Littérature scientifique sur le sujet « Aerospace Structure »
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Articles de revues sur le sujet "Aerospace Structure"
RAHIM, Erween, Takayuki OGAWA, Akihiko MIURA, Hiroyuki SASAHARA, Rei Koyasu et Yasuhiro Yao. « 3252 Ultrasonic Torsional Vibration Drilling of Aerospace Structure Material ». Proceedings of International Conference on Leading Edge Manufacturing in 21st century : LEM21 2011.6 (2011) : _3252–1_—_3252–4_. http://dx.doi.org/10.1299/jsmelem.2011.6._3252-1_.
Texte intégralDOS SANTOS E LUCATO, S. L., R. M. MCMEEKING et A. G. EVANS. « SMS-12 : Shape Morphing Truss Structure for Aerospace and Marine Applications(SMS-II : SMART MATERIALS AND STRUCTURES, NDE) ». Proceedings of the JSME Materials and Processing Conference (M&P) 2005 (2005) : 30. http://dx.doi.org/10.1299/jsmeintmp.2005.30_4.
Texte intégralBajurko, Piotr. « Modelling of the Aerospace Structure Demonstrator Subcomponent ». Transactions on Aerospace Research 2019, no 1 (1 mars 2019) : 37–52. http://dx.doi.org/10.2478/tar-2019-0004.
Texte intégralAl-Madani, Ramadan A., M. Jarnaz, K. Alkharmaji et M. Essuri. « Finite Element Modeling of Composites System in Aerospace Application ». Applied Mechanics and Materials 245 (décembre 2012) : 316–22. http://dx.doi.org/10.4028/www.scientific.net/amm.245.316.
Texte intégralYAMAMOTO, Tetsuya. « Application of adhesive bonded structure on aerospace. » Journal of the Surface Finishing Society of Japan 40, no 11 (1989) : 1203–6. http://dx.doi.org/10.4139/sfj.40.1203.
Texte intégralSainfort, P., Christophe Sigli, G. M. Raynaud et P. Gomiero. « Structure and Property Control of Aerospace Alloys ». Materials Science Forum 242 (janvier 1997) : 25–32. http://dx.doi.org/10.4028/www.scientific.net/msf.242.25.
Texte intégralHorton, B., Y. Song, D. Jegley, F. Collier et J. Bayandor. « Predictive analysis of stitched aerospace structures for advanced aircraft ». Aeronautical Journal 124, no 1271 (18 novembre 2019) : 44–54. http://dx.doi.org/10.1017/aer.2019.137.
Texte intégralJiayu, Yao. « A method of coding for aerospace product quality DNA ». MATEC Web of Conferences 151 (2018) : 05006. http://dx.doi.org/10.1051/matecconf/201815105006.
Texte intégralTADA, Yasuo. « Composite structure test facility in Natl. Aerospace Lab.. » Journal of the Japan Society for Composite Materials 18, no 1 (1992) : 33–38. http://dx.doi.org/10.6089/jscm.18.33.
Texte intégralLee, Jong-Woong, Cheol-Won Kong et Young-Shin Lee. « The Design of Aerospace Structure by Explosive Loading ». International Journal of Aerospace and Lightweight Structures (IJALS) - 03, no 04 (2013) : 531. http://dx.doi.org/10.3850/s2010428614000075.
Texte intégralThèses sur le sujet "Aerospace Structure"
Ahn, Junghyun. « Integrated analysis procedure of aerospace composite structure ». Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/43106.
Texte intégralIncludes bibliographical references (p. 50).
The emergence of composite material application in major commercial aircraft design, represented by the Boeing 787 and Airbus A350-XWB, signals a new era in the aerospace industry. The high stiffness to weight ratio of continuous fiber composites (CFC) makes CFCs one of the most important materials to be introduced in modern aircraft industry. In addition to inherent strength (per given weight) of CFCs, they also offer the unusual opportunity to design the structure and material concurrently. The directional properties (and the ability to change these properties through the design process) of composite materials can be used in aeroelastically tailored wings, the fuselage and other critical areas. Due to the longer lifecycle (25-30 years) of a commercial airliner and the tools and processes developed for the airplane of previous product development cycles, new technology often ends up being deployed less effectively because of the mismatch in the technical potential (what can be done) vs. design tools and processes (what was done before). Tools and processes need to be current to take advantage of latest technology, and this thesis will describe one possible approach in primary composite structural design area using integrated structural analysis
by Junghyun Ahn.
S.M.
Key, Ross A. « Automated manufacturing processes for secondary structure aerospace composites ». Thesis, University of Nottingham, 2016. http://eprints.nottingham.ac.uk/33572/.
