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Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite,

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] 2012

Boeing/NASA composite components flight service evaluation

Coggeshall, Randy L.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

Composite structures damage tolerance analysis methodologies

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] 2012

Compression after impact experiments and analysis on honeycomb core sandwich panels with thin facesh

McQuigg, Thomas D.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Compressive testing of stitched frame and stringer alternate configurations

Leone, Frank A., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2016. 2016-

Delamination growth in composite materials

Newark, Del. : Center for Composite Materials, College of Engineering, University of Delaware ; [Washington, D.C.] : National Aeronautics and Space Administration, [1985?] 1985

Development of an advanced composite aileron for the L-1011 transport aircraft

Griffin, C. F. (Charles Francis), 1944-
[Washington, D.C.?] : National Aeronautics and Space Admininstration, Scientific and Technical Information Branch, 1982. 1982

Effect of stress concentrations in composite structures progress report

Babcock, Charles D.
Pasadena CA : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration, 1985] 1985

The effects of foam thermal protection system on the damage tolerance characteristics of composite s

Nettles, A. T. (Alan T.)
[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011] 2011

Evaluation of capillary reinforced composites by Samuel W. Ciardullo and Lewis J. Stoffer.

Ciardullo, Samuel W.
Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group ; [Cleveland, Ohio] : National Aeronautics and Space Administration, NASA Lewis Research Center, [1985] 1985

The exact solution for linear thermoelastic axisymmetric deformations of generally laminated circula

Nemeth, Michael P., author.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] 2012

Finite element analysis of composite joint configurations with gaps and overlaps

Krueger, Ronald, author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2014. 2014-

In-situ investigation of advanced structural coatings and composites

Ustundag, Ersan.
[Cleveland, Ohio] : National Aeronautics and Space Administration, [Glenn Research Center, 2003] 2003

Innovative design of composite structures the use of curvilinear fiber format in composite structure

Hyer, M. W.
Blacksburg, VA : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1990] 1990

Innovative design of composite structures the use of curvilinear fiber format to improve buckling re

Hyer, M. W.
Blacksburg, VA : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1990] 1990

Investigation of the thermomechanical response of shape memory alloy hybrid composite beams

Davis, Brian A.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005] 2005

A life prediction model for laminated composite structural components final technical report

College Station, Texas : Mechanics and Materials Center, Texas A&M University ; Hampton, VA : NASA Langley Research Center, [1990] 1990

LSP composite susbrtrate manufacturing processing guide

Kovach, Daniel J., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013. 2013-

Modeling of composite beams and plates for static and dynamic analysis

Hodges, Dewey H.
Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology, [1990] 1990

A new technique for simulating composite material final report

Volakis, John Leonidas, 1956-
Ann Arbor, Mich. : University of Michigan, Radiation Laboratory, Dept. of Electrical Engineering and Computer Science ; [Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1991] 1991

Observation of the initiation and progression of damage in compressively loaded composite plates con

Waas, Anthony M.
Pasadena, Calif. : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, D.C.? : National Aeronautics and Space Administration, 1986] 1986

Open circuit resonant sensors for composite damage detection and diagnosis

Mielnik, John J.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Probability techniques for reliability analysis of composite materials

Wetherhold, Robert C.
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994] 1994

Progressive fracture of fiber composite thin shell structures under internal pressure and axial load

Cios, Krzysztof J., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, September 1996. 1996-

A protection and detection surface (PADS) for damage tolerance

Shuart, Mark J.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

Relationship between mechanical-property and energy-absorption trends for composite tubes

Farley, Gary L.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992. 1992

Reliability, risk and cost trade-offs for composite designs

Shiao, Michael C., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996. 1996-

Research in structures, structural dynamics, and materials, 1989 work-in-progress and other special

AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (30th : 1989 : Mobile, Ala.)
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989] 1989

Skin/stiffener interface stresses in composite stiffened panels

Wang, James Ting-Shun.
Marietta, Ga. : Lockheed-Georgia Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984] 1984

Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open se

Collins, J. Scott.
Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University, [1989] 1989

Structural tests and development of a laminar flow control wing surface composite chordwise joint

Lineberger, L. B.
Marietta, Ga. : Lockheed-Georgia Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984] 1984

A study of the utilization of advanced composites in fuselage structures of commercial aircraft fina

Long Beach, Calif. : Douglas Aircraft Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

Transport composite fuselage technology impact dynamics and acoustic transmission

Burbank, Calif. : Lockheed-California Co. ; [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986. 1986

Validation of design and analysis techniques of tailored composite structures

Wijayratne, Dulnath D.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2004] 2004