Explore: Residual Strength
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AI-Generated Overview About “residual-strength”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Impact damage resistance and residual property assessment of [0/+/-45/90]s SCS-6/Timetal 21S
By Jennifer L. Miller
“Impact damage resistance and residual property assessment of [0/+/-45/90]s SCS-6/Timetal 21S” Metadata:
- Title: ➤ Impact damage resistance and residual property assessment of [0/+/-45/90]s SCS-6/Timetal 21S
- Author: Jennifer L. Miller
- 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
“Impact damage resistance and residual property assessment of [0/+/-45/90]s SCS-6/Timetal 21S” Subjects and Themes:
- Subjects: ➤ Fiber orientation - Impact damage - Impact resistance - Impact tests - Metal matrix composites - Residual strength - X ray inspection
Edition Identifiers:
- The Open Library ID: OL17791964M - OL15414541M
- Online Computer Library Center (OCLC) ID: 34051841
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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2Estimating the R-Curve from residual strength data
By Thomas W. Orange
“Estimating the R-Curve from residual strength data” Metadata:
- Title: ➤ Estimating the R-Curve from residual strength data
- Author: Thomas W. Orange
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1985
- Publish Location: [Cleveland, Ohio
“Estimating the R-Curve from residual strength data” Subjects and Themes:
- Subjects: ➤ Crack propagation - Estimating - Fracture mechanics - R-curves - Residual strength - Resistance
Edition Identifiers:
- The Open Library ID: OL18289894M - OL16151527M
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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3Damage tolerance in filament-wound graphite/epoxy pressure vessels
By William E. Simon
“Damage tolerance in filament-wound graphite/epoxy pressure vessels” Metadata:
- Title: ➤ Damage tolerance in filament-wound graphite/epoxy pressure vessels
- Author: William E. Simon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Lamar University, College of Engineering - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Beaumont, Tex - [Washington, DC
“Damage tolerance in filament-wound graphite/epoxy pressure vessels” Subjects and Themes:
- Subjects: ➤ Damage assessment - Failure analysis - Filament winding - Graphite-epoxy composites . - Impact damage - Impact tolerances - Pressure vessels - Residual strength
Edition Identifiers:
- The Open Library ID: OL15414644M - OL17792069M
- Online Computer Library Center (OCLC) ID: 34112587
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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4The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles
By A. T. Nettles
“The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles” Metadata:
- Title: ➤ The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles
- Author: A. T. Nettles
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 2011
- Publish Location: Huntsville], Ala
“The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles” Subjects and Themes:
- Subjects: ➤ Damage assessment - Launch vehicles - Thermal protection - Sandwich structures - Residual strength - Ares 1 launch vehicle - Composite structures - Composite materials - Impact damage
Edition Identifiers:
- The Open Library ID: OL43927159M
- Online Computer Library Center (OCLC) ID: 744420941
Access and General Info:
- First Year Published: 2011
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Carbon fibre composite coupons - static and fatigue behaviour after impact damage
By G. Clark
“Carbon fibre composite coupons - static and fatigue behaviour after impact damage” Metadata:
- Title: ➤ Carbon fibre composite coupons - static and fatigue behaviour after impact damage
- Author: G. Clark
- Number of Pages: Median: 13
- Publisher: ➤ Aeronautical Research Laboratories
- Publish Date: 1986
- Publish Location: Melbourne, Australia
“Carbon fibre composite coupons - static and fatigue behaviour after impact damage” Subjects and Themes:
- Subjects: Graphite-epoxy composites - Fatigue - Impact damage - Delaminating - Residual strength
Edition Identifiers:
- The Open Library ID: OL18998262M
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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6Evaluation of 6013-T6 sheet for damage tolerance applications
By W. G. J. 't Hart
“Evaluation of 6013-T6 sheet for damage tolerance applications” Metadata:
- Title: ➤ Evaluation of 6013-T6 sheet for damage tolerance applications
- Author: W. G. J. 't Hart
- Number of Pages: Median: 53
- Publisher: National Aerospace Laboratory
- Publish Date: 1992
- Publish Location: Amsterdam
“Evaluation of 6013-T6 sheet for damage tolerance applications” Subjects and Themes:
- Subjects: Aluminum alloys - Corrosion resistance - Fatigue tests - Residual strength
Edition Identifiers:
- The Open Library ID: OL19750844M
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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7Residual strength of damage tolerant aluminium-lithium sheet materials (NLR contribution to BREU 3250, Task 3)
By W. G. J. 't Hart
“Residual strength of damage tolerant aluminium-lithium sheet materials (NLR contribution to BREU 3250, Task 3)” Metadata:
- Title: ➤ Residual strength of damage tolerant aluminium-lithium sheet materials (NLR contribution to BREU 3250, Task 3)
