Explore: Sandwich Structures
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Source: The Open Library
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Search results from The Open Library
1Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces
By William L. Ko
“Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces” Metadata:
- Title: ➤ Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces
- Author: William L. Ko
- Language: English
- Number of Pages: Median: 37
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - Hanover, Md - Edwards, Calif
“Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces” Subjects and Themes:
- Subjects: ➤ Debonding (Materials) - Stress distribution - Curved panels - Sandwich structures - Structural engineering - Aerospace engineering - Composite materials - Sandwich construction - Hypersonic planes - Testing - Research - Aerothermodynamics - Delamination - Deterioration
Edition Identifiers:
- The Open Library ID: OL18137667M - OL17136008M - OL15556458M - OL19158922M - OL17591577M
- Online Computer Library Center (OCLC) ID: 42885460
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Study 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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3A higher-order bending theory for laminated composite and sandwich beams
By Geoffrey M. Cook
“A higher-order bending theory for laminated composite and sandwich beams” Metadata:
- Title: ➤ A higher-order bending theory for laminated composite and sandwich beams
- Author: Geoffrey M. Cook
- 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
“A higher-order bending theory for laminated composite and sandwich beams” Subjects and Themes:
- Subjects: ➤ Bending theory - Shear stress - Laminates - Sandwich structures - Beams (Supports) - Stress-strain relationships
Edition Identifiers:
- The Open Library ID: OL17572299M - OL17125322M - OL18118863M - OL15498732M
- Online Computer Library Center (OCLC) ID: 39776136
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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4Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments
By William L. Ko
“Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments” Metadata:
- Title: ➤ Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments
- Author: William L. Ko
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Dryden Flight Research Facility
- Publish Date: 1991
- Publish Location: ➤ [Washington, DC] - Edwards, Calif
“Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments” Subjects and Themes:
- Subjects: Metallic composites - Buckling (Mechanics) - Sandwich structures - Metal matrix composites - Buckling
Edition Identifiers:
- The Open Library ID: OL17102294M - OL18034828M - OL21499506M - OL15298935M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Reactivity of [pi]-complexes of Ti, V, and Nb towards dithioacetic acid
By Stan A. Duraj
“Reactivity of [pi]-complexes of Ti, V, and Nb towards dithioacetic acid” Metadata:
- Title: ➤ Reactivity of [pi]-complexes of Ti, V, and Nb towards dithioacetic acid
- Author: Stan A. Duraj
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Reactivity of [pi]-complexes of Ti, V, and Nb towards dithioacetic acid” Subjects and Themes:
- Subjects: ➤ Desulfurizing - Vanadium - Sandwich structures - Catalysts - Niobium alloys - Reactivity - Metal surfaces - Catalysis - Synthesis (Chemistry)
Edition Identifiers:
- The Open Library ID: OL18077331M - OL15405817M - OL17114270M
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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6Compression response of a sandwich fuselage keel panel with and without damage
By David M. McGowan
“Compression response of a sandwich fuselage keel panel with and without damage” Metadata:
- Title: ➤ Compression response of a sandwich fuselage keel panel with and without damage
- Author: David M. McGowan
- 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
“Compression response of a sandwich fuselage keel panel with and without damage” Subjects and Themes:
- Subjects: ➤ Fuselages - Graphite-epoxy composites - Honeycomb cores - Sandwich structures - Impact damage - Composite structures - Finite element method
Edition Identifiers:
- The Open Library ID: OL17806199M - OL15452252M
- Online Computer Library Center (OCLC) ID: 37496094
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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7Military handbook no. 23A. Structural sandwich composites
By United States. Dept. of Defense.
“Military handbook no. 23A. Structural sandwich composites” Metadata:
- Title: ➤ Military handbook no. 23A. Structural sandwich composites
- Author: ➤ United States. Dept. of Defense.
