Search results for: Johnson, W. S.
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1
Impact and residual fatigue behavior of ARALL and AS6/5245 composite materials
Authors: Johnson, W. S.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1986Physical Description: 1 volume.Holdings: Loading…
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2
Damage development in titanium metal matrix composites subjected to cyclic loading
Authors: Johnson, W. S.
Published: National Aeronautics and Space Administration, Langley Research Center, 1992Physical Description: 1 volume.Holdings: Loading…
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3
Experimental and analytical investigation of the fracture processes of boron/aluminum laminates containing notches
Authors: Johnson, W. S.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983Physical Description: 41 pages : illustrations ; 28 cm.Holdings: Loading…
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4
Fatigue behavior of continuous fiber silicon-carbide/aluminum composites
Authors: Johnson, W. S.
Published: National Aeronautics and Space Administration, Langley Research Center, 1984Physical Description: 1 volume : illustrations ; 28 cm.Holdings: Loading…
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5
Evaluation of several micromechanics models for discontinuously reinforced metal matrix composites
Authors: Johnson, W. S.
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1990Physical Description: 1 volume.Holdings: Loading…
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6
Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites
Authors: Johnson, W. S. (W. Steven)
Published: National Aeronautics and Space Administration, Langley Research Center, 1987Physical Description: 1 volume.Holdings: Loading…
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7
Fatigue damage accumulation in various metal matrix composites
Authors: Johnson, W. S. (W. Steven)
Published: National Aeronautics and Space Administration, Langley Research Center, 1987Physical Description: 1 volume.Holdings: Loading…
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8
Influence of the resin on interlaminar mixed-mode fracture
Authors: Johnson, W. S. (W. Steven)
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1985Physical Description: 1 volume.Holdings: Loading…
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9
Stress analysis of the cracked lap shear specimen : an ASTM round robin
Authors: Johnson, W. S. (W. Steven)
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1986Physical Description: 1 volume.Holdings: Loading…
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10
Fatigue of continuous fiber reinforced metallic materials
Authors: Johnson, W. S. (W. Steven)
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1993Physical Description: 1 volume.Holdings: Loading…
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11
Development of testing and analysis methodology to assess the long term durability of polymeric composites at high temperatures
Authors: Johnson, W. S. (W. Steven)
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1990Physical Description: 1 volume.Holdings: Loading…
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12
Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites
Authors: Johnson, W. S. (W. Steven)
Published: National Aeronautics and Space Administration, Langley Research Center, 1990Physical Description: 10 pages : illustrations., Also available via Internet from the NASA Technical Report Server web site. Address as of 1/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900012093%5F1990012093.pdf; current access available via PURL.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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13
Investigation of fiber bridging in double cantilever beam specimens
Authors: Johnson, W. S. (W. Steven)
Published: National Aeronautics and Space Administration, Langley Research Center, 1986Physical Description: 1 volume.Holdings: Loading…
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14
Delamination and debonding of materials : a symposium sponsored by ASTM Committees D-30 on High Modulus Fibers and Their Composites and E-24 on Fracture Testing, Pittsburgh, Pa., 8...
Published: ASTM, 1985Other Authors: “…Johnson, W. S.…”
Physical Description: 503 pages : illustrations ; 24 cm.Holdings: Loading…
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15
Observations of fatigue crack initiation and damage growth in notched titanium matrix composites
Authors: Naik, R. A.Other Authors: “…Johnson, W. S.…”
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1990
Physical Description: 1 volume.Holdings: Loading…
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16
Prediction of matrix fatigue crack initiation in notched SCS-6/Ti-15-3 metal matrix composites
Authors: Hillberry, B. M.Other Authors: “…Johnson, W. S.…”
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1991
Physical Description: 1 volume.Holdings: Loading…
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17
Stress-strain analysis of a [0/90]2s titanium matrix laminate subjected to a generic hypersonic flight profile
Authors: Mirdamadi, M.Other Authors: “…Johnson, W. S.…”
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1992
Physical Description: 1 volume.Holdings: Loading…
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18
Modeling fatigue crack growth in cross ply titanium matrix composites
Authors: Bakuckas, J. G.Other Authors: “…Johnson, W. S.…”
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1993
Physical Description: 1 volume.Holdings: Loading…
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19
Implementation of thermal residual stresses in the analysis of fiber bridged matrix crack growth in titanium matrix composites
Authors: Bakuckas, J. G.Other Authors: “…Johnson, W. S.…”
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
Physical Description: 1 volume.Holdings: Loading…
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20
Prediction of stress-strain response of SCS-6/timetal-21S subjected to a hypersonic flight profile
Authors: Mirdamadi, M.Other Authors: “…Johnson, W. S.…”
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
Physical Description: 1 volume.Holdings: Loading…
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Related Subjects
Metallic composites
Fatigue
Composite materials
Titanium
Metal matrix composites
Metals
Adhesive joints
Fatigue (Materials)
Fracture mechanics
Materials
Silicon carbide
Adhesive bonding
Adhesives
Fatigue life
Fiber composites
Fibrous composites
Laminated materials
Testing
Thermal stresses
Affinity chromatography
Aging (Materials)
Aluminum
Aluminum alloys
Bridges (structures)
CRACK INITIATION
Cantilever beams
Cantilever bridges
Ceramic-matrix composites
Composite structures
Crack bridging