Relevant bibliographies by topics / Aircraft application

Contents

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

Academic literature on the topic 'Aircraft application'

Author: Grafiati
Published: 4 June 2021
Last updated: 9 March 2023

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Journal articles on the topic "Aircraft application"

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Yao, Jin Bo, Yue Ming Yang, Qin Yu Yang, Xiu Juan Liu, and Dun Jin. "Application of LED Light Source in the Flow Imaging." Applied Mechanics and Materials 380-384 (August 2013): 219–22. http://dx.doi.org/10.4028/www.scientific.net/amm.380-384.219.

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Aircraft in flight, such as supercooled water droplets encountered icing conditions suitable for the external environment, the relevant parts of the body will freeze, making the aircraft's aerodynamic performance deterioration, severe endanger flight safety, in addition, the aircraft parked in the open winter months , there will be icing, you need to clean up before takeoff. We should grasp the mechanism of aircraft icing, environmental factors and easy to freeze parts of the body. This paper presents a simulation using the wind tunnel icing device icing wind tunnel simulations can reproduce the real situation of aircraft icing, for guiding practice and got good results.
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Min, Kyung Ju, and Ho Sung Lee. "Composite Materials Characterization for Aircraft Application." Materials Science Forum 857 (May 2016): 169–73. http://dx.doi.org/10.4028/www.scientific.net/msf.857.169.

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Various composite materials have been developed for many of aircrafts feature and it is important to establish the composite materials characterization procedure based on the airworthiness requirement. Since properties of composites are a function of the properties of the constituent phases, their relative amounts, and processing methods, the overall processing must be carefully evaluated. This paper presents a composite materials evaluation procedure for composite aircraft and provide the effective statistical allowable to be approved by airworthiness certification agency. All material, specimens, fixtures and test results contained within this study were traceable and approved by the agency. In this study 8 different mechanical properties are obtained for 4 environmental conditions from 5 batches for robust sampling. By using modified coefficient of variation, the B-basis value of 0°tensile strength of carbon/epoxy unidirectional composite for elevated temperature/wet condition increases from 2,291MPa to 2,331MPa. The result would be applied to qualify domestic composite materials for aircraft within the level of a global standard.
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Alestra, Stephane, Cristophe Bordry, Cristophe Brand, Evgeny Burnaev, Pavel Erofeev, Artem Papanov, and Cassiano Silveira-Freixo. "Application of Rare Event Anticipation Techniques to Aircraft Health Management." Advanced Materials Research 1016 (August 2014): 413–17. http://dx.doi.org/10.4028/www.scientific.net/amr.1016.413.

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Generally faults in complex technical systems (such as aircrafts) can be considered as rare events. In this paper we apply classification techniques to problem of rare events anticipation and demon-strate the approach to predictive maintenance of aircrafts through the real-world test cases from aircraft operations based on the data granted by AIRBUS.
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Broer, Agnes A. R., Rinze Benedictus, and Dimitrios Zarouchas. "The Need for Multi-Sensor Data Fusion in Structural Health Monitoring of Composite Aircraft Structures." Aerospace 9, no. 4 (March 30, 2022): 183. http://dx.doi.org/10.3390/aerospace9040183.

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With the increased use of composites in aircraft, many new successful contributions to the advancement of the structural health monitoring (SHM) field for composite aerospace structures have been achieved. Yet its application is still not often seen in operational conditions in the aircraft industry, mostly due to a gap between research focus and application, which constraints the shift towards improved aircraft maintenance strategies such as condition-based maintenance (CBM). In this work, we identify and highlight two key facets involved in the maturing of the SHM field for composite aircraft structures: (1) the aircraft maintenance engineer who requires a holistic damage assessment for the aircraft’s structural health management, and (2) the upscaling of the SHM application to realistic composite aircraft structures under in-service conditions. Multi-sensor data fusion concepts can aid in addressing these aspects and we formulate its benefits, opportunities, and challenges. Additionally, for demonstration purposes, we show a conceptual design study for a fusion-based SHM system for multi-level damage monitoring of a representative composite aircraft wing structure. In this manner, we present how multi-sensor data fusion concepts can be of benefit to the community in advancing the field of SHM for composite aircraft structures towards an operational CBM application in the aircraft industry.
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Wu, Yue. "Application of aluminum alloy in aircraft." Journal of Physics: Conference Series 2228, no. 1 (March 1, 2022): 012024. http://dx.doi.org/10.1088/1742-6596/2228/1/012024.

