Books on the topic 'Composite laminate design'

T, Haftka Raphael, and Hajela Prabhat 1956-, eds. Design and optimization of laminated composite materials. New York: Wiley, 1999.

Rosado, Pablo Rodríguez. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

Rosado, Pablo Rodríguez. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

Rodriguez, P. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

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

Design, Fabrication and Mechanics of Composite Structures Seminar (1984 Arlington, Va.). Design, fabrication and mechanics of composite structures: Seminar notes, reference materials for seminar of May 1-4, 1984, Arlington, VA. Lancaster, PA, USA: Technomic Pub. Co., 1985.

Sun, Guojun. Optimal design of laminated-composite circular-cylindrical shells subjected to combined loads. [S.l.]: American Society of Mechanical Engineers, 1988.

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

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

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

Chattopadhyay, Aditi. Analysis of smart composite structures including debonding. [Washington, DC: National Aeronautics and Space Administration, 1997.

Chattopadhyay, Aditi. Analysis of smart composite structures including debonding. [Washington, DC: National Aeronautics and Space Administration, 1997.

Fan, Mark S. Structural design and analysis of a light-weight laminated composite heat sink for spaceflight PWBs. Washington, D.C: National Aeronautics and Space Administration, 1997.

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

Analysis of failure in fiber polymer laminates: The theory of Alfred Puck. Heidelberg: Springer, 2008.

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

Optimal cure cycle design of a resin-fiber composite laminate. Norfolk, Va: Old Dominion University Research Foundation, 1987.

C, Chamis C., and United States. National Aeronautics and Space Administration., eds. Composite laminate tailoring with probabilistic constraints and loads. [Washington, D.C.]: NASA, 1990.

Peters, S. T., ed. Composite Filament Winding. ASM International, 2011. http://dx.doi.org/10.31399/asm.tb.cfw.9781627083386.

George C. Marshall Space Flight Center., ed. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

Progressive failure analysis methodology for laminated composite structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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.

Analysis of smart composite structures including debonding. [Washington, DC: National Aeronautics and Space Administration, 1997.

Structural design and analysis of a light-weight laminated composite heat sink for spaceflight PWBs. Greenbelt, Md: National Aeronautics and Space Administration, Goddard Space Flight Center, 1997.

Structural design and analysis of a light-weight laminated composite heat sink for spaceflight PWBs. Greenbelt, Md: National Aeronautics and Space Administration, Goddard Space Flight Center, 1997.

A new merit function for evaluating the flaw tolerance of composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

A new merit function for evaluating the flaw tolerance of composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

A new merit function for evaluating the flaw tolerance of composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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.

Knops, Martin. Analysis of Failure in Fiber Polymer Laminates: The Theory of Alfred Puck. Springer, 2010.

Milestone 4: Test plan for reusable hydrogen composite tank system (RHCTS) : task 3, composite tank materials. [Downey, Calif.]: 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). [Downey, Calif.]: 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). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.

Design of test specimens and procedures for generating material properties of Douglas fir-epoxy laminated wood composite material, with the generation of baseline data at two environmental conditions: Final report for period March 1982 through March 1985. Dayton, Ohio: University of Dayton Research Institute, 1985.