Explore: Compression Loads
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Source: The Open Library
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1Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels
By Dawn C. Jegley
“Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels” Metadata:
- Title: ➤ Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels
- Author: Dawn C. Jegley
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - For sale by the National Technical Information Service] - Langley Research Center
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - Hampton, Va - [Washington, DC]
“Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels” Subjects and Themes:
- Subjects: Composite materials - Sandwich structures - Compression loads
Edition Identifiers:
- The Open Library ID: OL14685348M - OL18055695M - OL19246673M - OL15366951M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Short-wavelength buckling and shear failures for compression-loaded composite laminates
By Mark J. Shuart
“Short-wavelength buckling and shear failures for compression-loaded composite laminates” Metadata:
- Title: ➤ Short-wavelength buckling and shear failures for compression-loaded composite laminates
- Author: Mark J. Shuart
- Language: English
- Number of Pages: Median: 210
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1985
- Publish Location: Hampton, Va
“Short-wavelength buckling and shear failures for compression-loaded composite laminates” Subjects and Themes:
- Subjects: ➤ Buckling (Mechanics) - Shear (Mechanics) - Composite materials - Buckling - Compression loads - Fiber composites - Matrix materials - Laminates - Shear stress
Edition Identifiers:
- The Open Library ID: OL16152659M - OL17634945M - OL18290563M
- Online Computer Library Center (OCLC) ID: 18577777
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3The utilization of advanced composites in military aircraft
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“The utilization of advanced composites in military aircraft” Metadata:
- Title: ➤ The utilization of advanced composites in military aircraft
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Publisher: AGARD - Agard
- Publish Date: 1992
- Publish Location: ➤ Neuilly sur Seine - Neuilly sur Seine, France
“The utilization of advanced composites in military aircraft” Subjects and Themes:
- Subjects: Composite materials - Compression loads - Military aircraft
Edition Identifiers:
- The Open Library ID: OL19244747M - OL14329511M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Analytical comparison of three stiffened panel concepts
By Jill M. Maloney
“Analytical comparison of three stiffened panel concepts” Metadata:
- Title: ➤ Analytical comparison of three stiffened panel concepts
- Author: Jill M. Maloney
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Analytical comparison of three stiffened panel concepts” Subjects and Themes:
- Subjects: ➤ Compression loads - Design analysis - Fuel tanks - Panels - Reinforced plates - Reusable launch vehicles - Structural members
Edition Identifiers:
- The Open Library ID: OL15424041M - OL17796408M
- Online Computer Library Center (OCLC) ID: 35282956
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Test load verification through strain data analysis
By V. Verderaime
“Test load verification through strain data analysis” Metadata:
- Title: ➤ Test load verification through strain data analysis
- Author: V. Verderaime
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Aeronautics and Space Administration, Marshall Space Flight Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - MSFC, Ala - Washington, DC
“Test load verification through strain data analysis” Subjects and Themes:
- Subjects: ➤ Elastic bending - Fracturing - Safety factors - Compression loads - Inelastic stress - Proving - Static tests - Polycrystals - Criteria
Edition Identifiers:
- The Open Library ID: OL21864612M - OL15413589M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Reliability-based failure analysis of brittle materials
By Lynn M. Powers
“Reliability-based failure analysis of brittle materials” Metadata:
- Title: ➤ Reliability-based failure analysis of brittle materials
- Author: Lynn M. Powers
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Reliability-based failure analysis of brittle materials” Subjects and Themes:
- Subjects: Compressive strength - Cracking (Fracturing) - Compression loads - Stress analysis - Brittle materials
Edition Identifiers:
- The Open Library ID: OL18078536M - OL15408277M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy
By Alan T. Nettles
“The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy” Metadata:
- Title: ➤ The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy
- Author: Alan T. Nettles
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992 - 1994
- Publish Location: ➤ [Washington, DC] - Springfield, Va - [Washington, D.C - [Springfield, Va
