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Статті в журналах з теми "Composite aircraft structure"
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.
Повний текст джерелаUtami, Mala, Jonathan Ernest Sirait, Beny Budhi Septyanto, Aries Sudiarso, and I. Nengah Putra Apriyanto. "Laminar Composite Materials for Unmanned Aircraft Wings." Defense and Security Studies 3 (December 21, 2022): 106–12. http://dx.doi.org/10.37868/dss.v3.id211.
Повний текст джерелаLi, Fenglei, Shengnian Zhang, and Wanxiang Cheng. "Application and Optimization of Wing Structure Design of DF-2 Light Sports Aircraft Based on Composite Material Characteristics." Journal of Nanomaterials 2022 (June 21, 2022): 1–10. http://dx.doi.org/10.1155/2022/6967016.
Повний текст джерелаGanjeh, Babak, and Mohd Roshdi Hassan. "Cost-Efficient Composite Processing Techniques for Aerospace Applications – A Review." Applied Mechanics and Materials 325-326 (June 2013): 1465–70. http://dx.doi.org/10.4028/www.scientific.net/amm.325-326.1465.
Повний текст джерелаDu, Ya Xiong, Shu Li, and Kai Guo. "Strength Analysis for Composite Windshield of Commercial Aircraft." Advanced Materials Research 1030-1032 (September 2014): 1010–13. http://dx.doi.org/10.4028/www.scientific.net/amr.1030-1032.1010.
Повний текст джерелаArmstrong, Keith. "Civil Aircraft Composite Structure Repair Technology." Materials Technology 14, no. 4 (January 1999): 198–210. http://dx.doi.org/10.1080/10667857.1999.11752840.
Повний текст джерелаGrant, Carroll. "Automated processes for composite aircraft structure." Industrial Robot: An International Journal 33, no. 2 (March 2006): 117–21. http://dx.doi.org/10.1108/01439910610651428.
Повний текст джерелаLee, WJ, BH Seo, SC Hong, MS Won, and JR Lee. "Real world application of angular scan pulse-echo ultrasonic propagation imager for damage tolerance evaluation of full-scale composite fuselage." Structural Health Monitoring 18, no. 5-6 (February 24, 2019): 1943–52. http://dx.doi.org/10.1177/1475921719831370.
Повний текст джерелаChernov, Andrey, Ivan Kondakov, and Yury Mirgorodskiy. "Experimental Study of Impact-Protective Elements for Unidirectional Ribs of Lattice Composite Aircraft Structures." MATEC Web of Conferences 304 (2019): 01016. http://dx.doi.org/10.1051/matecconf/201930401016.
Повний текст джерелаZhang, Jia Rui, Zhen Yu Feng, and Tian Chun Zou. "Certification for Effect of Environment on Composite Properties." Advanced Materials Research 284-286 (July 2011): 396–400. http://dx.doi.org/10.4028/www.scientific.net/amr.284-286.396.
Повний текст джерелаДисертації з теми "Composite aircraft structure"
Bigand, Audrey. "Damage assessment on aircraft composite structure due to lightning constraints." Thesis, Toulouse, ISAE, 2020. http://www.theses.fr/2020ESAE0027.
Повний текст джерелаAs composite materials are now widely used in the aeronautical industry, the sizing of these structures andtheir protection against lightning has become a major issue. It is important to develop predictive tools to obtaina structure concept that meets certification requirements with a controlled time and cost during the designphase. The interaction of lightning with a composite structure is a complex multi-physics phenomenon, with afurther difficulty due to the presence of a metallic protection on the surface and a layer of paint. In this context,this study aimed to develop an understanding of the forces generated by lightning and to assess itsconsequences in terms of damage to the composite. To this end, the phenomenon was first broken down tostudy its different components and define the impact of their interactions. In a first step, the free arc wascompared to the arc root in interaction with different substrates to define a vaporisation model of the lightningprotection. In a second step, the overpressure generated by the explosion of the surface protection duringvaporisation was evaluated to define spatio-temporal pressure profiles. In a third step, a mechanicalcharacterization of the paint was developed in order to quantify its confinement effect on the surface explosion.At each stage, a theory was developed and analysed via numerical models and tests. Finally, these threedifferent bricks are brought together in a mechanical model simulating the lightning impact on a compositestructure in order to predict the damage. In addition, a user subroutine has been developed to apply thiscomplex loading as well as a damage law. These models are compared with lightning laboratory test results todetermine their validity limits and their ability to predict the damage
Svalstedt, Mats, and Sofia Swedberg. "Commercial Aircraft Wing Structure : - Design of a Carbon Fiber Composite Structure." Thesis, KTH, Skolan för teknikvetenskap (SCI), 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-276702.
