Academic literature on the topic 'Aerospace Structure'
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Journal articles on the topic "Aerospace Structure"
RAHIM, Erween, Takayuki OGAWA, Akihiko MIURA, Hiroyuki SASAHARA, Rei Koyasu, and 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_.
Full textDOS SANTOS E LUCATO, S. L., R. M. MCMEEKING, and 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.
Full textBajurko, Piotr. "Modelling of the Aerospace Structure Demonstrator Subcomponent." Transactions on Aerospace Research 2019, no. 1 (March 1, 2019): 37–52. http://dx.doi.org/10.2478/tar-2019-0004.
Full textAl-Madani, Ramadan A., M. Jarnaz, K. Alkharmaji, and M. Essuri. "Finite Element Modeling of Composites System in Aerospace Application." Applied Mechanics and Materials 245 (December 2012): 316–22. http://dx.doi.org/10.4028/www.scientific.net/amm.245.316.
Full textYAMAMOTO, 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.
Full textSainfort, P., Christophe Sigli, G. M. Raynaud, and P. Gomiero. "Structure and Property Control of Aerospace Alloys." Materials Science Forum 242 (January 1997): 25–32. http://dx.doi.org/10.4028/www.scientific.net/msf.242.25.
Full textHorton, B., Y. Song, D. Jegley, F. Collier, and J. Bayandor. "Predictive analysis of stitched aerospace structures for advanced aircraft." Aeronautical Journal 124, no. 1271 (November 18, 2019): 44–54. http://dx.doi.org/10.1017/aer.2019.137.
Full textJiayu, 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.
Full textTADA, 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.
Full textLee, Jong-Woong, Cheol-Won Kong, and 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.
Full textDissertations / Theses on the topic "Aerospace Structure"
Ahn, Junghyun. "Integrated analysis procedure of aerospace composite structure." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/43106.
Full textIncludes 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/.
Full textHu, Zhuopei. "Finite Element Modeling of Aerospace Materials and Structure." University of Akron / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=akron1344224158.
Full textZheng, 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.
Full textSeddon, 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.
Full textBhatti, Wasim. "Mechanical integration of a PEM fuel cell for a multifunctional aerospace structure." Thesis, Loughborough University, 2016. https://dspace.lboro.ac.uk/2134/21513.
Full textPalsule, Sanjay. "Structure and properties of aerospace molecular composites : third generation polymers." Thesis, Heriot-Watt University, 1994. http://hdl.handle.net/10399/1388.
Full textKhataee, Amin. "Structure and properties of some Ti-Al-Ru alloys." Thesis, Imperial College London, 1987. http://hdl.handle.net/10044/1/46915.
Full textLiang, 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.
Full textSeveral 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.
Full text#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.
Books on the topic "Aerospace Structure"
Ryzhikova, tamara. Marketing in the aerospace field. ru: INFRA-M Academic Publishing LLC., 2020. http://dx.doi.org/10.12737/1003199.
Full textH, Laakso John, and Langley Research Center, eds. 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.
Find full textCenter, Langley Research, ed. 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.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. 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.
Find full textStarke, 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.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. 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.
Find full textCraig, J. I. (James I.), 1942- and SpringerLink (Online service), eds. Structural analysis: With applications to aerospace structures. Dordrecht: Springer, 2009.
Find full textJ, Loughlan, ed. Aerospace structures. London: Elsevier Applied Science, 1990.
Find full textL, Regel £. L., and United States. National Aeronautics and Space Administration., eds. Modelling directional soldification: Progress report on grant NAG8-831, 1 May 1991 to 31 October 1992. Potsdam, N.Y: Clarkson University, 1991.
Find full textL, Regelʹ L., and United States. National Aeronautics and Space Administration., eds. Modelling directional soldification: Progress report on grant NAG8-831, 1 May 1991 to 31 October 1992. Potsdam, N.Y: Clarkson University, 1991.
Find full textBook chapters on the topic "Aerospace Structure"
Krumweide, Gary C., and Eddy A. Derby. "Aerospace Equipment and Instrument Structure." In Handbook of Composites, 1004–21. Boston, MA: Springer US, 1998. http://dx.doi.org/10.1007/978-1-4615-6389-1_48.
Full textZhang, Yipeng, Hai Huang, and Shenyan Chen. "Structure analysis and optimisation of SSS-1 microsatellite." In Aerospace and Associated Technology, 351–56. London: Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-64.
Full textGunasegeran, Muthukumaran, P. Edwin Sudhagar, and A. Ananda Babu. "Failure of Composite Structure." In Repair of Advanced Composites for Aerospace Applications, 103–11. Boca Raton: CRC Press, 2022. http://dx.doi.org/10.1201/9781003200994-9.
Full textArviso, Michael, D. Gregory Tipton, and Patrick S. Hunter. "Preliminary Validation of a Complex Aerospace Structure." In 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.
Full textPironneau, Olivier. "Numerical Study of a Monolithic Fluid–Structure Formulation." In Variational Analysis and Aerospace Engineering, 401–20. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-45680-5_15.
Full textSanjay, A. V., and B. Sudarshan. "Effect of oblique shocks interaction on the inlet structure in a hypersonic flow." In Aerospace and Associated Technology, 522–27. London: Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-96.
