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Matula, Dominik, and Martin Bugaj. "Analysis of selected aircrafts suitable for PPL training." In Práce a štúdie. University of Zilina, 2021. http://dx.doi.org/10.26552/pas.z.2021.2.25.

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The main goal of the paper is based on the analysis to define the criteria for selecting an aircraft suitable for PPL training. We achieved the main goal by meeting two sub-goals. The first sub-objective is the analysis of training organizations in Slovakia, on the basis of which we have selected entities for the second sub-objective thus the analysis of selected aircrafts suitable for PPL training. In this work we analyze three, most used training aircrafts for PPL training in Slovakia. We analyze selected aircrafts in terms of three main parts, which include, analysis of technical parameters
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Venkatesan, Yaamunan, Rohitha Paruchuri, and T. S. Ravigururajan. "A CFD Analysis of Transverse Airflow Around the Exterior of an Aircraft Fuselage Inside a Large Enclosure." In ASME/JSME 2011 8th Thermal Engineering Joint Conference. ASMEDC, 2011. http://dx.doi.org/10.1115/ajtec2011-44431.

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A model for predicting the airflow over the aircraft exterior with in a hangar is presented in this paper. The main reason behind this was to analyze the amount of air flowing over the aircraft at the time of painting, in order to dry the paint effectively and avoid possible hazardous effects on the people painting the aircraft. The air flow was supplied through the HVAC system in the hangar area. The HVAC system was available at the ceiling and air flows from the diffuser at the ceiling level. Grills were placed at the floor level in order to capture the air that flows down in the hangar area
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Templalexis, Ioannis, Ioannis Lionis, and Sotiris Kitinos. "Correlation Between Engine and Aircraft Loadings for Several Mission Types." In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-15611.

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Abstract Fighter aircraft constitutes a well-defined class of aircraft. Their extensive use on a daily basis by operators stands as a strong motive behind studies that concern their rate of “exhaustion ”. For an aircraft operator either civil or military, it is very important at any point in time to have a clear view of the engines’ and the aircrafts’ operating condition. This is valuable information in order to foresee undesired incidences and in order to schedule missions in accordance to the actual and anticipated maintenance needs. For the latter, the operator would also need to know the r
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Wesołowski, Mariusz, and Krzysztof Blacha. "The Impact of Load Bearing Capacity of Airfield Pavement Structures on the Air Traffic Safety." In Environmental Engineering. VGTU Technika, 2017. http://dx.doi.org/10.3846/enviro.2017.124.

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Airfield pavement is a marked and appropriately prepared surface of an airfield functional element that performs a definite function in aircraft operations. The structure of airfield pavement is most often composed of a set of layers whose task is to absorb and transfer loads coming from moving aircraft onto the ground in a way that ensures its definite durability. Structures of airfield pavements are designed for a definite exploitation period on the assumption of predicted volume and structure of the air traffic. Safety of air operations conducted by aircrafts on airfield pavements depends m
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Paruchuri, Rohitha, Yaamunan Venkatesan, and T. S. Ravigururajan. "Modeling Airflow Inside an Aircraft Interior With Multiple Inlets and Outlets." In ASME/JSME 2011 8th Thermal Engineering Joint Conference. ASMEDC, 2011. http://dx.doi.org/10.1115/ajtec2011-44432.

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A model for predicting the airflow inside an aircraft interior is presented in this paper. The objective was to optimize the amount of air flowing inside the aircraft at the time of painting, in order to dry the paint effectively and to minimize hazardous effects on the painting crew. The hangar area was split into three regions such that three aircrafts were placed for the purpose of painting. The three regions were separated with curtains between them which acted as separators between the aircraft. A 3D model of the aircraft fuselage with its openings was developed. The fuselage has two pilo
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Máčadi, Marek, and Alena Novák Sedláčková. "Legislative framework for an aircraft maintenance technician." In Práce a štúdie. University of Žilina, 2021. http://dx.doi.org/10.26552/pas.z.2021.1.13.

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The purpose of this paper is to create up-to-date aviation legislations study material focused on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks for future students of aircraft maintenance technology at the Air Transport Department, FPEDAS of the University of Žilina. As a relatively new studying programme, it has a lack of study materials in the field of aviation legislation, mainly in the field of aviation maintenance, whether in terms of technical requirements of aircrafts a
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Hernandez-Rivera, Ricardo, Abel Hernandez-Guerrero, Cuauhtemoc Rubio-Arana, and Raul Lesso-Arroyo. "Numerical Study in Wing Tip Vortex for a Modified Commercial Boeing Aircraft." In ASME 2008 International Mechanical Engineering Congress and Exposition. ASMEDC, 2008. http://dx.doi.org/10.1115/imece2008-68149.

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Recent studies have shown that the use of winglets in aircrafts wing tips have been able to reduce fuel consumption by reducing the lift-induced drag caused by wing tip vortex. This paper presents a 3-D numerical study to analyze the drag and lift forces, and the behavior of the vortexes generated in the wing tips from a modified commercial Boeing aircraft 767-300/ER. This type of aircraft does not contain winglets to control the wing tip vortex, therefore, the aerodynamic effects were analyzed adding two models of winglets to the wing tip. The first one is the vortex diffuser winglet and the
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Hallez, Raphael, Claudio Colangeli, Jacques Cuenca, and Laurent De Ryck. "Impact of electric propulsion on aircraft noise – all-electric light aircrafts case study." In 2018 AIAA/IEEE Electric Aircraft Technologies Symposium. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4982.

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Kupciuniene, Kristina, and Robertas Alzbutas. "External Events Importance for Safety of the Ignalina Nuclear Power Plant." In 16th International Conference on Nuclear Engineering. ASMEDC, 2008. http://dx.doi.org/10.1115/icone16-48230.

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Probabilistic risk analysis of external events impact on the safety important systems of Ignalina nuclear power plant (NPP) is performed. At first, the methodology was established for screening out external events, which impact on Ignalina NPP safety is not significant. In order to estimate probabilities of external events occurrences the statistical data were collected, mathematical models were constructed and probabilities of these events occurrences were determined. For risk estimation, the following external events were studied: forest fires, external floods, aircraft crash, seismic events
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Reports on the topic "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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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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Ehst, David A. Commercial Aircraft Protection. Office of Scientific and Technical Information (OSTI), 2016. http://dx.doi.org/10.2172/1346573.

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Chapa, Mark A. Predicting Aircraft Availability. Defense Technical Information Center, 2013. http://dx.doi.org/10.21236/ada580972.

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ARMY WAR COLL CARLISLE BARRACKS PA. Aircraft Rotor Surface Coating Qualification Testing Aircraft Rotor Surface Coating. Defense Technical Information Center, 2006. http://dx.doi.org/10.21236/ada481301.

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Simoncic, Adam D. Aircraft Block Speed Calculations for JOSAC/USTRANSCOM Aircraft Using Linear Regression. Defense Technical Information Center, 2013. http://dx.doi.org/10.21236/ada580613.

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Teague, Edward, Jr Kewley, and Robert H. Swarming Unmanned Aircraft Systems. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada488664.

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K. Ashley. Identification of Aircraft Hazards. Office of Scientific and Technical Information (OSTI), 2006. http://dx.doi.org/10.2172/899282.

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