Повний текст джерелаDetta projekt utforskar den klassiska vingstrukturen av ett kommersiellt flygplan för en obemannad luftfarkost gjord helt i kolfiberarmerad polymer. Det är en del av ett samarbete som består av flera projektgrupper som forskar på olika delar av flygplanet. Målet med projektet är att designa den inre vingstrukturen för en miljövänligare, mer effektiv uppskalad 2:1 version av drönaren Skywalker X8. För att göra flygplanet så effektiv som möjligt så behöver den vara lättviktig. Lasterna var först uppskattade via XFLR5 och en första design gjordes. Designen testades sedan med finita elementmetoden (FEM) i programmet Ansys Static Structural. Materialet som testades var kolfiber/epoxi prepreg. Den slutgiltiga vingdesignen väger 3.815 kg, och består av en bom och en tjocklek på 1 mm av vingskalet. Totala vikten av flygplanet, inklusive framdrivningssystemet samt virveldämpare på båda vingspetsarna som är framtagna av andra grupper, är 20.262 kg. Glidtalet beräknades även, och är som mest effektiv runt 2-3°.
Mahdi, Stephane. "The performance of bonded repairs to composite structures." Thesis, Imperial College London, 2001. http://hdl.handle.net/10044/1/7815.
Повний текст джерелаBail, Justin L. "Non-desctructive investigation & FEA correlation on an aircraft sandwich composite structure." Akron, OH : University of Akron, 2007. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=akron1196702586.
Повний текст джерела"December, 2007." Title from electronic thesis title page (viewed 02/25/2008) Advisor, Wieslaw Binienda; Faculty readers, Craig Menzemer, Robert Goldbert; Department Chair, Wieslaw Binienda; Dean of the College, George K. Haritos; Dean of the Graduate School, George R. Newkome. Includes bibliographical references.
Bail, Justin. "Non-Destructive Investigation & FEA Correlation on an Aircraft Sandwich Composite STructure." University of Akron / OhioLINK, 2007. http://rave.ohiolink.edu/etdc/view?acc_num=akron1196702586.
Повний текст джерелаLiu, Hongfen. "A structural design comparison of metallic and composite aircraft pressure retaining doors." Thesis, Cranfield University, 2012. http://dspace.lib.cranfield.ac.uk/handle/1826/7308.
Повний текст джерелаCrump, Duncan Andrew. "Performance analysis of a reduced cost manufacturing process for composite aircraft secondary structure." Thesis, University of Southampton, 2009. https://eprints.soton.ac.uk/142803/.
Повний текст джерелаSatterwhite, Matthew Ryan. "Development and Validation of Fluid-Structure Interaction in Aircraft Crashworthiness Studies." Thesis, Virginia Tech, 2013. http://hdl.handle.net/10919/51559.
Повний текст джерелаMaster of Science
Backhouse, R. "Multiaxial non-crimp fabrics : characterisation of manufacturing capability for composite aircraft primary structure applications." Thesis, Cranfield University, 1998. http://dspace.lib.cranfield.ac.uk/handle/1826/1929.
Повний текст джерелаXu, Rongxin. "Optimal design of a composite wing structure for a flying-wing aircraft subject to multi-constraint." Thesis, Cranfield University, 2012. http://dspace.lib.cranfield.ac.uk/handle/1826/7290.
Повний текст джерелаКниги з теми "Composite aircraft structure"
Chamis, C. C. Structural tailoring of select fiber composite structures. [Washington, D.C.]: NASA, 1990.
Знайти повний текст джерелаLeite Cavalcanti, Welchy, Kai Brune, Michael Noeske, Konstantinos Tserpes, Wiesław M. Ostachowicz, and Mareike Schlag, eds. Adhesive Bonding of Aircraft Composite Structures. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4.
Повний текст джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Repair of Aircraft Structures Involving Composite Materials. S.l: s.n, 1986.
