Books on the topic 'Composite structure model'
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G, Wadley H. N., and Lewis Research Center, eds. Cost models for MMC manufacturing processes: Tog. National Aeronautics and Space Administration, [Lewis Research Center, 1996.
Find full textSaravanos, D. A. An integrated methodology for optimizing structural composite damping. Lewis Research Center, 1989.
Find full textC, Chamis C., and Lewis Research Center, eds. An integrated methodology for optimizing structural composite damping. Lewis Research Center, 1989.
Find full textV, Sankar Bhavani, and Langley Research Center, eds. Micromechanical models for textile structural composites. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textSaravanos, D. A. Computational simulation of damping in composite structures. National Aeronautics and Space Administration, 1990.
Find full textC, Chamis C., and United States. National Aeronautics and Space Administration., eds. Computational simulation of damping in composite structures. National Aeronautics and Space Administration, 1990.
Find full textXiong, Y. A design model for composite joints with multiple fasteners. National Research Council Canada, Institute for Aerospace Research, 1994.
Find full textR, Ambur Damodar, and United States. National Aeronautics and Space Administration., eds. Response of composite panels with stiffness gradients due to stiffener terminations and cutouts. National Aeronautics and Space Administration, 1997.
Find full textLazić, Vera B. Mathematical theory of composite and prestressed structures. Matematički institut SANU, 2003.
Find full textKolpakov, A. G. Stressed Composite Structures: Homogenized Models for Thin-Walled Nonhomogeneous Structures with Initial Stresses. Springer Berlin Heidelberg, 2004.
Find full textChattopadhyay, Aditi. Analysis of smart composite structures including debonding. National Aeronautics and Space Administration, 1997.
Find full textChattopadhyay, Aditi. Analysis of smart composite structures including debonding. National Aeronautics and Space Administration, 1997.
Find full textE, Seeley Charles, McGowan Anna, and United States. National Aeronautics and Space Administration., eds. Modeling and analysis of composite wing sections for improved aeroelastic and vibration characteristics using smart materials. National Aeronautics and Space Administration, 1996.
Find full textKolundžija, Branko M. Electromagnetic modeling of composite metallic and dielectric structures. Artech House, 2002.
Find full textJ, Sutliff Thomas, and United States. National Aeronautics and Space Administration., eds. Structural dynamic testing of composite propfan blades for a cruise missile wind tunnel model. National Aeronautics and Space Administration, 1993.
Find full textAllen, David H. Analysis of static contact in laminated composite plates using damage mechanics: Final technical report. NASA Langley Research Center, 1995.
Find full textCenter, Langley Research, ed. Analysis of static contact in laminated composite plates using damage mechanics: Final technical report. NASA Langley Research Center, 1995.
Find full textH, Allen David, Texas A & M University. Mechanics and Materials Center., and Langley Research Center, eds. A life prediction model for laminated composite structural components: Final technical report. Mechanics and Materials Center, Texas A&M University, 1990.
Find full textUnited States. National Aeronautics and Space Administration., ed. Buckling and damage resistance of transversely-loaded composite shells. National Aeronautics and Space Administration, 1998.
Find full textMira, Mitra, ed. Wavelet methods for dynamical problems: With application to metallic, composite, and nano-composite structures. Taylor & Francis, 2010.
Find full textC, Chamis C., Murthy P. L. N, and United States. National Aeronautics and Space Administration., eds. Structural behavior of composites with progressive fracture. NASA, 1990.
