Search results for: Bigelow, C. A.
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1
Nonlinear adhesive behavior effects in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1985Physical Description: 1 volume : illustrations ; 28 cm.Holdings: Loading…
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2
Fatigue of graphite/epoxy buffer strip panels with center cracks
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1985Physical Description: 1 volume : illustrations ; 28 cm.Holdings: Loading…
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3
A cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1985Physical Description: 1 volume.Holdings: Loading…
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4
Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1991Physical Description: 1 volume.Holdings: Loading…
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5
A. Micromechanics-based strength prediction methodology for notched metal matrix composites
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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6
The effects of uneven fiber spacing on thermal residual stresses in a unidirectional SCS-6Ti-15-3 laminate
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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7
Thermal residual stresses in silicon-carbide/titanium [0/90] laminate
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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8
A macro-mechanics analysis of a notched metal matrix composite
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1990Physical Description: 1 volume.Holdings: Loading…
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9
Time-dependent deformation of titanium metal matrix composites
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995Physical Description: 1 volume.Holdings: Loading…
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10
Analysis of notched metal matrix composites under tension loading
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center, 1988Physical Description: 1 volume.Holdings: Loading…
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11
Effects of moisture, elevated temperature, and fatigue loading on the behavior of graphite/epoxy buffer strip panels with center cracks
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1988Physical Description: 1 volume.Holdings: Loading…
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12
Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet
Authors: Bigelow, C. A.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986Physical Description: 1 volume.Holdings: Loading…
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13
Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites
Authors: Johnson, W. S. (W. Steven)Other Authors: “…Bigelow, C. A.…”
Published: National Aeronautics and Space Administration, Langley Research Center, 1987
Physical Description: 1 volume.Holdings: Loading…
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14
An improved boundary force method for analyzing cracked anisotropic materials
Authors: Tan, P. W.Other Authors: “…Bigelow, C. A.…”
Published: National Aeronautics and Space Administration, Langley Research Center, 1988
Physical Description: 1 volume.Holdings: Loading…
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15
Finite-element analyses and fracture simulation in thin-sheet aluminum alloy
Authors: Newman, J. C.Other Authors:
Published: National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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16
Three-dimensional elastic-plastic finite-element analyses of constraint variations in cracked bodies
Authors: Newman, J. C.Other Authors: “…Bigelow, C. A.…”
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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17
Three-dimensional CTOA and constraint effects during stable tearing in a thin-sheet material
Authors: Dawicke, D. S.Other Authors:
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995Physical Description: 1 volume.Holdings: Loading…
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18
Fatigue damage in cross-ply titanium metal matrix composites containing center holes
Authors: Bakuckas, J. G.Other Authors:
Published: National Aeronautics and Space Administration, Langley Research Center, 1992Physical Description: 1 volume.Holdings: Loading…
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19
Experimental and analytical investigation of the fracture processes of boron/aluminum laminates containing notches
Authors: Johnson, W. S.Other Authors: “…Bigelow, C. A.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
Physical Description: 41 pages : illustrations ; 28 cm.Holdings: Loading…
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Related Subjects
Composite materials
Fatigue
Finite element method
Fracture mechanics
Laminated materials
Metallic composites
Aluminum alloys
Materials
Metal matrix composites
Micromechanics
Titanium
Adhesive bonding
Adhesives
Airframes
Aluminum boron composites
Anisotropy
Bonding
COMPUTER PROGRAMS
Crack propogation
Crack tips
Cracks
Elastic deformation
Epoxy resins
FRACTURE MECHANICS
Fiber-matrix interfaces
Fibrous composites
Fracture
Graphite fibers
Integral equations
MATHEMATICAL MODELS