Texte intégralHu, Zhuopei. « Finite Element Modeling of Aerospace Materials and Structure ». University of Akron / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=akron1344224158.
Texte intégralZheng, LiangKan 1972. « Fluid-structure coupling for aeroelastic computations in the time domain using low fidelity structural models ». Thesis, McGill University, 2005. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=99127.
Texte intégralSeddon, Caroline Michelle. « Modelling transient dynamic fluid-structure interaction in aerospace applications ». Thesis, University of Salford, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.492434.
Texte intégralBhatti, Wasim. « Mechanical integration of a PEM fuel cell for a multifunctional aerospace structure ». Thesis, Loughborough University, 2016. https://dspace.lboro.ac.uk/2134/21513.
Texte intégralPalsule, Sanjay. « Structure and properties of aerospace molecular composites : third generation polymers ». Thesis, Heriot-Watt University, 1994. http://hdl.handle.net/10399/1388.
Texte intégralKhataee, Amin. « Structure and properties of some Ti-Al-Ru alloys ». Thesis, Imperial College London, 1987. http://hdl.handle.net/10044/1/46915.
Texte intégralLiang, Lijun. « Experimental investigation of an aeroelastic structure with continuous nonlinear stiffness ». Thesis, McGill University, 2003. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=80123.
Texte intégralSeveral linear and nonlinear system tests are presented, and the results compared and analyzed. The effects of linear plunge stiffness on the stability of the aeroelastic system are discussed, and the nonlinear system response is studied for different degrees of cubic nonlinearity in pitch.
In several nonlinear system tests, limit cycle oscillations (LCO) are observed when the air speed is above the linear flutter speed. The effects of airfoil initial conditions and air speeds on the LCO amplitude, frequency, and convergence rate are studied.
The effective linear flutter speed is predicted using the so-called "flutter-margin" method for both the linear and nonlinear cases. The prediction results for the nonlinear cases are compared with those for the linear cases and with the actual flutter speed.
Ozsoy, Serhan. « Vibration Induced Stress And Accelerated Life Analyses Of An Aerospace Structure ». Master's thesis, METU, 2006. http://etd.lib.metu.edu.tr/upload/2/12606966/index.pdf.
Texte intégral#8217
s dynamic characteristics and varying loadings. Therefore, experimental, numerical or a combination of both methods are used for fatigue evaluations. Fatigue failure can occur on systems and platforms as well as components to be mounted on the platform. In this thesis, a helicopter&
#8217
s Missile Warning Sensor - Cowling assembly is analyzed. Analytical, numerical and experimental approaches are used wherever necessary to perform stress and fatigue analyses. Operational flight tests are used for obtaining the loading history at the analyzed location by using sensors. Operational vibration profiles are created by synthesizing the data (LMS Mission Synthesis). Numerical fatigue analysis of the assembly is done for determining the natural modes and the critical locations on the assembly by using a finite element model (MSC Fatigue). In addition, numerical multiaxial PSD analysis is performed for relating the experimental results (Ansys). Residual stresses due to riveting are determined (MSC Marc) and included in experimental analysis as mean stresses. Bolt analysis is performed analytically (Hexagon) for keeping the v assembly stresses in safe levels while mounting the experimental prototype to the test fixture. Fatigue tests for determining the accelerated life parameters are done by an electromagnetic shaker and stress data is collected. Afterwards, fatigue test is performed for determining whether the assembly satisfies the required operational life. Resonance test is performed at the frequency in which the critical location is at resonance, since there was no failure observed after fatigue testing. A failure is obtained during resonance test. At the end of the study, an analytical equation is brought up which relates accelerated life test durations with equivalent alternating stresses. Therefore, optimization of the accelerated life test duration can be done, especially in military applications, by avoiding the maximum stress level to reach or exceed the yield limit.
Livres sur le sujet "Aerospace Structure"
Ryzhikova, tamara. Marketing in the aerospace field. ru : INFRA-M Academic Publishing LLC., 2020. http://dx.doi.org/10.12737/1003199.
Texte intégralH, Laakso John, et Langley Research Center, dir. System integration and demonstration of adhesive bonded high temperature aluminum alloys for aerospace structure : Phase II. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1993.
Trouver le texte intégralCenter, Langley Research, dir. NASA-UVa light aerospace alloy and structure technology program supplement : Aluminum-based materials for high speed aircraft. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1997.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. NASA-UVa light aerospace alloy and structure technology program supplement : Aluminum-based materials for high speed aircraft. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Trouver le texte intégralStarke, E. A. NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement : aluminum-based materials for high speed aircraft. Hampton, Va : Langley Research Center, 1993.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. NASA-UVa light aerospace alloy and structure technology program suppleyment : Aluminum-based materials for high speed aircraft. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Trouver le texte intégralCraig, J. I. (James I.), 1942- et SpringerLink (Online service), dir. Structural analysis : With applications to aerospace structures. Dordrecht : Springer, 2009.