“The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy” Subjects and Themes:
- Subjects: ➤ Strain distribution - Prestressing - Compression loads - Strains and stresses - Impact tests - Composite materials - Epoxy matrix composites - Compressive strength - Impact strength
Edition Identifiers:
- The Open Library ID: OL15498386M - OL17676897M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy
By A. T. Nettles
“The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy” Metadata:
- Title: ➤ The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy
- Author: A. T. Nettles
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992 - 1994
- Publish Location: ➤ [Washington, D.C - [Springfield, Va - [Washington, DC] - Springfield, Va
“The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy” Subjects and Themes:
- Subjects: ➤ Strain distribution - Prestressing - Compression loads - Strains and stresses - Impact tests - Composite materials - Epoxy matrix composites - Compressive strength - Impact strength
Edition Identifiers:
- The Open Library ID: OL14686529M - OL17834464M
- Online Computer Library Center (OCLC) ID: 39618369
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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9Prestraining and its influence on subsequent fatigue life
By Sreeramesh Kalluri
“Prestraining and its influence on subsequent fatigue life” Metadata:
- Title: ➤ Prestraining and its influence on subsequent fatigue life
- Author: Sreeramesh Kalluri
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Prestraining and its influence on subsequent fatigue life” Subjects and Themes:
- Subjects: ➤ Inconel (Trademark) - Fatigue tests - Compression loads - Aircraft construction materials - Cumulative damage - Tensile stress - Prestressing - Heat resistant alloys - Fatigue life
Edition Identifiers:
- The Open Library ID: OL15420702M - OL17794538M
- Online Computer Library Center (OCLC) ID: 34612929
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Compression response of laminated composites containing an open hole
By Fu-Kuo Chang
“Compression response of laminated composites containing an open hole” Metadata:
- Title: ➤ Compression response of laminated composites containing an open hole
- Author: Fu-Kuo Chang
- Publisher: ➤ Society for the Advancement of Material & Process Engineering
- Publish Date: 1988
- Publish Location: Covina, Calif
“Compression response of laminated composites containing an open hole” Subjects and Themes:
- Subjects: Composite materials - Compression loads - Laminates
Edition Identifiers:
- The Open Library ID: OL18928205M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Fatigue response of notched laminates subjected to tension-compression cyclic loads
By Charles E. Bakis
“Fatigue response of notched laminates subjected to tension-compression cyclic loads” Metadata:
- Title: ➤ Fatigue response of notched laminates subjected to tension-compression cyclic loads
- Author: Charles E. Bakis
- Language: English
- Publisher: ➤ Virginia Polytechnic Institute and State University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC - Blacksburg, Va - Springfield, Va
“Fatigue response of notched laminates subjected to tension-compression cyclic loads” Subjects and Themes:
- Subjects: ➤ Compression loads - Crack initiation - Fatigue (Materials) - Graphite-epoxy composites - Life (Durability) - Tensile properties
Edition Identifiers:
- The Open Library ID: OL15415616M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware
By A. T. Nettles
“Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware” Metadata:
- Title: ➤ Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware
- Author: A. T. Nettles
- Language: English
- Number of Pages: Median: 27
- Publisher: ➤ National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 2010
- Publish Location: Huntsville], Ala
“Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware” Subjects and Themes:
- Subjects: ➤ Tolerances (mechanics) - Fatigue (materials) - Composite materials - Compression loads - Degradation - Damage - Failure
Edition Identifiers:
- The Open Library ID: OL43925054M
- Online Computer Library Center (OCLC) ID: 706732471
Access and General Info:
- First Year Published: 2010
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Normalization of impact energy by laminate thickness for compression after impact testing
By A. T. Nettles
“Normalization of impact energy by laminate thickness for compression after impact testing” Metadata:
- Title: ➤ Normalization of impact energy by laminate thickness for compression after impact testing
- Author: A. T. Nettles
- Language: English
- Number of Pages: Median: 37
- Publisher: ➤ National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 2013
- Publish Location: Huntsville, Alabama
“Normalization of impact energy by laminate thickness for compression after impact testing” Subjects and Themes:
