Relevant bibliographies by topics / Airplane structures

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

Academic literature on the topic 'Airplane structures'

Author: Grafiati
Published: 4 June 2021
Last updated: 6 February 2022

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Journal articles on the topic "Airplane structures"

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Lin, L., Y. X. Ren, M. Y. Huang, X. D. Zhi, and D. Z. Wang. "Failure Modes of a Reticulated Dome in a Small Airplane Crash." Advances in Civil Engineering 2019 (August 8, 2019): 1–10. http://dx.doi.org/10.1155/2019/5025637.

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Since the 9/11 incident, many engineering research works have been conducted on the impact resistance of large-span space structures. In the present study, a small airplane, Bombardier Challenger 850, was chosen as the test subject. An airplane crash on a single-layered Kiewitt-8 reticulated dome with span 60 m considering roof sheathing effect was simulated using ANSYS/LS-DYNA software. The principles of establishing the numerical model of small airplanes were determined. In addition, the impact styles of small airplane and impact positions on the dome were investigated. The failure modes of
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Nesterenko, G. I. "Fatigue and service lives of airplane structures." Journal of Machinery Manufacture and Reliability 39, no. 1 (2010): 98–100. http://dx.doi.org/10.3103/s1052618810010164.

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Nesterenko, Boris G., and Grigory I. Nesterenko. "Fatigue and Damage Tolerance of Aging Airplane Structures." Advanced Materials Research 891-892 (March 2014): 1669–74. http://dx.doi.org/10.4028/www.scientific.net/amr.891-892.1669.

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The paper highlights key questions in ensuring safe operation of aging civil\transport aircraft in Russia. Presented is the analysis of current requirements to fatigue, fail-safe and damage tolerance for transport aircraft structures stated in FARs, Advisory Circulars (UAS) and Russian Airworthiness Regulations\ AR IAC Aviation Regulations. The paper gives the design goals and actual service life values\ service years of aging aircraft fleet and data on full-scaled fatigue tests, together with methods and approaches to ensure safe operation of aircraft structures in case of multiple site damag
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Rao, S. S. "Optimization of airplane wing structures under gust loads." Computers & Structures 21, no. 4 (1985): 741–49. http://dx.doi.org/10.1016/0045-7949(85)90150-6.

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Rao, S. S. "Optimization of airplane wing structures under taxiing loads." Computers & Structures 26, no. 3 (1987): 469–79. http://dx.doi.org/10.1016/0045-7949(87)90047-2.

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Makarov, Ihor Andriyovych, and Sergey Romualdovich Ignatovich. "SELECTION AND OPTIMIZATION OF FUSELAGE COMPONENTS FOR MODERN AIRPLANES." Aerospace technic and technology, no. 7 (August 31, 2019): 12–20. http://dx.doi.org/10.32620/aktt.2019.7.02.

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Nowadays the level of development of airplane materials shows the tendency of usage of advanced composite structures. However, these materials have plenty of advantages and disadvantages, the most crucial is the ability to absorb water from the environment and because of this layers of composite structures disbonded and consequently became useless. This issue demonstrates the limitation of usage of advanced composite structures. Despite this fact application of conventional materials (such as Aluminum or Titanium alloys) are limited by the weight of structure and manufacturability. In given ar
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Duró, Josep M., and Josep M. Bergadà. "Airplane Vortices Evolution Near Ground." Applied Sciences 11, no. 1 (2021): 457. http://dx.doi.org/10.3390/app11010457.

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Airport traffic around the world has sharply increased over the years; as a result, airports need to be enlarged and the landing or taking off times between two consecutive airplanes must be reduced. To precisely determine the minimum time required between two consecutive airplanes, it is essential to understand the main physical characteristics of the vortices generated under airplanes’ wings and their evolution under different atmospheric conditions. In the present paper, such information is obtained through the complex potential equation of a vortex together with the potential Bernoulli equ
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Tang, Wenbo, Pak Wai Chan, and George Haller. "Lagrangian Coherent Structure Analysis of Terminal Winds Detected by Lidar. Part II: Structure Evolution and Comparison with Flight Data." Journal of Applied Meteorology and Climatology 50, no. 10 (2011): 2167–83. http://dx.doi.org/10.1175/2011jamc2689.1.

