Books on the topic 'Test structure design'

Japan) Workshop on Modeling of Dynamic Behavior of Wood Structure (1997 Tsukuba-shi. Workshop on Modeling of Dynamic Behavior of Wood Structure: 11-12 December 1997 ; visual projection room of BRI, with eventual move for observation of a shaking table test at National Disaster Prevention Research Institute. Building Research Institute, Ministry of Construction, Japan, 2000.

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format in composite structure design. College of Engineering, Virginia Polytechnic Institute and State University, 1990.

George C. Marshall Space Flight Center., ed. Hybrid residual flexibility/mass-additive method for structural dynamic testing. National Aeronautics and Space Administration, Marshall Space Flight Center, 2003.

Borri, Claudio, and Claudio Mannini, eds. Aeroelastic Phenomena and Pedestrian-Structure Dynamic Interaction on Non-Conventional Bridges and Footbridges. Firenze University Press, 2010. http://dx.doi.org/10.36253/978-88-6453-202-8.

Liu, Jun, Zhufeng Yue, Xiaoliang Geng, Shifeng Wen, and Wuzhu Yan. Long-Life Design and Test Technology of Typical Aircraft Structures. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-8399-0.

Taylor, David. Design of certain silicon semi-customized structures incorporating self-test. The Polytechnic, 1989.

Gdanskiy, Nikolay. Fundamentals of the theory and algorithms on graphs. INFRA-M Academic Publishing LLC., 2020. http://dx.doi.org/10.12737/978686.

Childs, Dara W. Design review and analysis for a Pratt & Whitney fluid-film bearing and seal testing rig: Final report. National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Design review and analysis for a Pratt & Whitney fluid-film bearing and seal testing rig: Final report. National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Milestone 4: Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). Rockwell Aerospace, Space Systems Division, 1994.

United States. National Aeronautics and Space Administration., ed. Milestone 4: Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). Rockwell Aerospace, Space Systems Division, 1994.

Center, Langley Research, ed. Experimental validation of an integrated controls-structures design methodology for a class of flexible space structures. National Aeronautics and Space Administration, Langley Research Center, 1994.

National Cooperative Highway Research Program and National Research Council (U.S.). Transportation Research Board, eds. Structural design of culvert joints. National Cooperative Highway Research Program, Transportation Research Board of the National Academies, 2012.

Sysoevam, Elena, Sergey Trushin, Vladimir Konovalov, Vladimir Gur'ev, and Vyacheslav Etenko. Architectural structures and design theory: Low-rise residential buildings. INFRA-M Academic Publishing LLC., 2023. http://dx.doi.org/10.12737/1921385.

Hyer, M. W. Innovative design of composite structures: Further studies in the use of a curvilinear fiber format to improve structural efficiency. College of Engineering, Virginia Polytechnic Institute and State University, 1988.

J, Hooper Steven, Nicholson Mark, and Langley Research Center, eds. Design and test of an improved crashworthiness small composite airframe. National Aeronautics and Space Administration, Langley Research Center, 2002.

L, Oates David, Gonsalez Jose C, and Hugh L. Dryden Flight Research Center., eds. Design and evaluation of a new boundary-layer rake for flight testing. National Aeronautics and Space Administration, Dryden Flight Research Center, 2000.

Krishnaswamy, Smita. Design, Analysis and Test of Logic Circuits Under Uncertainty. Springer Netherlands, 2013.

Lavoie, J. Andre. Design and application of a quasistatic crush test fixture for investigating scale effects in energy absorbing composite plates. Langley Research Center, 1993.

Ahmed, R. Design and test of low-profile composite aerospace tank dome: (MSFC Center Director's Discretionary Fund final report, project no. 96-28). National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.

George C. Marshall Space Flight Center., ed. Design and test of low-profile composite aerospace tank dome: (MSFC Center Director's Discretionary Fund final report, project no. 96-28). National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.