- Subjects: ➤ Laminates - Thickness - Impact strength - Compression loads - Mechanical properties - Impact tolerances
Edition Identifiers:
- The Open Library ID: OL54280011M
- Online Computer Library Center (OCLC) ID: 851803234
Access and General Info:
- First Year Published: 2013
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy
By D. S. Dawicke
“Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy” Metadata:
- Title: ➤ Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy
- Author: D. S. Dawicke
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy” Subjects and Themes:
- Subjects: Crack propagation - Fatigue (Materials) - Compression loads - Aluminum alloys
Edition Identifiers:
- The Open Library ID: OL17837096M
- Online Computer Library Center (OCLC) ID: 39776177
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Micromechanics of compression failures in open hole composite laminates
By Eunice Gail Guynn
“Micromechanics of compression failures in open hole composite laminates” Metadata:
- Title: ➤ Micromechanics of compression failures in open hole composite laminates
- Author: Eunice Gail Guynn
- Language: English
- Number of Pages: Median: 206
- Publisher: ➤ Mechanics and Materials Center, Texas A&M University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - [Washington, D.C - College Station, Tex
“Micromechanics of compression failures in open hole composite laminates” Subjects and Themes:
- Subjects: ➤ Composite materials - Crack propagation - Fracture - Tensile properties - Mathematical models - Testing - Compression loads - Compression testing - Materials - Holes (Mechanics) - Hole geometry (Mechanics) - Failure analysis - Composite structures
Edition Identifiers:
- The Open Library ID: OL17684168M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Measurement of displacement around holes in composite plates subjected to quasi-static compression
By John C. Duke
“Measurement of displacement around holes in composite plates subjected to quasi-static compression” Metadata:
- Title: ➤ Measurement of displacement around holes in composite plates subjected to quasi-static compression
- Author: John C. Duke
- Number of Pages: Median: 60
- Publisher: Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Measurement of displacement around holes in composite plates subjected to quasi-static compression” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19987727M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17A damage tolerance study conducted with structure relevant specimens
By S. Labonte
“A damage tolerance study conducted with structure relevant specimens” Metadata:
- Title: ➤ A damage tolerance study conducted with structure relevant specimens
- Author: S. Labonte
- Number of Pages: Median: 38
- Publisher: National Aerospace Laboratory
- Publish Date: 1993
- Publish Location: Amsterdam
“A damage tolerance study conducted with structure relevant specimens” Subjects and Themes:
- Subjects: Compression loads - Impact damage - Delaminating
Edition Identifiers:
- The Open Library ID: OL19751220M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Investigation of anomalous behavior in metallic-based materials under compressive loading
By Christopher M. Gil
“Investigation of anomalous behavior in metallic-based materials under compressive loading” Metadata:
- Title: ➤ Investigation of anomalous behavior in metallic-based materials under compressive loading
- Author: Christopher M. Gil
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Investigation of anomalous behavior in metallic-based materials under compressive loading” Subjects and Themes:
- Subjects: Silicon compounds - Compression loads - Anomalies - Silicon carbides
Edition Identifiers:
- The Open Library ID: OL15542069M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Buckling and postbuckling behavior of square compression-loaded graphite-epoxy plates with circular cutouts
By Michael P. Nemeth
“Buckling and postbuckling behavior of square compression-loaded graphite-epoxy plates with circular cutouts” Metadata:
- Title: ➤ Buckling and postbuckling behavior of square compression-loaded graphite-epoxy plates with circular cutouts
- Author: Michael P. Nemeth
- Language: English
- Number of Pages: Median: 30
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Buckling and postbuckling behavior of square compression-loaded graphite-epoxy plates with circular cutouts” Subjects and Themes:
- Subjects: ➤ Bending - Metal plates - Buckling - Buckling (Mechanics) - Testing - Compression loads - Compression testing - Graphite-epoxy compounds - Materials - Composite materials - Openings - Orthotropic plates
Edition Identifiers:
- The Open Library ID: OL16132222M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Identification of nonlinear micron-level mechanics for a precision deployable joint