- Publisher: Dept. of Defense
- Publish Date: 1968
- Publish Location: Washington, D. C
“Military handbook no. 23A. Structural sandwich composites” Subjects and Themes:
- Subjects: Sandwich structures - Composite materials
Edition Identifiers:
- The Open Library ID: OL20268380M
Author's Alternative Names:
"Defense Dept. (U.S.)", "U S Department of Defense", "U.S. Department of Defense", "U. S. Department of Defense", "[United States. Dept. of Defense]", "Us Department of Defense", "United States. Dept . of Defense", "U S Dept of Defense", "U.S. Dept. of Defense.", "U. S. Dept. of Defense.", "U.S. Dept. of Defense", "United States Department of Defense", "United States. Dept. of Defense", "U.S. Government Department of Defense", "United States. Department of Defense.",Access and General Info:
- First Year Published: 1968
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)
By Joanne L. Walsh
“Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)” Metadata:
- Title: ➤ Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)
- Author: Joanne L. Walsh
- Language: English
- Number of Pages: Median: 113
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2005
- Publish Location: Hampton, Va
“Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)” Subjects and Themes:
- Subjects: ➤ Body-wing configurations - Canard configurations - Aeroelasticity - Sandwich structures - Longitudinal control - Design analysis - Composite materials
Edition Identifiers:
- The Open Library ID: OL43894466M
- Online Computer Library Center (OCLC) ID: 781856606
Access and General Info:
- First Year Published: 2005
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9The 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
Online Access
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10Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage
By A. J. Hodge
“Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage” Metadata:
- Title: ➤ Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage
- Author: A. J. Hodge
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 2011
- Publish Location: Huntsville], Ala
“Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage” Subjects and Themes:
- Subjects: ➤ Compressive strength - Sandwich structures - Carbon fibers - Impact strength - Damage - Epoxy matrix composites - Laminates - Fiber composites
Edition Identifiers:
- The Open Library ID: OL43927530M
- Online Computer Library Center (OCLC) ID: 747568690
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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11Buckling of composite sandwich cylinders under axial compression
By E. W. Cheung
“Buckling of composite sandwich cylinders under axial compression” Metadata:
- Title: ➤ Buckling of composite sandwich cylinders under axial compression
- Author: E. W. Cheung
- Number of Pages: Median: 181
- Publisher: Elsevier Science Publishers
- Publish Date: 1988
- Publish Location: Amsterdam
“Buckling of composite sandwich cylinders under axial compression” Subjects and Themes:
- Subjects: Sandwich structures - Composite materials - Cylinders - Axial compression loads - Buckling
Edition Identifiers:
- The Open Library ID: OL18927156M
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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12Facesheet wrinkling in sandwich structures
By Robert P. Ley
“Facesheet wrinkling in sandwich structures” Metadata:
- Title: ➤ Facesheet wrinkling in sandwich structures
- Author: Robert P. Ley
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Facesheet wrinkling in sandwich structures” Subjects and Themes:
- Subjects: Sandwich structures - Wrinkling - Honeycomb cores - Design analysis
Edition Identifiers:
- The Open Library ID: OL15542668M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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13Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure
By R. Keith Bird
“Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure” Metadata:
- Title: ➤ Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure
- Author: R. Keith Bird
- 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
“Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure” Subjects and Themes:
- Subjects: ➤ Mechanical properties - Honeycomb cores - Titanium alloys - Liquid phases - Titanium aluminides - Titanium - Intermetallics - Compressive strength - Bonded joints - Sandwich structures - Hypersonic vehicles
Edition Identifiers:
- The Open Library ID: OL15542768M
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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14Room temperature and elevated temperature composite sandwich joint testing
By Sandra P. Walker
“Room temperature and elevated temperature composite sandwich joint testing” Metadata:
- Title: ➤ Room temperature and elevated temperature composite sandwich joint testing
- Author: Sandra P. Walker
- 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
“Room temperature and elevated temperature composite sandwich joint testing” Subjects and Themes:
- Subjects: ➤ Fatigue tests - Failure modes - Sandwich structures - High temperature - Composite structures - Fatigue life
Edition Identifiers:
- The Open Library ID: OL15546626M
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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15An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels
By A. T. Nettles
“An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels” Metadata:
- Title: ➤ An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels
- Author: A. T. Nettles
- Language: English
- 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: ➤ Washington, D.C - [Springfield, VA
“An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels” Subjects and Themes:
- Subjects: ➤ Phenolic resins - Aluminum - Testing - Impact - Glass fiber reinforced plastics - Glass - Sandwich structures - Impact damage - Graphite-epoxy composites - Composite materials - Honeycomb structures - Honeycomb cores
Edition Identifiers:
- The Open Library ID: OL16131120M
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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16Damage 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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17Buckling analysis of debonded sandwich panel under compression
By David W. Sleight