- Author: W. G. J. 't Hart
- Number of Pages: Median: 65
- Publisher: National Aerospace Laboratory
- Publish Date: 1992
- Publish Location: Amsterdam
“Residual strength of damage tolerant aluminium-lithium sheet materials (NLR contribution to BREU 3250, Task 3)” Subjects and Themes:
- Subjects: Aluminum alloys - Residual strength
Edition Identifiers:
- The Open Library ID: OL19750849M
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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8Residual strength analyses of riveted lap-splice joints
By B. R. Seshadri
“Residual strength analyses of riveted lap-splice joints” Metadata:
- Title: ➤ Residual strength analyses of riveted lap-splice joints
- Author: B. R. Seshadri
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2000
- Publish Location: Hampton, Va - [Springfield, Va
“Residual strength analyses of riveted lap-splice joints” Subjects and Themes:
- Subjects: ➤ Lap joints - Riveted joints - Cracks - Fracturing - Crack propagation - Holes (Mechanics) - Computer programs - Residual strength - Structural analysis - Rivets
Edition Identifiers:
- The Open Library ID: OL15574417M
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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9A progressive damage methodology for residual strength predictions of notched composite panels
By Timothy W. Coats
“A progressive damage methodology for residual strength predictions of notched composite panels” Metadata:
- Title: ➤ A progressive damage methodology for residual strength predictions of notched composite panels
- Author: Timothy W. Coats
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - Springfield, VA
“A progressive damage methodology for residual strength predictions of notched composite panels” Subjects and Themes:
- Subjects: ➤ Crack propagation - Loads (Forces) - Fracture strength - Fracture mechanics - Epoxy matrix composites - Laminates - Residual strength - Composite structures - Fractography
Edition Identifiers:
- The Open Library ID: OL15541851M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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10A progressive damage methodology for residual strength predictions of center-crack tension composite panels
By Timothy William Coats
“A progressive damage methodology for residual strength predictions of center-crack tension composite panels” Metadata:
- Title: ➤ A progressive damage methodology for residual strength predictions of center-crack tension composite panels
- Author: Timothy William Coats
- 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 progressive damage methodology for residual strength predictions of center-crack tension composite panels” Subjects and Themes:
- Subjects: ➤ Crack propagation - Fiber orientation - Loads (Forces) - Fracture strength - Crack bridging - Notch tests - Residual strength - Fiber strength - Composite structures - Fractography
Edition Identifiers:
- The Open Library ID: OL15505069M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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11Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate
By C. C. Poe
“Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate” Metadata:
- Title: ➤ Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate
- Author: C. C. Poe
- Language: English
- Number of Pages: Median: 48
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate” Subjects and Themes:
- Subjects: ➤ Propulsion systems - Space shuttles - Impact damage - Tensile strength - Graphite-epoxy composites - Materials - Laminates - Impact testing - Residual strength - Damage assessment
Edition Identifiers:
- The Open Library ID: OL16135134M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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12Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case
By C. C. Poe
“Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case” Metadata:
- Title: ➤ Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case
- Author: C. C. Poe
- Language: English
- Number of Pages: Median: 34
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case” Subjects and Themes:
- Subjects: ➤ Propulsion systems - Critical pressure - Space shuttles - Impact damage - Graphite-epoxy composites - Materials - Impact testing - Residual strength - Low speed - Rocket engine cases
Edition Identifiers:
- The Open Library ID: OL16122059M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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13Effect of partial interlaminar bonding on impact resistance and loaded-hole behavior of graphite/epoxy quasi-isotropic laminates
By Walter Illg
“Effect of partial interlaminar bonding on impact resistance and loaded-hole behavior of graphite/epoxy quasi-isotropic laminates” Metadata:
- Title: ➤ Effect of partial interlaminar bonding on impact resistance and loaded-hole behavior of graphite/epoxy quasi-isotropic laminates
- Author: Walter Illg
- Number of Pages: Median: 43
- Publisher: Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Effect of partial interlaminar bonding on impact resistance and loaded-hole behavior of graphite/epoxy quasi-isotropic laminates” Subjects and Themes:
- Subjects: Graphite-epoxy composites - Impact damage - Residual strength
Edition Identifiers:
- The Open Library ID: OL19988043M