By S. J. Bullock
“Identification of nonlinear micron-level mechanics for a precision deployable joint” Metadata:
- Title: ➤ Identification of nonlinear micron-level mechanics for a precision deployable joint
- Author: S. J. Bullock
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Identification of nonlinear micron-level mechanics for a precision deployable joint” Subjects and Themes:
- Subjects: ➤ Tension - Digital data - Nonlinearity - Dynamical systems - Joints (Junctions) - Compression loads - Load distribution (Forces) - Prestressing
Edition Identifiers:
- The Open Library ID: OL15507951M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Analysis and test of superplastically formed titanium hat-stiffened panels under compression
By Randall C. Davis
“Analysis and test of superplastically formed titanium hat-stiffened panels under compression” Metadata:
- Title: ➤ Analysis and test of superplastically formed titanium hat-stiffened panels under compression
- Author: Randall C. Davis
- Publisher: Sine nomine
- Publish Date: 1986
- Publish Location: [S.l.]
“Analysis and test of superplastically formed titanium hat-stiffened panels under compression” Subjects and Themes:
- Subjects: Titanium - Stiffening - Compression loads - Superplasticity
Edition Identifiers:
- The Open Library ID: OL19987961M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box
By Dawn C. Jegley
“Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box” Metadata:
- Title: ➤ Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box
- Author: Dawn C. Jegley
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box” Subjects and Themes:
- Subjects: ➤ Graphite-epoxy composites - Composite materials - Finite element method - Structural analysis - Compression loads - Wings - Composite structures
Edition Identifiers:
- The Open Library ID: OL15424044M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Torsional buckling tests of a simulated solar array
By E. A. Thornton
“Torsional buckling tests of a simulated solar array” Metadata:
- Title: ➤ Torsional buckling tests of a simulated solar array
- Author: E. A. Thornton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - School of Engineering & Applied Science, University of Virginia
- Publish Date: 1996
- Publish Location: ➤ Charlottesville, VA - [Washington, DC - Springfield, Va
“Torsional buckling tests of a simulated solar array” Subjects and Themes:
- Subjects: ➤ Buckling - Torsion - Booms (Equipment) - Twisting - Compression loads - Loading rate - Solar arrays
Edition Identifiers:
- The Open Library ID: OL15506280M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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24Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading
By David M. McGowan
“Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading” Metadata:
- Title: ➤ Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading
- Author: David M. McGowan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading” Subjects and Themes:
- Subjects: ➤ Sandwich structures - Impact damage - Compression loads - Impact tests - Residual strength - Structural analysis - Panels - Failure analysis - Composite structures
Edition Identifiers:
- The Open Library ID: OL15509435M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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25A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep
By Thomas S. Gates
“A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep” Metadata:
- Title: ➤ A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep
- Author: Thomas S. Gates
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, Va
“A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep” Subjects and Themes:
- Subjects: ➤ Tension - Compression loads - Aging (Materials) - Fiber composites - Creep tests - Polymer matrix composites - Compression tests - Tensile tests - Shear creep
Edition Identifiers:
- The Open Library ID: OL15498115M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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26Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy
By David S. Dawicke
“Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy” Metadata:
- Title: ➤ Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy
- Author: David S. Dawicke
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy” Subjects and Themes:
- Subjects: Crack propagation - Fatigue (Materials) - Compression loads - Aluminum alloys
Edition Identifiers:
- The Open Library ID: OL15498724M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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27Spectrum fatigue model for composite laminates
By Gerald E. Mabson
“Spectrum fatigue model for composite laminates” Metadata:
- Title: ➤ Spectrum fatigue model for composite laminates
- Author: Gerald E. Mabson
- Publisher: Sine nomine
- Publish Date: 1986
- Publish Location: [S.l.]
