Books on the topic 'Low-velocity impact'

Al-Jolahy, A. M. Low velocity impact by flat ended indenter. Manchester: UMIST, 1997.

Srinivasan, K. Response of composite materials to low velocity impact. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Bower, Mark V. Investigation of low velocity impact damage on filamentary composite materials. Huntsville, Ala: University of Alabama in Huntsville, 1987.

J, Douglas M., and George C. Marshall Space Flight Center., eds. A comparison of quasi-static indentation to low-velocity impact. MSFC, AL: National Aeronautics and Space Administration, Marshall Space Flight Center, 2000.

V, Sankar Bhavani, and Langley Research Center, eds. Indentation-flexure and low-velocity impact damage in graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

V, Sankar Bhavani, and Langley Research Center, eds. Indentation-flexure and low-velocity impact damage in graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Lance, D. G. Low velocity instrumented impact testing of four new damage tolerant carbon/epoxy composite systems. Huntsville, Ala: George C. Marshall Space Flight Center, 1990.

Kelkar, Ajit Dhundiraj. Analyses of quasi-isotropic composite plates under quasi-static point loads simulating low-velocity impact phenomena. Norfolk, Va: Old Dominion University, 1985.

Lymer, John Douglas. The characterization of low velocity impact damage in composite materials using an embedded optical fibre assessment system. [Downsview, Ont.]: Department of Aerospace Science and Engineering, 1988.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Acoustic emission monitoring of low velocity impact damage in graphite/epoxy laminates during tensile loading. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Acoustic emission monitoring of low velocity impact damage in graphite/epoxy laminates during tensile loading. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United States. National Aeronautics and Space Administration., ed. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration., ed. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration, ed. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration., ed. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration, ed. The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

Liebowitz, Harold. The effect of low velocity impact on the strength characteristics of composite materials laminates: End of the year progress report. Washington, D.C: George Washington University, 1986.

Rühl, Andreas. On the Time and Temperature Dependent Behaviour of Laminated Amorphous Polymers Subjected to Low-Velocity Impact. Berlin, Heidelberg: Springer Berlin Heidelberg, 2017. http://dx.doi.org/10.1007/978-3-662-54641-3.

Imielińska, Krystyna. Degradation and damage of advanced laminate polymer composites due to environmental effects and low velocity impact. Gdańsk: Politechnika Gdańska, 2005.

United States. National Aeronautics and Space Administration., ed. A COMPARISON OF QUASI-STATIC INDENTATION TO LOW-VELOCITY IMPACT... NASA/TP-2000-210481... DEC. 6, 2000. [S.l: s.n., 2003.

United States. National Aeronautics and Space Administration., ed. A COMPARISON OF QUASI-STATIC INDENTATION TO LOW-VELOCITY IMPACT... NASA/TP-2000-210481... DEC. 6, 2000. [S.l: s.n., 2003.

United States. National Aeronautics and Space Administration., ed. A COMPARISON OF QUASI-STATIC INDENTATION TO LOW-VELOCITY IMPACT... NASA/TP-2000-210481... DEC. 6, 2000. [S.l: s.n., 2003.

United States. National Aeronautics and Space Administration., ed. A study of the use of contact loading to simulate low velocity impact: Final report, NASA grant no. NASA NCC8-23. [Washington, DC: National Aeronautics and Space Administration, 1997.

Center, Langley Research, ed. Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Farley, Gary L. Effect of low-velocity or ballistic impact damage on the strength of thin composite and aluminum shear panels. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Farley, Gary L. Effect of low-velocity or ballistic impact damage on the strength of thin composite and aluminum shear panels. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Liebowitz, Harold. The effect of low velocity impact in the strength characteristics of composite materials laminates: End of the year progress report, NASA grant NAG 1-158. Washington, D.C: School of Engineering and Applied Science, George Washington University, 1986.

W, Illg, Garber D. P, and Langley Research Center, eds. A program to determine the effect of low-velocity impacts on the strength of the filament-wound rocket motor case for the space shuttle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Low-Velocity Impact on Composite Sandwich Plates. Storming Media, 1996.

National Aeronautics and Space Administration (NASA) Staff. Comparison of Quasi-Static Indentation to Low-Velocity Impact. Independently Published, 2018.

National Aeronautics and Space Administration (NASA) Staff. Indentation-Flexure and Low-Velocity Impact Damage in Graphite/Epoxy Laminates. Independently Published, 2018.

National Aeronautics and Space Administration (NASA) Staff. Study of the Use of Contact Loading to Simulate Low Velocity Impact. Independently Published, 2018.

Singh, Kalyan Kumar, and Mahesh Shinde. Impact Behavior of Fibre Reinforced Laminates: Fundamentals of Low Velocity Impact and Related Literature on FRP. Springer Singapore Pte. Limited, 2022.

National Aeronautics and Space Administration (NASA) Staff. Low Velocity Instrumented Impact Testing of Four New Damage Tolerant Carbon/Epoxy Composite Systems. Independently Published, 2018.

The correlation of low-velocity impact resistance of graphite-fiber-reinforced composites with matrix properties. [Washington, D.C: National Aeronautics and Space Administration, 1986.

Summary and evaluation of low-velocity impact tests of solid steel billet onto concrete pads. Washington, DC: Spent Fuel Project Office, Office of Nuclear Material Safety and Safeguards, U.S. Nuclear Regulatory Commission, 1998.

Rühl, Andreas. On the Time and Temperature Dependent Behaviour of Laminated Amorphous Polymers Subjected to Low-Velocity Impact. Springer Berlin / Heidelberg, 2017.

Lymer, John Douglas *. The characterization of low velocity impact damage in composite materials using an embedded optical fibre assessment system. 1988.