Relevant bibliographies by topics / Aircraft

Contents

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

Academic literature on the topic 'Aircraft'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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Journal articles on the topic "Aircraft"

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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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DUEE, Raphael, Alexis MARTIN, Hugo VASSEUR, and Jean-Frédéric DESJARDINS. "Aircraft automatic detection on Station7hz interface using signal processing and artificial intelligence - ACOUDET - First method." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 270, no. 6 (2024): 5767–75. http://dx.doi.org/10.3397/in_2024_3644.

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The global project is to design a automatic noise event detection and classification system in real time using signal processing and artificial intelligence (AI). The first phase focuses on transport noise (aircrafts, trains, road vehicles, etc.). Secondly, the plan is to extend detection to construction site noise and any natural or life sources. This paper presents the first method developed to detect audible aircrafts pass-by. It focused on the development of a prototype detection algorithm, its results in situ conditions, and insights on future developments to create a robust aircraft and
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Olugbeji, Jemitola P., Okafor E. Gabriel, and Godwin Abbe. "Wing Thickness Optimization for Box Wing Aircraft." Recent Patents on Engineering 14, no. 2 (2020): 242–49. http://dx.doi.org/10.2174/1872212113666190206123755.

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Background: In the interest of improving aircraft performance, studies have highlighted the benefits of Box wing configurations over conventional cantilever aircraft configuration. Generally, the greater an aircraft's average thickness to chord ratio (τ), the lower the structural weight as well as volumetric capacity for fuel. On the other hand, the lower the ., the greater the drag reduction. A review of patents related to the Box-wing aircraft was carried out. While methodologies for optimizing wing thickness of conventional aircrafts have been studied extensively, limited research work exis
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Yao, Dongdong, and Qunli Xia. "Finite-Time Convergence Guidance Law for Hypersonic Morphing Vehicle." Aerospace 11, no. 8 (2024): 680. http://dx.doi.org/10.3390/aerospace11080680.

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Aiming at the interception constraint posed by defensive aircrafts against hypersonic morphing vehicles (HMVs) during the terminal guidance phase, this paper designed a guidance law with the finite-time convergence theory and control allocation methods based on the event-triggered theory, achieving evasion of the defensive aircraft and targeting objectives for a morphing vehicle in the terminal guidance phase. Firstly, this paper established the aircraft motion model; the relative motion relationships between HMV, defensive aircraft, and target; and the control equations for the guidance syste
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Hong, Wei Jiang, and Dong Li Ma. "Influence of Control Coupling Effect on Landing Performance of Flying Wing Aircraft." Applied Mechanics and Materials 829 (March 2016): 110–17. http://dx.doi.org/10.4028/www.scientific.net/amm.829.110.

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As flying wing aircraft has no tail and adopts blended-wing-body design, most of flying wing aircrafts are directional unstable. Pitching moment couples seriously with rolling and yawing moment when control surfaces are deflected, bringing insecurity to landing stage. Numerical simulation method and semi-empirical equation estimate method were combined to obtain a high aspect ratio flying wing aircraft’s aerodynamic coefficients. Modeling and simulation of landing stage were established by MATLAB/Simulink. The control coupling effect on lift and drag characteristics and anti-crosswind landing
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Rogalski, Tomasz, and Boguslaw Dołęga. "THE METHOD OF EVALUATION OF THE AIRCRAFT CONTROL SYSTEM." Aviation 9, no. 2 (2005): 29–34. http://dx.doi.org/10.3846/16487788.2005.9635901.

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The dynamical development of general aviation demands compilation of new aircraft control methods. Those methods allow people without special airborne qualifications to pilot these aircrafts. The main goals of such a control system are to reduce a pilot's load, to improve control precision, and to protect an aircraft against dangerous situations. There are many criterions applied to grading and describing an aircraft's flying characteristics and the handling qualities of general aviation airplanes equipped with classical mechanical control systems. But a modern, small, transport aircraft shoul
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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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Xie, Naiming. "Estimating civil aircraft’s research and manufacture cost by using grey system model and neural network algorithm." Grey Systems: Theory and Application 5, no. 1 (2015): 89–104. http://dx.doi.org/10.1108/gs-12-2014-0054.