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Abstract From the perspective of aircraft manufacturing industry, aluminum alloy is a material with high practicability. It has the advantages of simple process, convenient processing, good forming performance, high durability and reliability, convenient maintenance, taking into account a series of advantages such as corrosion resistance, high strength, high stiffness and low cost. Applying it to the aircraft manufacturing industry can not only effectively control the cost of aircraft manufacturing, but also give full play to the material properties, improve the service performance of various aircraft components, improve the aircraft manufacturing level, and meet the development needs of the aircraft manufacturing industry. Based on the application case of aluminum alloy in aircraft, this paper studies the application of aluminum alloy in aircraft, and then puts forward the existing problems and solutions of aluminum alloy in aircraft, in order to provide valuable reference for the development of material field and aircraft manufacturing field in China.
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Bimo, Emanuel Ario, Eka Prabawa, Esra Kriahanta Sembiring, Oktaheroe Ramsi, Sjafrie Sjamsoeddin, Purnomo Yusgiantoro, and I. Wayan Midhio. "Application of AHP and PESTEL-SWOT Analysis on The Study of Military Amphibious Aircraft Acquisition Decision Making in Indonesia." Technium Social Sciences Journal 27 (January 8, 2022): 837–53. http://dx.doi.org/10.47577/tssj.v27i1.5414.

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Indonesia’s characteristics as an archipelagic state along with the increase of traditional and non-traditional threats in Indonesia require the ownership of military amphibious aircraft to oversee its maritime territories and perform logistics distribution to remote areas with minimum accessibility, especially its outermost islands. This study applied a combination of analytic hierarchy process (AHP), Political, Economic, Social, Techonology, Environment, and Legal (PESTEL) and Strength, Weakness, Opportunity, and Threat (SWOT) analysis to conduct a structured, systematic, measurable, and comprehensive decision-making process for selecting military amphibious aircraft and prescribe strategic recommendations on the acquisition plan. By using 3 criteria, 14 sub-criteria, and 3 alternative aircraft models, the results of AHP analysis showed that the Beriev Be-200 aircraft are the most preferred aircraft by the Indonesian users. The results of PESTEL-SWOT analysis show that good diplomatic relations between Indonesia and the manufacturer’s country of origin, users’ support to the plan, and user’s ability to adapt in operating and maintaining the aircraft support this decision. Meanwhile, limited fiscal capacity and domestic aircraft maintenance facilities/depots, as well as the risk of spare parts scarcity, have to be addressed for Indonesia to acquire its own military amphibious aircrafts.
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Loong, Ling Jin, Chockalingam Aravind Vaithilingam, Gowthamraj Rajendran, and Venkatkumar Muneeswaran. "Modelling and analysis of vienna rectifier for more electric aircraft applications using wide band-gap materials." Journal of Physics: Conference Series 2120, no. 1 (December 1, 2021): 012027. http://dx.doi.org/10.1088/1742-6596/2120/1/012027.

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Abstract This paper presents a comprehensive study on the switching effects of wide bandgap devices and the importance of power electronics in an aircraft application. Silicon (Si), silicon carbide (SiC), and gallium nitride (GaN) are wide bandgap devices that act as a power electronic switch in the AC-DC converter for More Electric Aircraft (MEA) applications. Therefore, it is important to observe their converting efficiency to identify the most suitable wide bandgap device among three devices for AC-DC converters in aircraft applications to provide high efficiency and high-power density. In this study, the characteristics of Si, SIC, and GaN devices are simulated using PSIM software. Also, this paper presents the performance of the Vienna rectifier for aircraft application. The Vienna rectifier using Si, SiC, and GaN devices are simulated using PSIM software for aircraft application. GaN with Vienna rectifier provides better performance than Si and SiC devices for aircraft applications among the three devices. It gives high efficiency, high power density, low input current THD to meet IEEE-519 standard, and high-power factor at mains.
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YOSHIDA, Osamu. "Bonded structure application for aircraft." Journal of the Japan Welding Society 60, no. 3 (1991): 212–18. http://dx.doi.org/10.2207/qjjws1943.60.212.

