Relevant bibliographies by topics / Aircraft analysis

Contents

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

Academic literature on the topic 'Aircraft analysis'

Author: Grafiati
Published: 4 June 2021
Last updated: 3 February 2022

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Journal articles on the topic "Aircraft analysis"

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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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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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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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Reddy, D. Ramana, M. V. Aditya Nag, and M. S. N. Gupta. "Stress and Deformation Analysis of Aircraft's Fuel Tank under Different Inertia Load Cases in Addition to a Static Test Pressure Using FEA." Advanced Materials Research 1115 (July 2015): 527–30. http://dx.doi.org/10.4028/www.scientific.net/amr.1115.527.

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In the modern era the aerospace technology plays a very significant role in the development of the mankind. The evolution of the light weight aircraft has a special focus in the present industrial trends. Several research organizations are in the process of developing Light Weight Aircraft, which is ideally suited for civil transport, aerial survey, training etc. This Light Weight Aircrafts are to be designed accordance to Federal Aviation Regulations part 23 (FAR-23). This paper deals with the analysis of the Aircraft's Fuel Tank under variable conditions. The analysis of aircraft fuel tank i
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Sutiawan, Sutiawan, Dena Hendriana, Hanny J. Berchmans, Henry Nasution, and Gembong Baskoro. "Design and Analysis of Warning System for Aircraft Wingtip Proximity to Hangar Column using Ultrasonic Sensor." Proceedings of The Conference on Management and Engineering in Industry 2, no. 1 (2020): 7–10. http://dx.doi.org/10.33555/cmei.v2i1.33.

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Aircraft maintenance is using very large hangar as a place to work on the aircrafts and the hangar can fit several aircrafts at the same time. The aircrafts are moved using tow cars in and out of the hangar. The hangar is so big that it requires columns for its structure and these columns present risk to the aircrafts for having wingtip collitions during towing in and out of the hangar. In this study, warning system for aircraft wingtip proximity to the hangar columns is designed. This warning system is using ultrasonic sensors attached to the columns and controlled by Arduino micro processor
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Janeba-Bartoszewicz, Edyta, and Adam Rojewski. "Analysis of hazards occurring during the use of hydrazine." WUT Journal of Transportation Engineering 125 (June 1, 2019): 37–43. http://dx.doi.org/10.5604/01.3001.0013.6493.

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The article presents the safety issue bonded to the Polish Air Force F-16 multirole aircraft. The authors pointed out the issue of fuel used for emergency supply system of these aircrafts. The paper emphasized the fact that these aircrafts require special fuel with designation H-70, which is 70% aqueous solution of toxic hydrazine. For this reason, the rescue services of Polish Air Force bases where Polish F-16 are stationed had to be adjusted accordingly. Just as importantly authors noticed that in the event of an emergency landing of this aircraft at different airports can receive difficulti
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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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FUĆ, Paweł, Monika KARDACH, and Marta MACIEJEWSKA. "Analysis of the availability of aircrafts with alternative propulsions." Combustion Engines 179, no. 4 (2019): 220–25. http://dx.doi.org/10.19206/ce-2019-437.

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Global air traffic doubles every 15 years. Therefore, aviation emission grows as well. It is advisable to look for an alternative aircrafts’ propulsion for both commercial and general aviation (usually flying closer to the ground). There are many prototypes proposed by homemade projects, through companies wanting to extend their offer. There are also several more advanced constructions ready to self-set or serially produced. In the article the main topic are electric aircrafts as an example of possibility to reduce the toxic compounds emission. According to the analysis some of companies speci
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Kumar, Sachin. "Computational Analysis for Random Winglet Designs on Light Aircraft." Journal of Advanced Research in Mechanical Engineering and Technology 05, no. 01 (2018): 01–16. http://dx.doi.org/10.24321/2454.8650.201801.

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Zhou, Hong, Zhan Xue Wang, and Xiao Bo Zhang. "Areo-Engine Cycle Parametric Analysis and Installed Performance Calculation Based on Aircraft Flight Mission." Applied Mechanics and Materials 482 (December 2013): 277–81. http://dx.doi.org/10.4028/www.scientific.net/amm.482.277.