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Purpose – The purpose of this paper is to propose novel civil aircraft cost parameters’ selection method and novel cost estimation approach for civil aircraft so as to effectively simulate or forecast civil aircraft cost under poor information and small sample. Design/methodology/approach – Based on existent cost estimation indexes, this paper summarized civil aircraft research and manufacturing cost impact index system and adopted grey relational model to select most important impact factors. Consider civil aircrafts’ cost information could not be easily collected, the author must estimate th
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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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Sharma, Vaibhav. "Fanwing Aircraft- Scope as an Agricultural Aircraft." International Journal for Research in Applied Science and Engineering Technology 9, no. VIII (2021): 603–7. http://dx.doi.org/10.22214/ijraset.2021.37436.

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The objective of this paper is to apply the concept of fan wing to agricultural aircrafts which are conventionally fixed wings aircrafts or multi-rotor drones. Fan wing is capable of producing good amount of lift at a sufficiently low speed without stalling, thus is apt for agricultural processes of irrigation, spraying pesticides, etc. Fan wing has a special ability that it doesn’t stalls (for the practical range of AOA), making this spraying method reliable. A fanwing aircraft is modelled using CATIA V5 and the flow visualizations for the same are performed on the ANSYS. This aircraft is the
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Dissertations / Theses on the topic "Aircraft"

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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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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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Black, Gary Douglas. "Aircraft configuration study for experimental 2-place aircraft and RPVs." Thesis, Monterey, California : Naval Postgraduate School, 1990. http://handle.dtic.mil/100.2/ADA227604.

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Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, March 1990.<br>Thesis Advisor(s): Howard, Richard M. Second Reader: Hauser, James P. "March 1990." Description based on signature page as viewed on August 25, 2009. DTIC Descriptor(s): Aerodynamic configurations, remotely piloted vehicles, military aircraft, lightweight, research aircraft, canard configurations, wings, aerodynamic drag, computer programs, scaling factor, aerodynamic stability, performance(engineering), comparison, microcomputers, trade off analysis, aeronautical engineering, theses. DTIC Identifier(s): Pushe
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Wan, Husain Wan Mohd Sufian Bin. "Maintainability prediction for aircraft mechanical components utilising aircraft feedback information." Thesis, Cranfield University, 2011. http://dspace.lib.cranfield.ac.uk/handle/1826/7272.

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The aim of this research is to propose an alternative approach to determine the maintainability prediction for aircraft components. In this research, the author looks at certain areas of the maintainability prediction process where missteps or misapplications most commonly occur. The first of these is during the early stage of the Design for Maintainability (DfMt) process. The author discovered the importance of utilising historical information or feedback information. The second area is during the maintainability prediction where the maintenance of components is quantified; here, the author p
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Ionescu, Irina Gabriela. "Aircraft noise regulation." Thesis, McGill University, 2004. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=82660.

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Aircraft noise is one of the most controversial environmental concerns in the aviation industry, partly due to the difficulty in harmonizing countries' regulation regarding this issue. The purpose of this thesis is to analyze the ways in which aircraft noise is regulated at the national and international levels, and to compare the legislative responses to aircraft noise issues in Europe and North America. Each of the four main chapters of the thesis takes into consideration a different aspect of the problem. The first chapter describes the objective and subjective ways of measuring airc
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彭遠輝 and Yuen-fai Alson Pang. "Managing aircraft noise." Thesis, The University of Hong Kong (Pokfulam, Hong Kong), 2002. http://hub.hku.hk/bib/B31255280.

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Wagner, Michael J. "AEW aircraft design." Thesis, Monterey, California. Naval Postgraduate School, 1992. http://hdl.handle.net/10945/23815.

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Books on the topic "Aircraft"

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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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Steve, Parker. Aircraft. Miles Kelly, 2009.

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Book chapters on the topic "Aircraft"

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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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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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Schmitt, Dieter, and Volker Gollnick. "Aircraft Characteristics." In Air Transport System. Springer Vienna, 2015. http://dx.doi.org/10.1007/978-3-7091-1880-1_5.