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MITSUHASHI, Kiyomichi, Ryozo SEO, and Masahiko YOKOTA. "Optical Technology Application in Aircraft." Journal of the Japan Society for Aeronautical and Space Sciences 36, no. 408 (1988): 18–25. http://dx.doi.org/10.2322/jjsass1969.36.18.

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Gramopadhye, Anand K., David Kraus, Pradeep Rao, and Daniel Jebaraj. "Application of Advanced Technology to Team Training." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 40, no. 21 (October 1996): 1072–76. http://dx.doi.org/10.1177/154193129604002106.

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Research on civil aircraft inspection and maintenance has shown the importance of teamwork in completing aircraft inspection and maintenance tasks. Training has been identified as one of the primary intervention strategies in improving team performance. If training is to be successful, it is clear that we need to provide aircraft maintenance technicians (AMTs) with training tools to help enhance their team skills and improve team performance within the aircraft inspection/maintenance environment. In response to this need, this paper describes the development of a computer-based multimedia team training tool, the Aircraft Maintenance Team Training (AMTT) software.
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Dissertations / Theses on the topic "Aircraft application"

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Chopra, Shubh. "Development of mobile applications for crop scouting with small unmanned aircraft systems." Kansas State University, 2017. http://hdl.handle.net/2097/35507.

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Master of Science
Department of Computer Science
Antonio R. Asebedo
Mitchell L. Neilsen
Small unmanned aircraft systems (sUAS) have been in commercial use since the1980’s and over 8-12% of its current uses are in the agricultural sector, but only involving limited uses like surveying, mapping and imaging, which is expected to increase to 47% according to AUVSI with the association of Artificial Intelligence over the next decade. Our research is one such effort to help farmers utilize advanced sUAS technology coupled with Artificial Intelligence and give them meaningful results in a widely used and user friendly interface, like a mobile application. The vision for this application is to provide a completely automated experience to the farmer for a repetitive and periodic analysis of his/her crops where all the instruction needed from the farmer is a push of a button on a one time configured application and ultimately providing results in seconds. This would help the farmer scout their crops, assess yield potential, and determine if additional inputs are needed for increasing grain yield and profit per acre. For making this application we focused on user-friendliness by abstracting crop algorithms, minimized necessary user inputs, and automate the construction of flight paths. Due to internet connection not always being available at farm fields, processing was kept to on-board compute systems and the mobile device to give live results to farmers without reliance on cloud-based analytics. The application is configured to work with DJI Aircraft using OpenCv for video processing and mobile vision, GIS and GPS data for accurate mapping, locating device, sUAS on the mobile application, and FFMPEG for encoding and decoding compressed video data. An algorithm developed by Precision-Ag Lab at the K-State Agronomy Department was implemented into the sUAS application for providing real time yield estimations and nitrogen recommendation algorithm for winter wheat.
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Simpson, Mark N. "The application of semi-active control technology to aircraft landing gear." Thesis, Loughborough University, 1988. https://dspace.lboro.ac.uk/2134/6764.