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The aircraft/engine integration design numerical simulation model was established. The engine design performance specifications were obtained by calculating aircraft lift-drag characteristics, mission analysis, constraint analysis. Combining engine cycle parametric analysis with installation loss computing, the engine performance parameters can be found, which meet the aircraft flight envelope performance requirements. Taking double bypass variable cycle engine as an example to check the model, the results show that the variable cycle engine can meet aircrafts thrust and fuel consumption deman
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Dissertations / Theses on the topic "Aircraft analysis"

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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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Cuppernull, Michael J. 1957. "Aircraft remanufacturing process improvement analysis." Thesis, Massachusetts Institute of Technology, 1999. http://hdl.handle.net/1721.1/88823.

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Behroozi, Mohammad H. "Finite element analysis of aircraft tyres." Thesis, University of Birmingham, 2014. http://etheses.bham.ac.uk//id/eprint/5390/.

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In this thesis, the Finite Element (FE) Analysis of aircraft tyres is presented. The modelling and simulations of detailed construction of tyre enable tyre manufacturers to evaluate new designs and development before a prototype is fabricated, and aim to reduce the research costs and efforts to optimise the current tyre design of tyres. The material properties is key in the FE modelling and analysis, a number of sample from the rubber compounds and reinforcement were used to characterise the elastic, hyperelastic and viscoelastic behaviour of material. In this research, two aircraft tyres were
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Magnani, Federico. "Analysis of aircraft cirrus clouds spectral measurements." Bachelor's thesis, Alma Mater Studiorum - Università di Bologna, 2019.

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In questa tesi vengono descritte le proprietà dell’atmosfera terrestre nel lontano infrarosso (FIR) e il loro impatto climatico. Negli ultimi anni sempre più attenzione è stata posta nella ricerca in questo campo e sono stati sviluppati strumenti e metodi di analisi innovativi, come dimostrato dalla nascita della missione Far-infrared-Outgoing-Radiation Understanding and Monitoring (FORUM) che propone il lancio di un satellite attrezzato con strumenti FIR. Quasi il 45% dell’energia emessa dal pianeta è portata da onde nel FIR, attraverso il meccanismo del trasferimento radiativo: poichè l’atmo
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Baghdadi, Nadjib. "Bifurcation and continuation analysis : flexible aircraft dynamics." Thesis, University of Bristol, 2011. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.539769.

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Muller, Kurt W. "Analysis of a semi-tailless aircraft design." Thesis, Monterey, California. Naval Postgraduate School, 2002. http://hdl.handle.net/10945/6044.

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Approved for public release; distribution is unlimited<br>Many unique aircraft configurations came out of Germany in World War II, one of these was the Blohm and Voss BV P 208. By using longitudinal and directional control surfaces located outboard of the wing tips they are removed from the downwash of the main wing. Additionally, the result is fewer component surfaces with less total surface area, thereby reducing both friction and interference drag and manufacturing cost. The configuration should lend itself well to low-observability, making it a good stealth candidate. The P 208,
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Rubin, Felix. "Modelling & Analysis of a TiltWing Aircraft." Thesis, KTH, Flygdynamik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-244832.

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The aim of this report is the investigation of a hybrid vertical take-off and landing (VTOL) tilt wing aircraft which is in development at the company Dufour Aerospace. Using a model, programmed in MATLAB® different stages of flight can be simulated and investigated. Maininvestigation area of this report is the transition between cruise and hover conditions of the aircraft.The simulation is based on the six-degree-of-freedom nonlinear equations of motion for aircraft modified for tilt wing operation. The model characteristics have been determined using various CFD programs, wind tunnel data, a
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Dowdle, Aidan Patrick. "A Requirements analysis methodology for turboelectric aircraft." Thesis, Massachusetts Institute of Technology, 2017. http://hdl.handle.net/1721.1/111912.

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Thesis: S.M., Massachusetts Institute of Technology, Department of Electrical Engineering and Computer Science, 2017.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (pages 81-82).<br>The aviation industry today requires novel aircraft technology to provide for its rapidly growing demand. Of the many aircraft technologies being proposed, turboelectric is of particular interest for commercial-sized aircraft. Turboelectric propulsion enables novel airframe configurations, boundary layer ingestion, and distributed propulsion, each of which can reduce the amount of
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Poudel, Minesh. "Aircraft emergency evacuation : analysis, modelling and simulation." Toulouse 2, 2008. http://www.theses.fr/2008TOU20026.