Full textBracco, F. V. "Structure of High-Speed Full-Cone Sprays." In 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.
Full textAcharjee, Devjit, Bandyopadhyay, and Debasish Bandyopadhyay. "Numerical study of tilted multi-storied RCC buildings on shallow foundations considering soil-structure interaction." In Aerospace and Associated Technology, 284–89. London: Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-51.
Full textKerschen, G., L. Soula, J. B. Vergniaud, and A. Newerla. "Assessment of Nonlinear System Identification Methods using the SmallSat Spacecraft Structure." In 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.
Full textSun, Yixuan, Shikui Luo, Jie Bai, Zijia Liu, and Shaofan Tang. "Design and Optimization of the Flexible Support Structure for Space Mirror." In Aerospace Mechatronics and Control Technology, 119–28. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-6640-7_10.
Full textConference papers on the topic "Aerospace Structure"
Naydenkin, E. V., I. P. Mishin, I. V. Ratochka, and V. A. Vinokurov. "High-strength nanostructured titanium alloy for aerospace industry." In ADVANCED MATERIALS WITH HIERARCHICAL STRUCTURE FOR NEW TECHNOLOGIES AND RELIABLE STRUCTURES. AIP Publishing LLC, 2015. http://dx.doi.org/10.1063/1.4932850.
Full textJoshi, Ashok. "Structure - Control Interactions in Flexible Aerospace Vehicles." In 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, and Leandro Ribeiro de Camargo. "Modal Correlation of an Aerospace Structure." In 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.
Full textKawabe, Hiroki, Yuichiro Aoki, and Toshiya Nakamura. "Biological Optimization of Aerospace Shell Structure." In AIAA SCITECH 2022 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-2602.
Full textKim, Seung Jo, Ki-Ook Kim, Jungsun Park, Maenghyo Cho, Eui Sup Shin, and Jin Yeon Cho. "Advancements of Aerospace Computational Structure Technology in Korea." In 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.
Full textBlair, Max, and Greg Reich. "A demonstration of CAD/CAM/CAE in a fully associative aerospace design environment." In 37th Structure, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-1630.
Full textELLIS, DAVID. "Overview - Design of an efficient lightweight airframe structure forthe National Aerospace Plane." In 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.
Full textEremenko, A. "Aquarius main structure configuration." In 2013 IEEE Aerospace Conference. IEEE, 2013. http://dx.doi.org/10.1109/aero.2013.6496819.
Full textZorn, Joshua E., and Roger L. Davis. "Structural Dynamics Solution Procedure for Multi-Discipline Fluid/Structure/Thermal Simulation." In 53rd AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-0281.
Full textAlexander, Eric, Ben Carey, Michael DiNardo, Herman Gill, Joey Gonzalez, Mike Harry, Alex Isidro, et al. "Validated Aerospace Soft Impact Modeling Platform." In 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.
Full textReports on the topic "Aerospace Structure"
Swanson, F., E. Kamykowski, M. Horn, and N. Holden. Neutron radiography of aerospace structure hidden corrosion. Office of Scientific and Technical Information (OSTI), September 1995. http://dx.doi.org/10.2172/10130409.
Full textFreeman, Arthur J., Oleg Y. Kontsevoi, Yuri N. Gornostyrev, and Nadezhda I. Medvedeva. Fundamental Electronic Structure Characteristics and Mechanical Behavior of Aerospace Materials. Fort Belvoir, VA: Defense Technical Information Center, April 2008. http://dx.doi.org/10.21236/ada480633.
Full textAtluri, S. N. AASERT-Structural Integrity of Aging of Aerospace Structures and Repairs. Fort Belvoir, VA: Defense Technical Information Center, December 1996. http://dx.doi.org/10.21236/ada326704.
Full textVenkayya, Vipperla B. Aerospace Structures Design on Computers. Fort Belvoir, VA: Defense Technical Information Center, March 1989. http://dx.doi.org/10.21236/ada208811.
Full textGrandhi, Ramana V., and Geetha Bharatram. Multiobjective Optimization of Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, July 1992. http://dx.doi.org/10.21236/ada260433.
Full textFarhat, Charbel. Multidisciplinary Thermal Analysis of Hot Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, May 2010. http://dx.doi.org/10.21236/ada564851.
Full textGrandt, A. F., Farris Jr., Hillberry T. N., and B. H. Analysis of Widespread Fatigue Damage in Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, February 1999. http://dx.doi.org/10.21236/ada360820.
Full textSelvam, R. P., and Zu-Qing Qu. Adaptive Navier Stokes Flow Solver for Aerospace Structures. Fort Belvoir, VA: Defense Technical Information Center, May 2004. http://dx.doi.org/10.21236/ada424479.
Full textAtwood, Clinton J., Thomas Eugene Voth, David G. Taggart, David Dennis Gill, Joshua H. Robbins, and Peter Dewhurst. Titanium cholla : lightweight, high-strength structures for aerospace applications. Office of Scientific and Technical Information (OSTI), October 2007. http://dx.doi.org/10.2172/922082.
Full textWebb, Philip. Unsettled Issues on the Viability and Cost-Effectiveness of Automation in Aerospace Manufacturing. SAE International, February 2021. http://dx.doi.org/10.4271/epr2021005.
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