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AbstractUsing observational data from coherent Doppler light detection and ranging (lidar) systems situated at the Hong Kong International Airport (HKIA), the authors extract Lagrangian coherent structures (LCS) intersecting the flight path of landing aircraft. They study the time evolution of LCS and compare them with onboard wind shear and altitude data collected during airplane approaches. Their results show good correlation between LCS extracted from the lidar data and updrafts and downdrafts experienced by landing aircraft. Overall, LCS analysis shows promise as a robust real-time tool to
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Zelenika, Saša, Zdenek Hadas, Sebastian Bader, et al. "Energy Harvesting Technologies for Structural Health Monitoring of Airplane Components—A Review." Sensors 20, no. 22 (2020): 6685. http://dx.doi.org/10.3390/s20226685.

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With the aim of increasing the efficiency of maintenance and fuel usage in airplanes, structural health monitoring (SHM) of critical composite structures is increasingly expected and required. The optimized usage of this concept is subject of intensive work in the framework of the EU COST Action CA18203 “Optimising Design for Inspection” (ODIN). In this context, a thorough review of a broad range of energy harvesting (EH) technologies to be potentially used as power sources for the acoustic emission and guided wave propagation sensors of the considered SHM systems, as well as for the respectiv
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Rios, J., R. Roy, and A. Lopez. "Design requirements change and cost impact analysis in airplane structures." International Journal of Production Economics 109, no. 1-2 (2007): 65–80. http://dx.doi.org/10.1016/j.ijpe.2006.11.004.

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Dissertations / Theses on the topic "Airplane structures"

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Llopart, Prieto Llorenç. "Modelling And Analysis Of Crack Turning On Aeronautical Structures." Doctoral thesis, Universitat Politècnica de Catalunya, 2007. http://hdl.handle.net/10803/6055.

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La motivació de la tesis deriva en el interès de la indústria aeronàutica a explotar, per mitjà d'un disseny adaptat, la utilització del gir d'esquerda per protegir els reforços situats davant una esquerda que s'està propagant en la xapa d'una estructura integral. L'objectiu principal és l'avaluació i predicció del gir d'esquerda en situacions de càrrega pròximes a Mode I, proporcionant una eina de modelització i un criteri confident. L'entorn industrial sota el qual s'ha realitzat aquest treball requereix una predicció ràpida del comportament estructural proporcionant informació útil als cons
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Swanson, Gary D. "Structural efficiency study of composite wing rib structures." Thesis, This resource online, 1987. http://scholar.lib.vt.edu/theses/available/etd-04292010-020010/.

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Unger, Eric Robert. "Integrated aerodynamic-structural wing design optimization." Diss., This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-09042008-063104/.

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Koh, Yeow Leung 1976. "In-situ structural health monitoring of composite repair patches." Monash University, Dept. of Mechanical Engineering, 2002. http://arrow.monash.edu.au/hdl/1959.1/7698.

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Ragon, Scott A. "Optimization of composite box-beam structures including effects of subcomponent interaction /." This resource online, 1994. http://scholar.lib.vt.edu/theses/available/etd-06162009-063327/.

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Aljets, Dirk. "Acoustic emission source location in composite aircraft structures using modal analysis." Thesis, University of South Wales, 2011. https://pure.southwales.ac.uk/en/studentthesis/acoustic-emission-source-location-in-composite-aircraft-structures-using-modal-analysis(6871e94b-6e94-4efd-b563-41b254ee27b4).html.