“Buckling analysis of debonded sandwich panel under compression” Metadata:
- Title: ➤ Buckling analysis of debonded sandwich panel under compression
- Author: David W. Sleight
- Number of Pages: Median: 10
- Publisher: Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va
“Buckling analysis of debonded sandwich panel under compression” Subjects and Themes:
- Subjects: Sandwich structures - Buckling
Edition Identifiers:
- The Open Library ID: OL19005405M
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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18A three-node C(superscript)0 element for analysis of laminated composite sandwich shells
By C. Wayne Martin
“A three-node C(superscript)0 element for analysis of laminated composite sandwich shells” Metadata:
- Title: ➤ A three-node C(superscript)0 element for analysis of laminated composite sandwich shells
- Author: C. Wayne Martin
- Number of Pages: Median: 13
- Publisher: Ames Research Center
- Publish Date: 1989
- Publish Location: Edwards, Calif
“A three-node C(superscript)0 element for analysis of laminated composite sandwich shells” Subjects and Themes:
- Subjects: Sandwich structures - Structural analysis - Composite materials - Finite element method - Shells
Edition Identifiers:
- The Open Library ID: OL19379634M
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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19Study of impact damage of Nomex honeycomb sandwich plates
By Zhang Tao
“Study of impact damage of Nomex honeycomb sandwich plates” Metadata:
- Title: ➤ Study of impact damage of Nomex honeycomb sandwich plates
- Author: Zhang Tao
- Publisher: ➤ School of Aeronautics, Harbin Institute of Technology
- Publish Date: 1989
- Publish Location: ➤ Harbin, Heilongjiang Province, China
“Study of impact damage of Nomex honeycomb sandwich plates” Subjects and Themes:
- Subjects: Impact - Sandwich structures - Impact damage
Edition Identifiers:
- The Open Library ID: OL21041792M
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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20Buckling of composite sandwich cylinders under axial compression
By Eric Waihon Cheung
“Buckling of composite sandwich cylinders under axial compression” Metadata:
- Title: ➤ Buckling of composite sandwich cylinders under axial compression
- Author: Eric Waihon Cheung
- Number of Pages: Median: 77
- Publisher: ➤ Dept. of Aerospace Science and Engineering, University of Toronto
- Publish Date: 1988
- Publish Location: [Downsview, Ont.]
“Buckling of composite sandwich cylinders under axial compression” Subjects and Themes:
- Subjects: Sandwich structures - Cylindrical shells - Composite materials - Axial compression loads - Buckling
Edition Identifiers:
- The Open Library ID: OL20898067M
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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21Buckling and postbuckling behavior of sandwich structures in the presence of a delamination
By M. Somers
“Buckling and postbuckling behavior of sandwich structures in the presence of a delamination” Metadata:
- Title: ➤ Buckling and postbuckling behavior of sandwich structures in the presence of a delamination
- Author: M. Somers
- Number of Pages: Median: 68
- Publisher: ➤ Technion Israel Institute of Technology, Dept. of Aeronautical Engineering
- Publish Date: 1989
- Publish Location: Haifa
“Buckling and postbuckling behavior of sandwich structures in the presence of a delamination” Subjects and Themes:
- Subjects: Sandwich structures - Composite structures - Delaminating - Buckling
Edition Identifiers:
- The Open Library ID: OL19380230M
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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22Effect of delamination location on postbuckling behavior of sandwich structures
By M. Somers
“Effect of delamination location on postbuckling behavior of sandwich structures” Metadata:
- Title: ➤ Effect of delamination location on postbuckling behavior of sandwich structures
- Author: M. Somers
- Number of Pages: Median: 48
- Publisher: ➤ Technion-Israel Institute of Technology, Faculty of Aerospace Engineering
- Publish Date: 1989
- Publish Location: Haifa, Israel
“Effect of delamination location on postbuckling behavior of sandwich structures” Subjects and Themes:
- Subjects: Sandwich structures - Damage - Composite materials - Buckling - Delaminating
Edition Identifiers:
- The Open Library ID: OL21041734M
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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23Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates
By Alexander Tessler
“Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates” Metadata:
- Title: ➤ Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates
- Author: Alexander Tessler
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2012
- Publish Location: Hampton, Va
“Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates” Subjects and Themes:
- Subjects: ➤ Composite structures - Laminates - Sandwich structures - Shear stress - Computational mechanics - Finite element method
Edition Identifiers:
- The Open Library ID: OL43987889M
- Online Computer Library Center (OCLC) ID: 809656201
Access and General Info:
- First Year Published: 2012
- 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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24Fiber composite sandwich thermostuctural behavior, computationalsimulation
By C. C. Chamis
“Fiber composite sandwich thermostuctural behavior, computationalsimulation” Metadata:
- Title: ➤ Fiber composite sandwich thermostuctural behavior, computationalsimulation
- Author: C. C. Chamis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Fiber composite sandwich thermostuctural behavior, computationalsimulation” Subjects and Themes:
- Subjects: ➤ Computerized simulation - Dimensional stability - Fiber composites - Honeycomb structures - Hydrothermal stress analysis - Hygral properties - Laminates - Sandwich structures - Shear properties - Structural analysis - Thermal expansion
Edition Identifiers:
- The Open Library ID: OL17115618M
Access and General Info:
- First Year Published: 1986
- 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.
Online Borrowing:
Online Marketplaces
Find Fiber composite sandwich thermostuctural behavior, computationalsimulation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.