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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

An Approximate solution and master curves for buckling of symmetrically laminated composite cylinder

Nemeth, Michael P., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013. 2013

Autoclave processing for composite material fabrication. 1. An analysis of resin flows and fiber com

Hou, T. H.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

Comparison of open-hole compression strength and compression after impact strength on carbon fiber/e

Hodge, A. J.
[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011] 2011

Composite transport wing technology development

Madan, Ram C.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1988] 1988

Design and manufacture of elastically tailored tow placed plates

Tatting, Brian F.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002] 2002

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

Evaluation of energy absorption of new concepts of aircraft composite subfloor intersections

Jones, Lisa E.
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va, : For sale by the National Technical Information Service. 1989] 1989

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

Fatigue damage in notched composite laminates under tension-tension cyclic loads

Blacksburg, Va. : Virginia Tech, Center for Composite Materials and Structures ; Hampton, Va. : NASA Langley Research Center, [1985] 1985

An improved compression molding technology for continuous fiber reinforced composite laminate Part 1

Hou, T. H.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991] 1991

Interlaminar fracture characterization a current review

Martin, Roderick H.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991] 1991

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

Modeling of unit-cells with Z-Pins using FLASH pre-processing and post-processing

Krueger, Ronald.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005] 2005

A new look at numerical analyses of free-edge stresses in composite laminates

Raju, I. S., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

Nondimensional parameters and equations for nonlinear and bifurcation analyses of thin anisotropic q

Nemeth, Michael P.
Hampton, Va. National Aeronautics and Space Administration, Langley Research Center, [2010] 2010

Normalization of impact energy by laminate thickness for compression after impact testing

Nettles, A. T. (Alan T.), author.
Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2013. 2013

On processing development for fabrication of fiber reinforced composite, II

Hou, T. H.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

Polymer matrix composite lines and ducts

Nettles, A. T. (Alan T.)
Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001] 2001

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

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 analysis of continuous fiber composite laminates

Thomas, David J.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

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-

Sublaminate analysis of interlaminar fracture in composites

Armanios, Erian A.
Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology ; [Washington, D.C. : NASA Langley Research Center, [1986] 1986

A treatise on equivalent-plate stiffnesses for stiffened laminated-composite plates and plate-like l

Nemeth, Michael P.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011