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The purpose of the research investigation was to study the application of semi-active control technology to the design of a suspension system to be used in a landing gear of a high speed military aircraft. A semi-active system was used because it will allow a system to be driven from the hydraulic systems already existing in the aircraft without extensive modification. The research work involved establishing a theoretical mathematical model for the semi-active damping system. This model involved a large number of non-linear dynamic phenomena and elements including a two-stage gas spring, lever geometry, break out friction, square law damping and the switching function needed to achieve the semi-active control. Validation of the model was carried out by means of an extensive study of the dynamic responses obtained from digital simulation. An extended programme of laboratory experiments was also carried out to confirm the theoretical and simulated results, and to demonstrate the potential benefits in performance which can be achieved with those obtained from standard and optimized passive suspension system. The experimental rig involved a physical model which used hydraulic elements of a general industry standard, but not specially approved for aircraft use. The apparatus was arranged to permit a considerable degree of freedom for implementing the control laws which facilitated the assessment of different control schemes and allowed, at the same time, the ready simulation of various passive damping arrangements. An extensive series of trials was carried out on the final design and involved frequency response tests and subjecting the experimental suspension to inputs obtained from a simulated runway profile. The profile simulation was a discrete representation of a particular runway chosen for its roughness which was characteristic of runways from which high-speed military aircraft operate. From the research investigation and these trials it was established that semi-active control of the damping function is superior to standard techniques and achieves a substantial reduction in the energy transmitted to the airframe during ground manoeuvres.
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Hyde, Richard Alden. "The application of robust control to VSTOL aircraft." Thesis, University of Cambridge, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.333330.

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Gill, Simon Adrain. "Application of human factors methodologies to aircraft maintainability." Thesis, University of Nottingham, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.537824.

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Plastow, Ian. "The development and application of computational methods for the design of aircraft fuel systems." Thesis, University of Bristol, 1994. http://hdl.handle.net/1983/1889c413-8033-41e3-8058-0c8f6e54bdf6.

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Maharaj, Davendra Yukteshwar. "The application of nonlinear control theory to robust helicopter flight control." Thesis, Imperial College London, 1994. http://hdl.handle.net/10044/1/7420.

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Bergkvist, Erik, and Tommy Sabbagh. "Smart Future Solutions for Maintenance of Aircraft : Enhancing Aircraft Maintenance at Saab AB." Thesis, Linköpings universitet, Industriell Produktion, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-176561.

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This master thesis has the purpose to analyse and identify smart efficient future solutions within the Maintenance, Repair and Overhaul (MRO) process for aircraft. The efficiency solutions, in form of new technologies and tools, should present a foundation that MRO suppliers can continue to develop to enhance and streamline their maintenance processes. The project was performed as a case study at the aerospace and defense company Saab AB in Linköping, where the company's MRO process was investigated. Through identifying possibilities and alternative technologies available today and in the near future, one continues to have a competitive and future-proof position in the market.  Through an own constructed course of action influenced from established methods, the thesis' purpose and aim was attained. The method was based on authentic approaches for case studies but also inspired by the so-called "Requirement Engineering". The combination of the methods resulted in a precise focus on the relevant subjects, together with a clear structure of the requirements on the technologies to reach a successful implementation. Through a detailed data collection comprised of study visits, interviews, literature studies, market analyses, and document reviews, multiple relevant technologies and requirement-lists for utilization were identified.  To concretize the use and potential improvements with the technologies, the project had the objective to develop a demonstrator with one of the technologies presented. The demonstrator should focus on minimizing the use of paper, which is a common problem among many market actors today. The most promising technology was considered to be a tablet application with an accommodated application. The selection of the tablet solution was based on the motivation that it is a well-established technology and a favorable first step from paperwork.  To conclude this master thesis, a tablet application was developed in Novacura Flow Studio, where the majority of the identified requirements were fulfilled. Beyond the demonstrator, an introduction and analysis of technologies, such as AR-glasses, voice guidance, additive manufacturing, and a digital twin, was presented.
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Dudgeon, Graham John William. "Individual channel analysis and design and its application to helicopter flight control." Thesis, University of Glasgow, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.325388.

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Bingham, Christopher Malcolm. "Application of variable structure control methods to actuator nonlinearities in aerospace systems." Thesis, Cranfield University, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.358823.

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Brown, Mark Anthony. "An investigation of three-dimensional displays for real-time, safety-critical command/control applications : with application to air traffic control." Thesis, Queen Mary, University of London, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.336445.

