Books on the topic 'Thick Composites'

H, Williams James. Modes of vibration on square fiberglass epoxy composite thick plate. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Y, Rajapakse, American Society of Mechanical Engineers. Applied Mechanics Division., and Joint Mechanics Meeting of ASME, ASCE, SES (1st : 1993 : Charlottesville, Va.), eds. Mechanics of thick composites: Presented at the 1st Joint Mechanics Meeting of ASME, ASCE, SES, MEET'N '93, Charlottesville, Virginia, June 6-9, 1993. New York: American Society of Mechanical Engineers, 1993.

Peretz, Friedmann, Kosmatka J. B, American Society of Mechanical Engineers. Aerospace Division., and American Society of Mechanical Engineers. Winter Meeting, eds. Recent advances in the structural dynamic modeling of composite rotor blades and thick composites: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Anaheim, California, November 8-13, 1992. New York: ASME, 1992.

Lee, Sung W., ed. Advances in Thick Section Composite and Sandwich Structures. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-31065-3.

Arnold, S. M. A thermoelastic transversely isotropic thick walled cylinder/disk application: An analytical solution and study. Cleveland, Ohio: Lewis Research Center, 1989.

Damage Tolerance of Thick-Section Composites Subjected to Ballistic Impact. Storming Media, 2001.

C, Smith, Lumban-Tobing F, and Langley Research Center, eds. Analysis of thick sandwich shells with embedded ceramic tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

United States. National Aeronautics and Space Administration, ed. Ultrasonic evaluation of mechanical properties of thick, multilayered, filament wound composites. [Washington, D.C: National Aeronautics and Space Administration, 1985.

C, Marques Elizabeth R., Lee Samson S, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Massachusetts Institute of Technology, and Lewis Research Center, eds. Modes of vibration on square fiberglass epoxy composite thick plate. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

T, Nettles A., and George C. Marshall Space Flight Center., eds. A novel method of testing the shear strength of thick honeycomb composites. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

United States. National Aeronautics and Space Administration., ed. Optimal cure cycle design for autoclave processing of thick composites laminates: A feasibility study. Norfolk, Va: Old Dominion University Research Foundation, 1985.

Friedmann, Peretz. Recent Advances in the Structural Dynamic Modeling of Composite Rotor Blades and Thick Composites: Presented at the Winter Annual Meeting of the Ameri (AMD). American Society of Mechanical Engineers, 1992.

Y, Rajapakse, Kardomateas George A, American Society of Mechanical Engineers. Applied Mechanics Division., and International Mechanical Engineering Congress and Exposition (1999 : Nashville, Tenn.), eds. Thick composites for load bearing structures: Presented at the 1999 ASME International Mechanical Engineering Congress and Exposition, November 14-19, 1999, Nashville, Tennessee. New York: American Society of Mechanical Engineers, 1999.

American Society of Mechanical Engineers. Applied Mechanics Division (Corporate Author), Yapa D. S. Rajapakse (Editor), George A. Kar (Editor), and George A. Kardomateas (Editor), eds. Thick Composites for Load Bearing Structures: Presented at the 1999 Asme International Mechanical Engineering Congress and Exposition, November 14-19, ... Tennessee (Ams Series, Volume 235). Amer Society of Mechanical, 1999.

Center, Langley Research, ed. Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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.

ASCE, SES (1st : 1993 : Charlottesville, Va.) Joint Mechanics Meeting of ASME. Mechanics of Thick Composites: Presented at the 1st Joint Mechanics Meeting of Asme, Asce, Ses-Meet'N'93, Charlottesville, Virginia, June 6-9, 1993 (Amd (Series), Vol. 162.). American Society of Mechanical Engineers, 1993.

E, Harris C., Morris D. H, and Langley Research Center, eds. Surface crack analysis applied to impact damage in a thick graphite/epoxy composite. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Combining Minds: How to Think about Composite Subjectivity. Oxford University Press, 2019.

A thermoelastic transversely isotropic thick walled cylinder/disk application: An analytical solution and study. Cleveland, Ohio: Lewis Research Center, 1989.

Zafer, Gürdal, and United States. National Aeronautics and Space Administration., eds. Compression of thick laminated composite beams with intitial impact-like damage. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1992.

Kennedy, Graeme. Manufacturing process optimization for improved failure performance of thick composite structures. 2007.

R, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

R, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

R, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

National Aeronautics and Space Administration (NASA) Staff. Compression of Thick Laminated Composite Beams with Initial Impact-Like Damage. Independently Published, 2018.

Walter, Illg, and Langley Research Center, eds. Strength of a thick graphite/epoxy rocket motor case after impact by a blunt object. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

National Aeronautics and Space Administration (NASA) Staff. Surface Crack Analysis Applied to Impact Damage in a Thick Graphite-Epoxy Composite. Independently Published, 2018.

United States. National Aeronautics and Space Administration., ed. Integrated analysis and design of thick composite structures for optimal passive damping characteristics. [Washington, D.C.]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. [Damage assessment and residual compression strength of thick composite plates with through-the-thickness reinforcements]: Semi-annual report for NASA grant NAG-1-1063, period: November 1, 1989 - June 1, 1990. [Washington, D.C.?: National Aeronautics and Space Administration, 1990.

Lee, Sung W. Advances in Thick Section Composite and Sandwich Structures: An Anthology of ONR-Sponsored Research. Springer International Publishing AG, 2021.

Lee, Sung W. Advances in Thick Section Composite and Sandwich Structures: An Anthology of ONR-sponsored Research. Springer, 2020.

Wellinski Morgan WELLINSKI MORGAN D. What Do You Think Success in Charlie Mackesy Framed Journal for Men and Women: What Do You Think Success in Charlie Mackesy Framed Journal to Write in with Inspirational Quotes and LoveWhat Do You Think Success in Charlie Mackesy Framed Gift, Compositio. Independently Published, 2021.

Notebook, Elephant. Betrong As an Elephant : Gray Softcover Notebook Diary with Elephant Design - Durable, Composite Leather Journal with Extra-Thick Lined Pages - Great for Kids, 6 by 9 Inches with 110 Pages: Office Products. Independently Published, 2020.

Notebook, Elephant. ZYWJUGE Be Strong Notebook : Gray Softcover Notebook Diary with Elephant Design - Durable, Composite Leather Journal with Extra-Thick Lined Pages - Great for Kids, 6 by 9 Inches with 110 Pages: Office Products. Independently Published, 2020.