Trouver le texte intégralJ, Loughlan, dir. Aerospace structures. London : Elsevier Applied Science, 1990.
Trouver le texte intégralL, Regel £. L., et United States. National Aeronautics and Space Administration., dir. Modelling directional soldification : Progress report on grant NAG8-831, 1 May 1991 to 31 October 1992. Potsdam, N.Y : Clarkson University, 1991.
Trouver le texte intégralL, Regelʹ L., et United States. National Aeronautics and Space Administration., dir. Modelling directional soldification : Progress report on grant NAG8-831, 1 May 1991 to 31 October 1992. Potsdam, N.Y : Clarkson University, 1991.
Trouver le texte intégralChapitres de livres sur le sujet "Aerospace Structure"
Krumweide, Gary C., et Eddy A. Derby. « Aerospace Equipment and Instrument Structure ». Dans Handbook of Composites, 1004–21. Boston, MA : Springer US, 1998. http://dx.doi.org/10.1007/978-1-4615-6389-1_48.
Texte intégralZhang, Yipeng, Hai Huang et Shenyan Chen. « Structure analysis and optimisation of SSS-1 microsatellite ». Dans Aerospace and Associated Technology, 351–56. London : Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-64.
Texte intégralGunasegeran, Muthukumaran, P. Edwin Sudhagar et A. Ananda Babu. « Failure of Composite Structure ». Dans Repair of Advanced Composites for Aerospace Applications, 103–11. Boca Raton : CRC Press, 2022. http://dx.doi.org/10.1201/9781003200994-9.
Texte intégralArviso, Michael, D. Gregory Tipton et Patrick S. Hunter. « Preliminary Validation of a Complex Aerospace Structure ». Dans Structural Dynamics, Volume 3, 741–51. New York, NY : Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-9834-7_64.
Texte intégralPironneau, Olivier. « Numerical Study of a Monolithic Fluid–Structure Formulation ». Dans Variational Analysis and Aerospace Engineering, 401–20. Cham : Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-45680-5_15.
Texte intégralSanjay, A. V., et B. Sudarshan. « Effect of oblique shocks interaction on the inlet structure in a hypersonic flow ». Dans Aerospace and Associated Technology, 522–27. London : Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-96.
Texte intégralBracco, F. V. « Structure of High-Speed Full-Cone Sprays ». Dans Recent Advances in the Aerospace Sciences, 189–212. Boston, MA : Springer US, 1985. http://dx.doi.org/10.1007/978-1-4684-4298-4_10.
Texte intégralAcharjee, Devjit, Bandyopadhyay et Debasish Bandyopadhyay. « Numerical study of tilted multi-storied RCC buildings on shallow foundations considering soil-structure interaction ». Dans Aerospace and Associated Technology, 284–89. London : Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-51.
Texte intégralKerschen, G., L. Soula, J. B. Vergniaud et A. Newerla. « Assessment of Nonlinear System Identification Methods using the SmallSat Spacecraft Structure ». Dans Advanced Aerospace Applications, Volume 1, 203–19. New York, NY : Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-9302-1_18.
Texte intégralSun, Yixuan, Shikui Luo, Jie Bai, Zijia Liu et Shaofan Tang. « Design and Optimization of the Flexible Support Structure for Space Mirror ». Dans Aerospace Mechatronics and Control Technology, 119–28. Singapore : Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-6640-7_10.
Texte intégralActes de conférences sur le sujet "Aerospace Structure"
Naydenkin, E. V., I. P. Mishin, I. V. Ratochka et V. A. Vinokurov. « High-strength nanostructured titanium alloy for aerospace industry ». Dans ADVANCED MATERIALS WITH HIERARCHICAL STRUCTURE FOR NEW TECHNOLOGIES AND RELIABLE STRUCTURES. AIP Publishing LLC, 2015. http://dx.doi.org/10.1063/1.4932850.
Texte intégralJoshi, Ashok. « Structure - Control Interactions in Flexible Aerospace Vehicles ». Dans 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
18th AIAA/ASME/AHS Adaptive Structures Conference
12th. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-2948.
Mariano, Silvio Luiz, Marcelo Gomes da Silva, André Moreno da Costa Moreira, Everaldo de Barros et Leandro Ribeiro de Camargo. « Modal Correlation of an Aerospace Structure ». Dans 2006 SAE Brasil Congress and Exhibit. 400 Commonwealth Drive, Warrendale, PA, United States : SAE International, 2006. http://dx.doi.org/10.4271/2006-01-2786.
