Search results for: Pindera, M.-J. (Marek-Jerzy), 1951-
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1
Effects of fiber and interfacial layer architectures on the thermoplastic response of metal matrix composites
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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2
An analytical/numerical correlation study of the multiple concentric cylinder model for the thermoplastic response of metal matrix composites
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1993Physical Description: 1 volume.Holdings: Loading…
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3
Optimization of residual stresses in MMC's using compensating/compliant interfacial layers. Part II, OPTCOMP user's guide
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994Physical Description: 1 volume.Holdings: Loading…
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4
An evaluation of a coupled microstructural approach for the analysis of functionally graded composites via the finite-element method
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995Physical Description: 1 volume.Holdings: Loading…
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5
Optimization of residual stresses in MMC's through process parameter control and the use of heterogeneous compensating/complaint interfacial layers : OPTCOMP2 user's guide
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1996Physical Description: 1 volume.Holdings: Loading…
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6
An efficient implementation of the GMC micromechanics model for multi-phased materials with complex microstructures
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997Physical Description: 1 volume.Holdings: Loading…
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7
HOTCFGM-1D : a coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1998Physical Description: 1 volume.Holdings: Loading…
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8
Optimization of residual stresses in MMC's through the variation of interfacial layer architectures and processing parameters
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1996Physical Description: 1 volume.Holdings: Loading…
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9
The effect of interface roughness and oxide film thickness on the inelastic response of thermal barrier coatings to thermal cycling
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-
Published: National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information ; National Technical Information Service [distributor], 1999Physical Description: 1 volume.Holdings: Loading…
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10
The effect of interface roughness and oxide film thickness on the inelastic response of thermal barrier coatings to thermal cycling
Authors: Pindera, M.-J. (Marek-Jerzy), 1951-, Aboudi, Jacob, 1935-, Arnold, S. M.
Published: National Aeronautics and Space Administration, Glenn Research Center, 1999Physical Description: 1 online resource (16 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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11
Isodyne stress analysis
Authors: Pindera, Jerzy-TadueszOther Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: Kluwer Academic Publishers, 1989
Physical Description: xxi, 263 pages : illustrations ; 25 cm.Holdings: Loading…
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12
Micromechanics of metal matrix composites using the generalized method of cells model (GMC) user's guide
Authors: Aboudi, Jacob, 1935-Other Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1992
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13
Multiple concentric cylinder model (MCCM) user's guide
Authors: Williams, Todd O.Other Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
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14
Micromechanical modeling of the thermal expansion of graphite/copper composites with nonuniform microstructure
Authors: Bednarcyk, Brett A.Other Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
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15
Radiation and temperature effects on the time-dependent response of T300-934 graphite-epoxy
Authors: Yancey, Robert N.Other Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: Virginia Polytechnic Institute and State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1988
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16
Micromechanical modeling of woven metal matrix composites : [final contractor report]
Authors: Bednarcyk, Brett A.Other Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
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17
Impact of functionally graded cylinders : theory
Authors: Aboudi, Jacob, 1935-Other Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001
Physical Description: 1 volume., Also available via Internet from the NASA web site. Address as of 4/23/03: http://gltrs.grc.nasa.gov/reports/2001/CR-2001-210967.pdf; current access is available via PURL.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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18
Efficient reformulation of HOTFGM : heat conduction with variable thermal conductivity
Authors: Zhong, YiOther Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2002
Physical Description: 1 volume., Also available via Internet from the NASA web site. Address as of 9/17/03: http://gltrs.grc.nasa.gov/reports/2002/CR-2002-211910.pdf; current access available via PURL.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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19
Mechanical response of unidirectional boron/aluminum under combined loading
Authors: Becker, WolfgangOther Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: College of Engineering, Virginia Polytech;nic Institute and State University ; [For sale by the National Technical Information Service], 1987
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20
Thermoelastic response of metal matrix composites with large-diameter fibers subjected to thermal gradients
Authors: Aboudi, Jacob, 1935-Other Authors: “…Pindera, M.-J. (Marek-Jerzy), 1951-…”
Published: [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1993
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Related Subjects
Micromechanics
Metal matrix composites
Metallic composites
Microstructure
Stress distribution
Computer programs
FIBER COMPOSITES
Mathematical models
Residual stress
Thermal stresses
Copper
Cylindrical bodies
Elastoplasticity
Film thickness
Functionally gradient materials
Interfaces
Oxide films
Surface roughness
Temperature effects
Thermal conductivity
Thickness
Titanium
User manuals (Computer programs)
Woven composites
Algorithms
Applications programs (Computers)
Asymptotic properties
Axial strain
Backward facing steps
Bonding