Find full textL, Boitnott Richard, Fasanella Edwin L, Langley Research Center, and United States. Army Aviation Systems Command., eds. Behavior of composite/metal aircraft structural elements and components under crash type loads: What are they telling us? National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textL, Boitnott Richard, Fasanella Edwin L, Langley Research Center, and United States. Army Aviation Systems Command., eds. Behavior of composite/metal aircraft structural elements and components under crash type loads: What are they telling us? National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textCenter, Langley Research, ed. Delamination modeling of composites for improved crash analysis. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textCenter, Langley Research, ed. Delamination modeling of composites for improved crash analysis. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textCarden, Huey D. Unique failure behavior of metal/composite aircraft structural components under crash type loads. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textL, Fasanella Edwin, and Langley Research Center, eds. Crashworthy evaluation of a 1/5-scale model composite fuselage concept. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textL, Fasanella Edwin, and Langley Research Center, eds. Crashworthy evaluation of a 1/5-scale model composite fuselage concept. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textL, Fasanella Edwin, and Langley Research Center, eds. Crashworthy evaluation of a 1/5-scale model composite fuselage concept. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textG, Rojas R., and Langley Research Center, eds. Electromagnetic on-aircraft antenna radiation in the presence of composite plates. The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering, 1994.
Find full textG, Rojas R., and Langley Research Center, eds. Electromagnetic on-aircraft antenna radiation in the presence of composite plates. The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering, 1994.
Find full textG, Rojas R., and Langley Research Center, eds. Electromagnetic on-aircraft antenna radiation in the presence of composite plates. The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering, 1994.
Find full textC, Chamis C., and United States. National Aeronautics and Space Administration., eds. Structural durability of damaged metallic panel repaired with composite patches. National Aeronautics and Space Administration, 1997.
Find full textC, Chamis C., and United States. National Aeronautics and Space Administration., eds. Structural durability of damaged metallic panel repaired with composite patches. National Aeronautics and Space Administration, 1997.
Find full textNemirovskiĭ, I︠U︡ V. Teploprovodnostʹ odnorodnykh i kompozitnykh tonkostennykh konstrukt︠s︡iĭ. Izd-vo "Art-Aveni︠u︡", 2009.
Find full textCarden, Huey D. Free vibrations of thin-walled semicircular graphite epoxy composite frames. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textCarden, Huey D. Free vibrations of thin-walled semicircular graphite epoxy composite frames. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textCarden, Huey D. Free vibrations of thin-walled semicircular graphite epoxy composite frames. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textCarden, Huey D. Free vibrations of thin-walled semicircular graphite epoxy composite frames. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textF, Hunter William, Noor Ahmed Khairy 1938-, and Langley Research Center, eds. Research in structures, structural dynamics, and materials, 1989: Work-in-progress and other special presentation papers presented at the AIAA/ASME/ASCE/AHS/ASC 30th Structures, Structural Dynamics, and Materials Conference held in Mobile, Alabama, April 3-5, 1989. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textKolpakov, A. A. Capacity and transport in contrast composite structures: Asymptotic analysis and applications. Taylor & Francis, 2010.
Find full textC, Wetherhold Robert, and Lewis Research Center, eds. Reliability analysis of continuous fiber composite laminates. National Aeronautics and Space Administration, Lewis Research Center, 1990.
Find full textCarek, David A. Structural analysis of high-rpm composite propfan blades for a cruise missle wind tunnel model. National Aeronautics and Space Administration, 1993.
Find full textCarek, David A. Structural analysis of high-rpm composite propfan blades for a cruise missle wind tunnel model. National Aeronautics and Space Administration, 1993.
Find full textE, Harris Charles, and United States. National Aeronautics and Space Administration., eds. Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue. National Aeronautics and Space Administration, 1995.
Find full textCenter, Langley Research, ed. Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textKędziora, Piotr. Optymalne projektowanie struktur kompozytowych z warstwami piezoelektrycznymi: Optimal design of composite structures with piezoelectric layers = Optimale Projektierung der Verbundwerkstoffstrukturen mit piezoelektrischen Schichten. Wydawnictwo PK, 2013.
Find full textUnited States. National Aeronautics and Space Administration., ed. Design protocols and analytical strategies that incorporate structural reliabilty models: Final report. Cleveland State University, 1995.
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