Showing 1 - 9 results of 9 for search 'National Aeronautics and Space Administration,', query time: 0.27s Refine Results
  1. 1
    Fatigue delamination onset prediction in tapered composite laminates /
    by Murri, Gretchen Bostaph
    Published 1989
    “...National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems...”
    Government Document Book
  2. 2
    Local delamination in laminates with angle ply matrix cracks.
    by O'Brien, T. Kevin
    Published 1991
    “...National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems...”
    Government Document Book
  3. 3
    Local delamination in laminates with angle ply matrix cracks.
    by O'Brien, T. Kevin
    Published 1991
    “...National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems...”
    Government Document Book
  4. 4
    Residual thermal and moisture influences on the strain energy release rate analysis of local delaminations from matrix cracks /
    by O'Brien, T. Kevin
    Published 1991
    “...National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems...”
    Government Document Book
  5. 5
    Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads /
    by Hinkley, J. A.
    Published 1992
    “...National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems...”
    Government Document Book
  6. 6
    Results of ASTM round robin testing for mode I interlaminar fracture toughness of composite materials /
    by O'Brien, T. Kevin
    Published 1992
    “...National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems...”
    Government Document Book
  7. 7
    Scale effects on the transverse tensile strength of graphite epoxy composites /
    by O'Brien, T. Kevin
    Published 1992
    “...National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems...”
    Government Document Book
  8. 8
    Analysis of matrix cracking and local delamination in (O/[theta]-[theta])s[subscript] graphite epoxy laminates under tension load /
    by Salpekar, S. A.
    Published 1991
    “...National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems...”
    Government Document Book
  9. 9
    Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load.
    “...National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems...”
    Government Document Microform Book
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