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Cette thèse s’intéresse à l’évacuation d’urgence des avions et plus particulièrement à la conception d’un simulateur numérique capable de représenter de façon réaliste ce processus afin de contribuer à la certification de configurations et de procédures d’évacuation d’urgence pour les avions gros porteurs. Cette thèse est composée de deux grandes parties. Dans la première partie, il s’est agi d’identifier le problème, de réaliser un état de l’art et de caractériser le comportement des passagers pendant l’évacuation. Dans la deuxième partie de la thèse il s’est agi de concevoir les élément cons
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Erlandsson, Tina. "Situation analysis for fighter aircraft combat survivability." Licentiate thesis, Örebro universitet, Akademin för naturvetenskap och teknik, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:oru:diva-20544.

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Fighter pilots operate in environments where an erroneous decision may have fatal consequences. A tactical decision support system (TDSS) could aid the pilots to analyze the situation and make correct decisions. The TDSS can, for instance, highlight important information and suggest suitable actions. The aim of this thesis is to provide a situation analysis model of combat survival that can be utilized in a TDSS. The first part of this thesis describes an analysis of what the model needs to describe and how it can be used. It is concluded that the model should evaluate the outcome of different
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Books on the topic "Aircraft analysis"

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Shaw, Robert J. NASA's aircraft icing analysis. National Aeronautics and Space Administration, 1986.

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Walters, James M. Aircraft accident analysis: Final reports. McGraw-Hill, 2000.

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Introduction to aircraft structural analysis. Butterworth-Heinemann, 2010.

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Curtis, Howard D. Fundamentals of aircraft structural analysis. Irwin, 1997.

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Donaldson, Bruce K. Analysis of aircraft structures: An introduction. 2nd ed. Cambridge University Press, 2008.

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Donaldson, Bruce K. Analysis of aircraft structures: An introduction. McGraw-Hill, 1993.

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Analysis of aircraft structures: An introduction. McGraw-Hill, 1993.

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Heller, H. Aircraft exterior noise measurement and analysis techniques. Agard, 1991.

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Holloway, Stephen. Aircraft acquisition finance and airline credit analysis. Pitman, 1992.

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Ahlers, Mark F., ed. Aircraft Thermal Management: Integrated Energy Systems Analysis. SAE International, 2016. http://dx.doi.org/10.4271/pt-178.

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Book chapters on the topic "Aircraft analysis"

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Sadraey, Mohammad H. "Aircraft performance analysis using numerical methods and MATLAB®." In Aircraft Performance. CRC Press, 2017. http://dx.doi.org/10.1201/9781315366913-10.

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Vasigh, Bijan, and Zane C. Rowe. "Analysis of aircraft leasing." In Foundations of Airline Finance. Routledge, 2019. http://dx.doi.org/10.4324/9780429429293-12.

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Howe, Denis. "Parametric Analysis and Optimisation." In Aircraft Conceptual Design Synthesis. John Wiley & Sons, Ltd, 2014. http://dx.doi.org/10.1002/9781118903094.ch8.

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Howe, Denis. "Analysis of Concept Design." In Aircraft Conceptual Design Synthesis. John Wiley & Sons, Ltd, 2014. http://dx.doi.org/10.1002/9781118903094.ch9.

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Rose, L. R. F. "Theoretical analysis of crack patching." In Bonded Repair of Aircraft Structures. Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2752-0_5.

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Gudmundsson, Snorri. "Aircraft Cost Analysis." In General Aviation Aircraft Design. Elsevier, 2014. http://dx.doi.org/10.1016/b978-0-12-397308-5.00002-7.

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Gudmundsson, Snorri. "Aircraft Weight Analysis." In General Aviation Aircraft Design. Elsevier, 2014. http://dx.doi.org/10.1016/b978-0-12-397308-5.00006-4.

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Gudmundsson, Snorri. "Aircraft Drag Analysis." In General Aviation Aircraft Design. Elsevier, 2014. http://dx.doi.org/10.1016/b978-0-12-397308-5.00015-5.

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Kritzinger, Duane. "Functional Hazard Analysis." In Aircraft System Safety. Elsevier, 2017. http://dx.doi.org/10.1016/b978-0-08-100889-8.00003-9.

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Kritzinger, Duane. "Fault tree analysis." In Aircraft System Safety. Elsevier, 2017. http://dx.doi.org/10.1016/b978-0-08-100889-8.00004-0.