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Books on the topic "Aircraft application"

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J, Glassman Arthur, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Turbine design and application. Washington, DC: Scientific and Technical Information Program, National Aeronautics and Space Administration, 1994.

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Noor, Ahmed Khairy. Advances in contact algorithms and their application to tires. Hampton, Va: Langley Research Center, 1988.

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H, Mayrand C., and Lewis Research Center, eds. Multiple-purpose subsonic naval aircraft (MPSNA): Multiple application propfan study (MAPS). Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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H, Mayrand C., and Lewis Research Center, eds. Multiple-purpose subsonic naval aircraft (MPSNA): Multiple application propfan study (MAPS). Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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Julian, Wolkovitch, and Ames Research Center, eds. Application of the joined wing to tiltrotor aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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Maine, Richard E. Application of parameter estimation to highly unstable aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

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Sanjay, Garg, Merrill Walter C, and United States. National Aeronautics and Space Administration., eds. Neural network application to aircraft control system design. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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Vincent, James H. Application of modern control design methodology to oblique wing research aircraft. Palo Alto, Calif: Systems Control Technology, Inc., 1991.

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Nguyen, Hung Lee. Application of mixing-controlled combustion models to gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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Nguyen, Hung Lee. Application of mixing-controlled combustion models to gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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Book chapters on the topic "Aircraft application"

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Xiong, Duanqin, Xiaochao Guo, Guowei Shi, and Bai Yu. "Application of LED in Aircraft Lighting." In Proceedings of the 13th International Conference on Man-Machine-Environment System Engineering, 267–73. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-38968-9_30.

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Hasanzadeh, Mahdi, and Shahram Mahboubi Zadeh. "Advanced Fibrous Composites for Aircraft Application." In Materials, Structures and Manufacturing for Aircraft, 89–112. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-91873-6_4.

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Colvin, Edward L. "Chapter 24 | Commercial Aircraft." In Supplement to Corrosion Tests and Standards: Application and Interpretation, Second Edition, 385–91. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 2022. http://dx.doi.org/10.1520/mnl202ndsup20190033.

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Liu, Qingfeng, Xiaochao Guo, Fei Peng, Wanli Lou, Duanqin Xiong, Lei Yang, Yu Bai, and Yanyan Wang. "Application of Crisis Intervention After Aircraft Mishap." In Man-Machine-Environment System Engineering, 575–82. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-2481-9_67.

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Brillhart, Ralph, Kevin Napolitano, Lloyd Morgan, and Robert LeBlanc. "Aircraft GVT Advances and Application – Gulfstream G650." In Advanced Aerospace Applications, Volume 1, 145–57. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-9302-1_13.

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Rizzo, Emanuele, and Aldo Frediani. "Application of Optimisation Algorithms to Aircraft Aerodynamics." In Variational Analysis and Aerospace Engineering, 419–46. New York, NY: Springer New York, 2009. http://dx.doi.org/10.1007/978-0-387-95857-6_23.

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Li, Guo, and Dongdong Wang. "Research on the Aircraft Noise Evaluation and Application." In Advances in Intelligent and Soft Computing, 829–35. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-27866-2_101.

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Imanov, Tapdig, Melih Yıldız, and Elif Koruyucu. "Lean Six Sigma Application for Aircraft Maintenance Process." In Progress in Sustainable Aviation, 137–53. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-12296-5_8.

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O’Higgins, Eugene, Kyle Graham, Derk Daverschot, and Julien Baris. "Machine Learning Application on Aircraft Fatigue Stress Predictions." In ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing, 1031–42. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-21503-3_81.

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Wang, Shiyu, Zhouwei Fan, and Xiongqing Yu. "An Application of QFD in Aircraft Conceptual Design." In Proceedings of the International Conference on Aerospace System Science and Engineering 2020, 193–216. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-33-6060-0_13.