Знайти повний текст джерелаDastin, Samuel J. Aircraft composite materials and structures: Seminar notes. Lancaster, PA: Technomic Publishing Co., 1986.
Знайти повний текст джерелаSmith, Peter J. Damage tolerant composite wing panels for transport aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Знайти повний текст джерелаRenaud, Guillaume. Advanced optimal design concepts for composite material aircraft repair. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.
Знайти повний текст джерелаPoon, C. A review of crashworthiness of composite aircraft structures. Ottawa: National Aeronautical Establishment, 1990.
Знайти повний текст джерелаDevelopment, Advisory Group for Aerospace Research and. The repair of aircraft structures involving composite materials. Neuilly-sur-Seine: Agard, 1986.
Знайти повний текст джерелаDevelopment, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Composite repair of military aircraft structures: Papers presented at the 79th Meeting of the AGARD Structures and Materials Panel, held in Seville, Spain 3-5 October 1994. Neuilly sur Seine, France: AGARD, 1995.
Знайти повний текст джерелаGlossop, N. D. W. Optical fibre damage detection for an aircraft composite leading edge. [S.l.]: [s.n.], 1990.
Знайти повний текст джерелаЧастини книг з теми "Composite aircraft structure"
Barut, Silvere. "Sensitive Coating Solutions to Lower BVID Threshold on Composite Structure." In Smart Intelligent Aircraft Structures (SARISTU), 745–51. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-22413-8_37.
Повний текст джерелаSaleem, M., Nishant Kumar Raj, Shreshth Gupta, and Yogesh Kumar. "Design and Analysis of Aluminium Matrix Composite Aircraft Wing Structure." In Lecture Notes in Mechanical Engineering, 53–60. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-6619-6_6.
Повний текст джерелаTran, B., P. G. Ifju, M. M. Mennu, A. Brenes, and S. Shbalko. "Applying Macro Fiber Composite Patches to Morph Complex Aircraft Structure." In Mechanics of Composite, Hybrid and Multifunctional Materials , Volume 6, 99–106. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-59868-6_15.
Повний текст джерелаVenkatesh, S., S. C. Lakshminarayana, and Byji Varughese. "Integrity Evaluation of Feature Level Test Specimen of an Aircraft Primary Composite Structure." In Advances in Structural Integrity, 93–101. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-7197-3_8.
Повний текст джерелаSu, Weiguo, Lan Zou, Zhitao Mu, and Xudong Li. "Stress Analysis of Cracked Metallic Aircraft Structure Adhesively Repaired with Composite Patch." In Lecture Notes in Electrical Engineering, 369–77. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54233-6_41.
Повний текст джерелаHavar, Tamas, and Eckart Stuible. "Design and Testing of Advanced Composite Load Introduction Structure for Aircraft High Lift Devices." In ICAF 2009, Bridging the Gap between Theory and Operational Practice, 365–74. Dordrecht: Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-2746-7_21.
Повний текст джерелаChoquet, Marc, René Héon, Christian Padioleau, Paul Bouchard, Christian Néron, and Jean-Pierre Monchalin. "Laser-Ultrasonic Inspection of the Composite Structure of an Aircraft in a Maintenance Hangar." In Review of Progress in Quantitative Nondestructive Evaluation, 545–52. Boston, MA: Springer US, 1995. http://dx.doi.org/10.1007/978-1-4615-1987-4_66.
Повний текст джерелаKelly, Don W., Murray L. Scott, and Rodney S. Thomson. "Composite Aircraft Structures." In Modeling Complex Engineering Structures, 247–74. Reston, VA: American Society of Civil Engineers, 2007. http://dx.doi.org/10.1061/9780784408506.ch09.
Повний текст джерелаGatewood, B. E. "Composite materials." In Virtual Principles in Aircraft Structures, 582–610. Dordrecht: Springer Netherlands, 1989. http://dx.doi.org/10.1007/978-94-009-1165-9_16.
Повний текст джерелаHarinarayana, Kota. "Design Approach to Composites in Fighter Aircraft: Current status." In Composite Structures, 1–19. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-662-11345-5_1.
Повний текст джерелаТези доповідей конференцій з теми "Composite aircraft structure"
COT, LEA, SHUVAJIT MUKHERJEE, MISAEL MELGAR, and RANJAN GANGULI. "Aircraft Composite Structure Preventive Maintenance." In Structural Health Monitoring 2015. Destech Publications, 2015. http://dx.doi.org/10.12783/shm2015/282.