“Spectrum fatigue model for composite laminates” Subjects and Themes:
- Subjects: Fatigue - Compression loads - Composite materials - Laminates
Edition Identifiers:
- The Open Library ID: OL20984915M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Behavior of damaged graphite/epoxy laminates under compression loading
By Bruce A. Byers
“Behavior of damaged graphite/epoxy laminates under compression loading” Metadata:
- Title: ➤ Behavior of damaged graphite/epoxy laminates under compression loading
- Author: Bruce A. Byers
- Number of Pages: Median: 63
- Publisher: ➤ Boeing Commercial Airplane Company
- Publish Date: 1980
- Publish Location: Seattle, Wash
“Behavior of damaged graphite/epoxy laminates under compression loading” Subjects and Themes:
- Subjects: Graphite-epoxy composites - Compression loads - Laminates
Edition Identifiers:
- The Open Library ID: OL19252529M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Theoretical-experimental correlation for buckling of composite cylinders under combined compression and torsion
By Carl T. Herakovich
“Theoretical-experimental correlation for buckling of composite cylinders under combined compression and torsion” Metadata:
- Title: ➤ Theoretical-experimental correlation for buckling of composite cylinders under combined compression and torsion
- Author: Carl T. Herakovich
- Number of Pages: Median: 111
- Publisher: ➤ Virginia Polytechnic Institute and State University, College of Engineering
- Publish Date: 1978
- Publish Location: Blacksburg, Va
“Theoretical-experimental correlation for buckling of composite cylinders under combined compression and torsion” Subjects and Themes:
- Subjects: Buckling - Composite materials - Compression loads - Torsion
Edition Identifiers:
- The Open Library ID: OL21334832M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Compressive fatigue behaviour of bovine compact bone
By Robert J. Gray
“Compressive fatigue behaviour of bovine compact bone” Metadata:
- Title: ➤ Compressive fatigue behaviour of bovine compact bone
- Author: Robert J. Gray
- Publisher: ➤ Institute for Aerospace Studies
- Publish Date: 1972
- Publish Location: [Downsview, Ont.]
“Compressive fatigue behaviour of bovine compact bone” Subjects and Themes:
- Subjects: Bones - Compression loads - Fatigue
Edition Identifiers:
- The Open Library ID: OL18998029M
Access and General Info:
- First Year Published: 1972
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Structural load
principal ones can be classified as live loads (loads which are not always present in the structure), dead loads (loads which are permanent and immovable excepting
Variable compression ratio
while under varying loads. Variable compression engines allow the volume above the piston at top dead centre to be changed. Higher loads require lower ratios
Space frame
inherent rigidity of the triangle; flexing loads (bending moments) are transmitted as tension and compression loads along the length of each strut. Chief applications
Truss bridge
typically straight, may be stressed from tension, compression, or sometimes both in response to dynamic loads. There are several types of truss bridges, including
Disk compression
then loads the DOS kernel (MSDOS.SYS, IBMDOS.COM etc.) If the DOS supports the preload API, the DOS BIOS attempts to load a preloadable compression driver
Load cell
and hopper applications. S-type load cells; used in tension applications with static and dynamic loads. Compression load cells; used in truck scales, large
Compression ratio
The compression ratio is the ratio between the maximum and minimum volume during the compression stage of the power cycle in a piston or Wankel engine
Spring (device)
load is applied to it. Compression spring Designed to operate with a compression load, so the spring gets shorter as the load is applied to it. Torsion
Container compression test
to protect the contents from compression damage etc. The dynamic loads have some relationship with expected field loads.: often factors of 4 or 5 are
Euler's critical load
straight for loads less than the critical load. The critical load is the greatest load that will not cause lateral deflection (buckling). For loads greater