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Conference papers on the topic "Aircraft application"

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Friedrich, Kaspar Andreas, Josef Kallo, and Johannes Schirmer. "Fuel Cells for Aircraft Application." In ASME 2009 7th International Conference on Nanochannels, Microchannels, and Minichannels. ASMEDC, 2009. http://dx.doi.org/10.1115/icnmm2009-82131.

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Although air transport is responsible for only about 2% of all anthropogenic CO2 emissions, the rapidly increasing volume of air traffic leads to a general concern about the environmental impact of aviation. Future aircraft generations have to face enhanced requirements concerning productivity, environmental compatibility and higher operational availability, thus effecting technical, operational and economical aspects of in-flight and on-ground power generation systems. Today’s development in aircraft architecture undergoes a trend to a “more electric aircraft” which is characterised by a higher proportion of electrical systems substituting hydraulically or pneumatically driven components, and, thus, increasing the amount of electrical power. Fuel cell systems in this context represent a promising solution regarding the enhancement of the energy efficiency for both cruise and ground operations. For several years the Institute of Technical Thermodynamics of the German Aerospace Center (Deutsches Zentrum fu¨r Luft- und Raumfahrt, DLR) in Stuttgart is engaged in the development of fuel cell systems for aircraft applications. The activities of DLR focus on: • Identification of fuel cell applications in aircraft in which the properties of fuel cell systems, namely high electric efficiency, low emissions and silent operation, are capitalized for the aircraft application. • Design and modeling of possible system designs. • Experimental investigations regarding specific aircraft relevant operating conditions. • Qualification of airworthy fuel cell systems. • Set up and full scale testing of fuel cell systems for application in research aircraft. In cooperation with Airbus several fuel cell applications within the aircraft for both ground and cruise operation could be identified. In consequence, fuel cell systems capable to support or even replace existing systems have been derived. In this context, the provision of inert gas for the jet fuel (kerosene) tank and electrical cabin power supply including water regeneration represent the most promising application fields. The contribution will present the state of development discussing the following points: • Modeling of different system architectures and evaluation of promising fuel cell technologies (PEFC vs. SOFC). • Experimental evaluation of fuel cell systems under relevant conditions (low-pressure, vibrations, reformate operation, etc.). • Fuel cell system demonstrator Hyfish (hydrogen powered model aircraft). • Fuel cell test in DLR’s research aircraft ATRA (A320) including the test of an emergency system based on hydrogen and oxygen with 20 kW of electrical power. The fuel cell system was integrated into an A320 aircraft and tested up to a flight altitude of 25 000 feet under several acceleration and inclination conditions.
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Taha, M. H. "Power electronics for aircraft application." In IEE Colloquium on Power Electronics for Demanding Applications. IEE, 1999. http://dx.doi.org/10.1049/ic:19990332.

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BOLUKBASI, A., D. FUREY, and A. GOODWORTH. "Application of expert systems to CAD/CAE." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2085.

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Nam, Taewoo, Danielle Soban, and Dimitri Mavris. "A Generalized Aircraft Sizing Method and Application to Electric Aircraft." In 3rd International Energy Conversion Engineering Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-5574.

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HAJELA, P., and R. GLOWASKY. "Application of piezoelectric elements in supersonic panel flutter suppression." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3191.

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Brombach, J., M. Jordan, F. Grumm, and D. Schulz. "Converter topology analysis for aircraft application." In 2012 International Symposium on Power Electronics, Electrical Drives, Automation and Motion (SPEEDAM 2012). IEEE, 2012. http://dx.doi.org/10.1109/speedam.2012.6264483.

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Iqbal, Asif, and Faisal Saleem. "Monitoring application for Unmanned Aircraft Systems." In 2018 Moscow Workshop on Electronic and Networking Technologies (MWENT). IEEE, 2018. http://dx.doi.org/10.1109/mwent.2018.8337170.

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SICLARI, M., and J. PITTMAN. "Application of NCOREL to aircraft configurations." In 4th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1830.

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Ellsmore, Paul, and Kevin Restrick. "Application of RETIVO to Civil Aircraft." In 7th AIAA ATIO Conf, 2nd CEIAT Int'l Conf on Innov and Integr in Aero Sciences,17th LTA Systems Tech Conf; followed by 2nd TEOS Forum. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-7808.