George C. Marshall Space Flight Center., ed. Design and test of low-profile composite aerospace tank dome: (MSFC Center Director's Discretionary Fund final report, project no. 96-28). National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.

Perry, William E. A structured approach to systems testing. 2nd ed. QED Information Sciences, 1988.

Chamis, C. C. Computational engine structural analysis. National Aeronautics and Space Administration, Lewis Research Center, 1986.

T, Carter Michael, and Langley Research Center, eds. Near minimum-time maneuvers of the Advanced Space Structures Technology Research Experiment (ASTREX) test article: Theory and experiments. National Aeronautics and Space Administration, Langley Research Center, 1994.

T, Carter Michael, and Langley Research Center, eds. Near minimum-time maneuvers of the Advanced Space Structures Technology Research Experiment (ASTREX) test article: Theory and experiments. National Aeronautics and Space Administration, Langley Research Center, 1994.

Hyer, M. W. Innovative design of composite structures: Design, manufacturing, and testing of plates utilitzing [sic] curvilinear fiber trajectories : final report for NASA. College of Engineering, Virginia Polytechnic Institute and State University ; Hampton, VA, 1994.

Paoletti, Paolo. Il Ponte a Santa Trinita: Com'era e dov'era : dalla distruzione nel 1944 al ritrovamento della testa della primavera nel 1961. Becocci, 1987.

Bazhenov, V. I. Modeling the fundamental characteristics and processes of spacecraft functioning. National Aeronautics and Space Administration, 1986.

E, Neff R., Ford Aerospace & Communications Corporation., and Lewis Research Center, eds. Space station experiment definition: Advanced power system test bed : final report, 15 December 1986 / H.E. Pollard, R.E. Neff. Ford Aerospace & Communication Corporation, 1986.

Julien, J. T. Leak and structural test of personnel airlock for LWR containments subjected to pressures and temperatures beyond design limits. Division of Engineering, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1989.

F, Seible, and United States. National Aeronautics and Space Administration., eds. Comparison of NASTRAN analysis with ground vibration results of UH-60A NASA/AEFA test configuration: Structural systems research project : final contractor report for NASA ARC contract NCC2-598. Dept. of Applied Mechanics and Engineering Sciences, University of California, San Diego, 1990.

L, Frost C., Engel Carl D, and George C. Marshall Space Flight Center., eds. SRB ascent aerodynamic heating design criteria reduction study: Final report. Renault Vehicles Industriels, 1989.

Sanatan, Chattopadhyay, Chattopadhyay Santanu, and SpringerLink (Online service), eds. Progress in VLSI Design and Test: 16th International Symposium, VDAT 2012, Shibpur, India, July 1-4, 2012. Proceedings. Springer Berlin Heidelberg, 2012.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, ed. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Richards, W. Lance. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Haldimann, Matthias, Andreas Luible, and Mauro Overend. Structural use of Glass. International Association for Bridge and Structural Engineering (IABSE), 2008. http://dx.doi.org/10.2749/sed010.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Impact of emerging NDE-NDI methods on aircraft design, manufacture and maintenance: papers presented at the 69th Meeting of the Structures and Materials Panel in Brussels, Belgium, 1st-6th October 1989. Advisory Group for Aerospace Research & Development, 1990.

Operations, Thiokol Corporation Space, and George C. Marshall Space Flight Center., eds. QM-8 final performance evaluation report. Thiokol Corp., Space Operations, 1989.

Operations, Thiokol Corporation Space, and George C. Marshall Space Flight Center., eds. QM-8 final performance evaluation report. Thiokol Corp., Space Operations, 1989.

Hiel, C. Snaplock fiber reinforced composites technology applied to overhead sign structures: Design, construct, and test a fiber reinforced composite overhead sign truss. California Dept. of Transportation, Division of Research and Innovation, 2008.

Hyer, M. W. Innovative design of composite structures: Axisymmetric deformations of unsymmetrically laminated cylinders loaded in axial compression : semiannual status report. College of Engineering, Virginia Polytechnic Institute and State University, 1990.