Texte intégralKawabe, Hiroki, Yuichiro Aoki et Toshiya Nakamura. « Biological Optimization of Aerospace Shell Structure ». Dans AIAA SCITECH 2022 Forum. Reston, Virginia : American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-2602.
Texte intégralKim, Seung Jo, Ki-Ook Kim, Jungsun Park, Maenghyo Cho, Eui Sup Shin et Jin Yeon Cho. « Advancements of Aerospace Computational Structure Technology in Korea ». Dans 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-2439.
Texte intégralBlair, Max, et Greg Reich. « A demonstration of CAD/CAM/CAE in a fully associative aerospace design environment ». Dans 37th Structure, Structural Dynamics and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-1630.
Texte intégralELLIS, DAVID. « Overview - Design of an efficient lightweight airframe structure forthe National Aerospace Plane ». Dans 30th Structures, Structural Dynamics and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-1406.
Texte intégralEremenko, A. « Aquarius main structure configuration ». Dans 2013 IEEE Aerospace Conference. IEEE, 2013. http://dx.doi.org/10.1109/aero.2013.6496819.
Texte intégralZorn, Joshua E., et Roger L. Davis. « Structural Dynamics Solution Procedure for Multi-Discipline Fluid/Structure/Thermal Simulation ». Dans 53rd AIAA Aerospace Sciences Meeting. Reston, Virginia : American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-0281.
Texte intégralAlexander, Eric, Ben Carey, Michael DiNardo, Herman Gill, Joey Gonzalez, Mike Harry, Alex Isidro et al. « Validated Aerospace Soft Impact Modeling Platform ». Dans ASME 2012 Fluids Engineering Division Summer Meeting collocated with the ASME 2012 Heat Transfer Summer Conference and the ASME 2012 10th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/fedsm2012-72459.
Texte intégralRapports d'organisations sur le sujet "Aerospace Structure"
Swanson, F., E. Kamykowski, M. Horn et N. Holden. Neutron radiography of aerospace structure hidden corrosion. Office of Scientific and Technical Information (OSTI), septembre 1995. http://dx.doi.org/10.2172/10130409.
Texte intégralFreeman, Arthur J., Oleg Y. Kontsevoi, Yuri N. Gornostyrev et Nadezhda I. Medvedeva. Fundamental Electronic Structure Characteristics and Mechanical Behavior of Aerospace Materials. Fort Belvoir, VA : Defense Technical Information Center, avril 2008. http://dx.doi.org/10.21236/ada480633.
Texte intégralAtluri, S. N. AASERT-Structural Integrity of Aging of Aerospace Structures and Repairs. Fort Belvoir, VA : Defense Technical Information Center, décembre 1996. http://dx.doi.org/10.21236/ada326704.
Texte intégralVenkayya, Vipperla B. Aerospace Structures Design on Computers. Fort Belvoir, VA : Defense Technical Information Center, mars 1989. http://dx.doi.org/10.21236/ada208811.
Texte intégralGrandhi, Ramana V., et Geetha Bharatram. Multiobjective Optimization of Aerospace Structures. Fort Belvoir, VA : Defense Technical Information Center, juillet 1992. http://dx.doi.org/10.21236/ada260433.
Texte intégralFarhat, Charbel. Multidisciplinary Thermal Analysis of Hot Aerospace Structures. Fort Belvoir, VA : Defense Technical Information Center, mai 2010. http://dx.doi.org/10.21236/ada564851.
Texte intégralGrandt, A. F., Farris Jr., Hillberry T. N. et B. H. Analysis of Widespread Fatigue Damage in Aerospace Structures. Fort Belvoir, VA : Defense Technical Information Center, février 1999. http://dx.doi.org/10.21236/ada360820.
Texte intégralSelvam, R. P., et Zu-Qing Qu. Adaptive Navier Stokes Flow Solver for Aerospace Structures. Fort Belvoir, VA : Defense Technical Information Center, mai 2004. http://dx.doi.org/10.21236/ada424479.
Texte intégralAtwood, Clinton J., Thomas Eugene Voth, David G. Taggart, David Dennis Gill, Joshua H. Robbins et Peter Dewhurst. Titanium cholla : lightweight, high-strength structures for aerospace applications. Office of Scientific and Technical Information (OSTI), octobre 2007. http://dx.doi.org/10.2172/922082.
Texte intégralWebb, Philip. Unsettled Issues on the Viability and Cost-Effectiveness of Automation in Aerospace Manufacturing. SAE International, février 2021. http://dx.doi.org/10.4271/epr2021005.
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