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Schmitt, Dieter, and Volker Gollnick. "Aircraft Manufacturer." In Air Transport System. Springer Vienna, 2015. http://dx.doi.org/10.1007/978-3-7091-1880-1_6.

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Conference papers on the topic "Aircraft"

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Kaye, Jordan, Mark Robeson, and Nathaniel Bordick. "Aircraft Survivability Rating." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9603.

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Sikorsky Aircraft and the US Army's Aviation Development Directorate - Aviation Applied Technology Directorate (ADD–AATD), as part of the co-funded Combat Tempered Aircraft Demonstration (CTPD), have developed a new methodology to rate aircraft survivability in a hostile environment. The new rating system incorporates combat reports to expand upon current vulnerability analyses used to evaluate an aircraft's ability to survive a hostile attack. The current method of evaluating an aircraft only takes into account one threat per analysis and does not accommodate combat statistics for attack outc
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Minkova-Walker, Mirela, and Jacob Cook. "Automating Tilt-Wing Aircraft: A Comprehensive Framework." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-105.

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Dufour Aerospace designs and manufactures an automated tilt-wing aircraft for critical cargo delivery missions. Emphasizing operational efficiency, the platform integrates path generation and tracking techniques tailored for the unique dynamics of tilt-wing flight and builds upon the existing lower level control. While there exist a myriad of methods for high-level aircraft automation ranging from PID to MPC, they often require a trade-off between complexity and the capability to handle non-linear dynamics of the system they are controlling. Hence, a lightweight, deterministic geometric path g
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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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Prather, William. "Coupling to aircraft and aircraft hardening." In 2008 IEEE International Symposium on Electromagnetic Compatibility - EMC 2008. IEEE, 2008. http://dx.doi.org/10.1109/isemc.2008.4652198.

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Bickmeier, Laura, and Ronald Ankner. "Aircraft to Aircraft Collision Risk Modeling." In 2024 Integrated Communications, Navigation and Surveillance Conference (ICNS). IEEE, 2024. http://dx.doi.org/10.1109/icns60906.2024.10550662.

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Robinson, Derek, James Bonn, and Daniel Murphy. "Aircraft Turnaround Times and Aircraft Itinerary Generation." In 11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-6848.

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Szurgyi, Stephen, Sanjiv Shresta, Dejan Neskovic, James DeArmon, and Scott Williams. "Analysis of observed aircraft-to-aircraft separations." In 2008 Integrated Communications, Navigation and Surveillance Conference (ICNS). IEEE, 2008. http://dx.doi.org/10.1109/icnsurv.2008.4559166.

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Mlynarčík, Martin, and Michal Janovec. "Conversion of passenger aircraft to cargo versions." In Práce a štúdie. University of Žilina, 2022. http://dx.doi.org/10.26552/pas.z.2022.1.23.

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In this presented paper on the topic of conversion of passenger aircrafts to cargo versions, the use of this transformation in the modern history of aviation is analyzed and the current situation is analyzed. For a better introduction to the issue, the introductory part defines the fundamental terms and explains the conversion itself and its various stages. The paper also discusses the companies that provide services for the actual conversion of passenger aircraft and the location where this process takes place. The paper is further supplemented by individual types of aircraft, which are divid
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Haluzová, Kristína, Martin Bugaj, and Michal Hrúz. "Aircraft airfoils." In Práce a štúdie. University of Žilina, 2023. http://dx.doi.org/10.26552/pas.z.2023.1.01.

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This work deals with the airfoils of aircraft. First of all, it focuses on the general properties of wings. Furthermore, the work deals with the issue of various types of wing shape and compares individual shapes of airfoils, their properties and gradual development. Next, current wings of commercial aircraft are described, dealing with the materials used, types of winglets, mechanization of the wing and also different uses of the airfoils. The work also describes and compares wings of two famous commercial airliners – Boeing 737-800 and Airbus A320-200. In the end, the work also focuses on va
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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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Reports on the topic "Aircraft"

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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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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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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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Muth, Thomas R., and William H. Peter. Aircraft Propeller Hub Repair. Office of Scientific and Technical Information (OSTI), 2015. http://dx.doi.org/10.2172/1185928.

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