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The aim of this research work was to develop an Acoustic Emission (AE) source location method suitable for Structural Health Monitoring (SHM) of composite aircraft structures. Therefore useful key signal features and sensor configurations were identified and the proposed method was validated using both artificially generated AE as well as actual AE resulting from damage. Acoustic Emission is a phenomenon where waves are generated in stressed materials. These waves travel through the material and can be detected with suitable sensors on the surface of the structure. These stress waves are attri
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Seitz, Timothy J. "Formulation of a structural model for flutter analysis of low aspect ratio composite aircraft wings." Diss., This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-05042006-164511/.

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Zhou, Weiyu. "Crash-impact behavior of graphite/epoxy composite sine wave webs." Diss., Georgia Institute of Technology, 1989. http://hdl.handle.net/1853/12226.

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Mosinyi, Bao Rasebolai Awerbuch Jonathan Lau Alan C. W. Tan Tein-Min. "Fatigue damage assessment of high-usage in-service aircraft fuselage structure /." Philadelphia, Pa. : Drexel University, 2007. http://hdl.handle.net/1860/2762.

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Dayyani, Iman. "Mechanical behavior of composite corrugated structures for skin of morphing aircraft." Thesis, Swansea University, 2015. https://cronfa.swan.ac.uk/Record/cronfa42865.

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Corrugated panels have gained considerable popularity in a range of engineering applications, particularly in morphing skin applications due to their remarkable anisotropic characteristics. They are stiff to withstand the aerodynamic loads and flexible to enable the morphing deformations. In this thesis a detailed review of the literature on corrugated structures is presented. The specific characteristics of corrugated structures such as: high anisotropic behaviour, high stiffness and good durability, lightness and cost effectiveness are discussed comprehensively. However for the application i
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Books on the topic "Airplane structures"

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Blackburn, Gerald A. Downey's aerospace history, 1947-1999. Arcadia Publishing, 2009.

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Blackburn, Gerald A. Downey's aerospace history, 1947-1999. Arcadia Publishing, 2009.

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FEDERAL AVIATION ADMINISTRATION. Certification of transport airplane structure. U.S. Dept. of Transportation, Federal Aviation Administration, 1999.

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Atluri, S. N. Structural Integrity of Aging Airplanes. Springer Berlin Heidelberg, 1991.

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Atluri, S. N., S. G. Sampath, and Pin Tong, eds. Structural Integrity of Aging Airplanes. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-84364-8.

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McGinty, Stephen. Fire in the night: The Piper Alpha disaster. Pan Books, 2009.

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McGinty, Stephen. Fire in the night: The Piper Alpha disaster. Pan Books, 2009.

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Fire in the night: The Piper Alpha disaster. Pan Books, 2009.

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Ballmann, Josef, ed. Flow Modulation and Fluid—Structure Interaction at Airplane Wings. Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-540-44866-2.

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Alletru, Nelly. L' usine d'aviation Marcel Bloch à Déols: Centre. Inventaire général du patrimoine culturel, 2007.

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Book chapters on the topic "Airplane structures"

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Nesterenko, Boris, Grirory I. Nesterenko, and Valentin N. Basov. "Fracture Behaviour of Skin Materials of Civil Airplane Structures." In ICAF 2009, Bridging the Gap between Theory and Operational Practice. Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-2746-7_38.

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Vanlanduit, Steve, Patrick Guillaume, Jimmy Vermeulen, and Kristof Harri. "Tracking of Cracks in Airplane Components Using Nonlinear Surface Wave Propagation Techniques." In Damage Assessment of Structures VI. Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-976-8.549.

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Ibrahimbegovic, Adnan, and Naida Ademovicć. "The dynamics of extreme impact loads in an airplane crash." In Nonlinear Dynamics of Structures Under Extreme Transient Loads. CRC Press, 2019. http://dx.doi.org/10.1201/9781351052504-6.

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Magnusen, P. E., D. C. Mooy, L. A. Yocum, and R. J. Rioja. "Development of High Toughness Sheet and Extruded Products for Airplane Fuselage Structures." In ICAA13 Pittsburgh. Springer International Publishing, 2012. http://dx.doi.org/10.1007/978-3-319-48761-8_78.