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Lohner, Hubertus, Isabelle Delay-Saunders, Karsten Hesse, Alexis Martinet, Martin Beneke, Pawandeep Kalyan, and Benedikt Langer. "Eco-efficient Materials for Aircraft Application." In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2011. http://dx.doi.org/10.4271/2011-01-2742.

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Reports on the topic "Aircraft application"

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Xun, Xianxue, Qihao Long, Bingchen Pan, and Wenpu Chen. Yidoyu and Its Application to Aircraft Design. Fort Belvoir, VA: Defense Technical Information Center, January 1993. http://dx.doi.org/10.21236/ada259262.

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

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Santos, Jr, and Auteliano A. Application of LCR Waves to Inspect Aircraft Structures. Fort Belvoir, VA: Defense Technical Information Center, January 2013. http://dx.doi.org/10.21236/ada589393.

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Doo, Johnny. Unsettled Issues Regarding the Use of eVTOL Aircraft during Natural Disasters. SAE International, January 2022. http://dx.doi.org/10.4271/epr2022001.

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Abstract:
Recent advancements of electric vertical takeoff and landing (eVTOL) aircraft have generated significant interest within and beyond the traditional aviation industry, and many new and novel applications have been identified and are under development. One promising application is rapid response during natural disasters, which can complement current capabilities to help save lives and enhance post-disaster recoveries. The Use of eVTOL Aircraft During Natural Disasters presents issues that need to be addressed before eVTOL aircraft are integrated into natural disaster response operations: eVTOL vehicle development Detect-and-avoid capabilities in complex and challenging operating environments Autonomous and remote operations Charging system compatibility and availability Operator and controller training Dynamic air space management Vehicle/fleet logistics and support Acceptance from stakeholders and the public
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Rogers, Lynn, I. R. Searle, R. Ikegami, R. W. Gordon, and D. Conley. Durability Patch: Application of Passive Damping to High Cycle Fatigue Cracking on Aircraft. Fort Belvoir, VA: Defense Technical Information Center, March 1997. http://dx.doi.org/10.21236/ada468821.

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Lockner, Thomas Ramsbeck, R. Kevin Howard, Gary Edward Pena, Larry X. Schneider, Matthew B. Higgins, and Steven Frank Glover. Final report on development of Pulse Arrested Spark Discharge (PASD) for aging aircraft wiring application. Office of Scientific and Technical Information (OSTI), September 2006. http://dx.doi.org/10.2172/896561.

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Fortin, R., M. Coyle, D. Oneschuk, O. Boulanger, A. Grenier, B. Harvey, and M. Ouellet. Application of remotely piloted aircraft systems (RPAS) to regional airborne geophysical mapping: a concept study. Natural Resources Canada/CMSS/Information Management, 2022. http://dx.doi.org/10.4095/330010.

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Gould, R. W., Amone Jr., Sydor R. A., Kohler M., Bissett D. D., and W. P. Application of a Near-Infrared Slope Algorithm to Derive Optical Properties From High-Resolution, Hyperspectral Aircraft Imagery. Fort Belvoir, VA: Defense Technical Information Center, October 2004. http://dx.doi.org/10.21236/ada432395.

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Cheng, Meng-Dawn. Development and Application of Novel Sampling Methodologies for Study of Volatile Particulate Matter in Military Aircraft Emissions. Fort Belvoir, VA: Defense Technical Information Center, September 2012. http://dx.doi.org/10.21236/ada581970.

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Fu, Tian, Todd E. Sparks, Frank Liou, Zhiqiang Fan, Jianzhong Ruan, Joseph Newkirk, and Syamala R. Pulugurtha. Evaluation of Direct Diode Laser Deposited Stainless Steel 316L on 4340 Steel Substrate for Aircraft Landing Gear Application. Fort Belvoir, VA: Defense Technical Information Center, March 2010. http://dx.doi.org/10.21236/ada523920.

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