Повний текст джерелаJonas, Paul, and Tom Aldag. "Certification of Bonded Composite Structure." In General Aviation Aircraft Meeting and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1987. http://dx.doi.org/10.4271/871022.
Повний текст джерелаPugazhenthi, V., S. Gopalakannan, and R. Rajappan. "Finite Element Analysis of Composite Shell Structure of Aircraft Wing Using Composite Structure." In 2018 IEEE International Conference on System, Computation, Automation and Networking (ICSCAN). IEEE, 2018. http://dx.doi.org/10.1109/icscan.2018.8541192.
Повний текст джерелаLiu, X., and S. Mahadevan. "Failure probability of a composite aircraft wing structure." In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-2048.
Повний текст джерелаBrunson, S., and M. Rais-Rohani. "A thin tailored composite wing box for a civil tiltrotor transport aircraft." In 37th Structure, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-1378.
Повний текст джерелаSoderquist, Joseph R. "Design/Certification Considerations in Civil Composite Aircraft Structure." In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1987. http://dx.doi.org/10.4271/871846.
Повний текст джерелаMillwater, H., K. Griffin, D. Wieland, A. West, H. Smith, M. Holly, and R. Holzwarth. "Probabilistic analysis of an advanced fighter/attack aircraft composite wing structure." In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-1567.
Повний текст джерелаBROWN, WILLIAM, and DARYL TIMMERMAN. "Benefits of composite structure for the tandem wing Advanced Technology Tactical Transport." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3167.
Повний текст джерелаEngelstad, Stephen P., Jason Action, Stephen B. Clay, Richard Holzwarth, Richard W. Dalgarno, and Don Robbins. "Assessment of Composite Damage Growth Tools for Aircraft Structure - Part I." In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1876.
Повний текст джерелаEngelstad, Stephen P., and Stephen Clay. "Assessment of Composite Damage Growth Tools for Aircraft Structure Part II." In 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-0725.
Повний текст джерелаЗвіти організацій з теми "Composite aircraft structure"
Hosur, Mahesh V., Shaik Jeelani, Uday K. Vaidya, and Sylvanus Nwosu. Survivability of Affordable Aircraft Composite Structures. Volume 2: High Strain Rate Characterization of Affordable Woven Carbon/Epoxy Composites. Fort Belvoir, VA: Defense Technical Information Center, April 2003. http://dx.doi.org/10.21236/ada421599.
Повний текст джерелаHosur, Mahesh V., Shaik Jeelani, Uday K. Vaidya, Sylvanus Nwosu, and Ajit D. Kelkar. Survivability of Affordable Aircraft Composite Structures. Volume 1: Overview and Ballistic Impact Testing of Affordable Woven Carbon/Epoxy Composites. Fort Belvoir, VA: Defense Technical Information Center, April 2003. http://dx.doi.org/10.21236/ada421600.
Повний текст джерелаHosur, Mahesh V., Shaik Jeelani, Uday K. Vaidya, and Ajit D. Kelkar. Survivability of Affordable Aircraft Composite Structures. Volume 3: Characterization of Affordable Woven Carbon/Epoxy Composites Under Low-Velocity Impact Loading. Fort Belvoir, VA: Defense Technical Information Center, April 2003. http://dx.doi.org/10.21236/ada421601.
Повний текст джерелаRoach, Dennis, and Thomas Rice. A Quantitative Assessment of Advanced NDI Techniques for Detecting Flaws in Composite Laminate Aircraft Structures. Office of Scientific and Technical Information (OSTI), August 2014. http://dx.doi.org/10.2172/1762097.
Повний текст джерелаRoach, D., and P. Walkington. Full-Scale Structural and NDI Validation Tests of Bonded Composite Doublers for Commercial Aircraft Applications. Office of Scientific and Technical Information (OSTI), February 1999. http://dx.doi.org/10.2172/4368.
Повний текст джерелаMatt, Howard M. Structural Diagnostics of CFRP Composite Aircraft Components by Ultrasonic Guided Waves and Built-In Piezoelectric Transducers. Office of Scientific and Technical Information (OSTI), January 2006. http://dx.doi.org/10.2172/899976.
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