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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14Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures
By Charles E. Harris
“Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures” Metadata:
- Title: ➤ Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures
- Author: Charles E. Harris
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures” Subjects and Themes:
- Subjects: ➤ Cracks - Residual strength - Structural analysis - Aircraft structures - Fracture mechanics - Applications programs (Computers) - Fatigue (Materials)
Edition Identifiers:
- The Open Library ID: OL15421517M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15Determination of residual stress in composite materials using ultrasonic waves
By S. I. Rokhlin
“Determination of residual stress in composite materials using ultrasonic waves” Metadata:
- Title: ➤ Determination of residual stress in composite materials using ultrasonic waves
- Author: S. I. Rokhlin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Determination of residual stress in composite materials using ultrasonic waves” Subjects and Themes:
- Subjects: ➤ Residual stress - Plane stress - Stress analysis - Thermal expansion - Ultrasonic radiation - Composite materials - Residual strength - Fiber-matrix interfaces - Anisotropy - Metal matrix composites
Edition Identifiers:
- The Open Library ID: OL15491675M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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16Isothermal fatigue, damage accumulation, and life prediction of a woven PMC
By Andrew L. Gyekenyesi
“Isothermal fatigue, damage accumulation, and life prediction of a woven PMC” Metadata:
- Title: ➤ Isothermal fatigue, damage accumulation, and life prediction of a woven PMC
- Author: Andrew L. Gyekenyesi
- 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]
“Isothermal fatigue, damage accumulation, and life prediction of a woven PMC” Subjects and Themes:
- Subjects: Residual strength - Polymer matrix composites - Compression tests - Compressive strength - Fatigue (Materials)
Edition Identifiers:
- The Open Library ID: OL15547921M
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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17Damage 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
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18Boeing/NASA composite components flight service evaluation
By Randy L. Coggeshall
“Boeing/NASA composite components flight service evaluation” Metadata:
- Title: ➤ Boeing/NASA composite components flight service evaluation
- Author: Randy L. Coggeshall
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“Boeing/NASA composite components flight service evaluation” Subjects and Themes:
- Subjects: ➤ Structural reliability - Elevators (Control surfaces) - Aircraft construction materials - Composite structures - Graphite-epoxy composites - Service life - Spoilers - Residual strength - Flight tests
Edition Identifiers:
- The Open Library ID: OL16135391M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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19Finite element analyses of stable crack growth in thin sheet material
By A. V. de Koning
“Finite element analyses of stable crack growth in thin sheet material” Metadata:
- Title: ➤ Finite element analyses of stable crack growth in thin sheet material
- Author: A. V. de Koning
- Number of Pages: Median: 30
- Publisher: National Aerospace Laboratory
- Publish Date: 1985
- Publish Location: Amsterdam
“Finite element analyses of stable crack growth in thin sheet material” Subjects and Themes:
- Subjects: ➤ Crack propagation - J integral - Crack initiation - Fracture mechanics - Aluminum alloys - Finite element method - Prediction analysis techniques - Residual strength
Edition Identifiers:
- The Open Library ID: OL20984657M
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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20Fatigue and residual strength behaviour of ARALL3 panels with bonded on doublers
By W. van der Hoeven
“Fatigue and residual strength behaviour of ARALL3 panels with bonded on doublers” Metadata:
- Title: ➤ Fatigue and residual strength behaviour of ARALL3 panels with bonded on doublers
- Author: W. van der Hoeven
- Number of Pages: Median: 77
- Publisher: National Aerospace Laboratory
- Publish Date: 1992
- Publish Location: Amsterdam
“Fatigue and residual strength behaviour of ARALL3 panels with bonded on doublers” Subjects and Themes:
- Subjects: Aluminum alloys - Laminates - Residual strength
Edition Identifiers:
- The Open Library ID: OL19750861M
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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21Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure
By Charles E. Harris
“Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure” Metadata:
- Title: ➤ Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure
- Author: Charles E. Harris
- 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
“Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure” Subjects and Themes:
- Subjects: ➤ Fuselages - Crack propagation - Computer programs - Crack initiation - Residual strength - Fatigue (Materials)
Edition Identifiers:
- The Open Library ID: OL17838756M
- Online Computer Library Center (OCLC) ID: 41033672
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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