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Conference papers on the topic "Aircraft analysis"

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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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Almeida, I. M., A. I. B. B. Paraguay, and M. L. A. B. Reichmann. "Aircraft accident in Brazil: Boeing vs. Legacy?" In RISK ANALYSIS 2008. WIT Press, 2008. http://dx.doi.org/10.2495/risk080471.

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Grose, D. "Reengineering the aircraft design process." In 5th Symposium on Multidisciplinary Analysis and Optimization. American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-4323.

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Kettering, Mark, and Daniel Biezad. "The roadable aircraft design project." In 6th Symposium on Multidisciplinary Analysis and Optimization. American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-4071.

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BUSH, LANCE, CHRISTOPHER LENTZ, JOHN REHDER, J. NAFTEL, and JEFFREY CERRO. "Structural weights analysis of advanced aerospace vehicles using finite element analysis." In Aircraft Design and Operations Meeting. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2130.

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Xue, Zhendan, and Christina Bloebaum. "Experimental Design Based Aircraft Egress Analysis Using VacateAir - An Aircraft Evacuation Simulation Model." In 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-6061.

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Provost, M. J. "Kalman filtering applied to time series analysis." In Aircraft Airborne Condition Monitoring. IEE, 2003. http://dx.doi.org/10.1049/ic:20030003.

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Aygün, Mehmet Murat, Yiğit Tascıoğlu, Gürsoy Genç, and Mustafa Altunay. "Electro-Mechanical Control Loading System for Rotary Wing Aircraft Simulators." In ASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/esda2014-20495.

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The focus of this paper is on the development of a high-fidelity electro-mechanical Control Loading System (CLS) for a rotary wing aircraft simulator. CLS is one of the major components of a flight simulator. It is used for providing realistic force feedback to pilots. The pilot in a real aircraft feels the forces acting on control surfaces through cockpit controls. During simulation, these forces are produced by CLS actuators. For this reason, CLS must behave exactly like the aircraft control hardware, statically and dynamically. The fidelity of the force feel simulation is a key criterion fo
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Holden, Carren, and Andy Keane. "Visualization Methodologies in Aircraft Design." In 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-4449.

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TAYLOR, III, ARTHUR, GENE HOU, and VAMSHI KORIVI. "Sensitivity analysis, approximate analysis, and design optimization for internal and external viscous flows." In Aircraft Design and Operations Meeting. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3083.

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Reports on the topic "Aircraft analysis"

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Hunter, David R., and Eugene F. Burke. Meta Analysis of Aircraft Pilot Selection Measures. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada253387.

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Hans Jordan. Analysis of Aircraft Crash Accident for WETF. Office of Scientific and Technical Information (OSTI), 2001. http://dx.doi.org/10.2172/775921.

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Wells, S. P., K. S. Cozart, M. B. Mitchell, and R. D. Dodsworth. Aircraft Hangar Fire Threat Study and Analysis. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada344628.

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Boyd, K. L., and S. Krishnan. Evaluation of Aircraft Structural Repair/Analysis Codes. Defense Technical Information Center, 1996. http://dx.doi.org/10.21236/ada388127.

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Seaton, Dave I. Task Analysis - Aircraft Structural Maintenance AFSC 458X2. Defense Technical Information Center, 1989. http://dx.doi.org/10.21236/ada218489.

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CAS INC HUNTSVILLE AL. Advanced Integrated Aircraft Survivability Equipment Analysis. Addendum. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada280649.

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K. Ashley. Frequency Analysis of Aircraft hazards for License Application. Office of Scientific and Technical Information (OSTI), 2006. http://dx.doi.org/10.2172/899283.

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NEW YORK UNIV NY SCHOOL OF MEDICINE. Passive Aircraft Status System (PASS): Design and Analysis. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada388961.

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Gong, C. Finite Element Analysis of Laser Residual Stress Analysis for 7050 Aircraft Aluminum. Office of Scientific and Technical Information (OSTI), 1998. http://dx.doi.org/10.2172/10102776.

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Tuegel, Eric J., Robert P. Bell, Alan P. Berens, et al. Aircraft Structural Reliability and Risk Analysis Handbook Volume 1: Basic Analysis Methods. Defense Technical Information Center, 2013. http://dx.doi.org/10.21236/ada587824.

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