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Magnusen, P. E., D. C. Mooy, L. A. Yocum, and R. J. Rioja. "Development of High Toughness Sheet and Extruded Products for Airplane Fuselage Structures." In ICAA13: 13th International Conference on Aluminum Alloys. John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch78.

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Nesterenko, Boris G., Grigory I. Nesterenko, Victor V. Konovalov, and Vitaly Ya Senik. "Russian Practice to Provide Safe Operation of Airplane Structures with Long-Term Operation." In ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-21503-3_22.

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Jochum, Robert, Antonio Rufin, Tanni Sisco, and Frederick Swanstrom. "Fatigue Considerations in the Development and Implementation of Mechanical Joining Processes for Commercial Airplane Structures." In ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-21503-3_17.

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Mar, James W. "Structural Integrity of Aging Airplanes: A Perspective." In Springer Series in Computational Mechanics. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-84364-8_17.

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Britten, G., C. Braun, M. Hesse, and J. Ballmann. "Computational Aeroelasticity with Reduced Structural Models." In Flow Modulation and Fluid—Structure Interaction at Airplane Wings. Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-540-44866-2_11.

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Jung, W., and H. G. Reimerdes. "Concepts for Reduced Structural Models of Airplane Wings in Aeroelasticity." In Flow Modulation and Fluid—Structure Interaction at Airplane Wings. Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-540-44866-2_10.

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Conference papers on the topic "Airplane structures"

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Ricci, Sergio, and Alessandro Scotti. "Aeroelastic Testing on a Three Surface Airplane." In 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
14th AIAA/ASME/AHS Adaptive Structures Conference
7th. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-2189.

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FASANELLA, E., E. WIDMAYER, and M. ROBINSON. "Structural analysis of the controlled impact demonstration of a jet transport airplane." In 27th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-939.

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Rivera, Jose, and James Florance. "Contributions of Transonic Dynamics Tunnel testing to airplane flutter clearance." In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-1768.

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Chen, P. C., D. D. Liu, and Eli Livne. "Unsteady Aerodynamic Shape Sensitivities for Airplane Aeroservoelastic Configuration Optimization." In 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-1759.

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ALLEN, M., M. REARDON, and F. GORDON. "Use of the flight simulator in performing AFTI/F-16 airplane aeroservoelastic analysis." In 27th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-957.

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Monteriro, Elvis, Suchilla Leao, Matheus Norton, Marina G. Martins, and Antonio F. Avila. "Fire Behavior of Hybrid Nano-Modified Composites for Airplane Interiors." In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0910.

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Liu, Wanbo, Balaji Kaushik, and Willem Anemaat. "Weight Investigation of a Novel Split-Wing Airplane Layout." In 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
20th AIAA/ASME/AHS Adaptive Structures Conference
14th AIAA. American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-1995.

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Machida, Shigeru, Takeshi Takatoya, and Kenichi Saitoh. "Structural Design and Flight Verification of Unmanned Supersonic Experimental Airplane." In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-2118.

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Cesnik, Carlos, and Eric Brown. "Active Warping Control of a Joined Wing/Tail Airplane Configuration." In 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-1715.

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MOSS, STEVEN, STANLEY COLE, and ROBERT DOGGETT, JR. "Some subsonic and transonic buffet characteristics of the twin-vertical-tails of a fighter airplane configuration." In 32nd Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-1049.

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Reports on the topic "Airplane structures"

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Sarrack, A. G. Airplane Crash Frequency for DWPF Structures. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/1482193.

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Ramesh, Anapathur V., David Twigg, and Tilak Sharma. Modeling Average Flight Risk due to Lightning Threat in Safety Analysis for Airplane Systems and Structures. SAE International, 2011. http://dx.doi.org/10.4271/2011-01-2567.

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