Explore: *honeycomb Cores
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AI-Generated Overview About “%2Bhoneycomb-cores”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Compression 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
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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2Thermal behavior of a titanium honeycomb-core sandwich panel
By William L. Ko
“Thermal behavior of a titanium honeycomb-core sandwich panel” Metadata:
- Title: ➤ Thermal behavior of a titanium honeycomb-core sandwich panel
- Author: William L. Ko
- Language: English
- Number of Pages: Median: 13
- Publisher: ➤ National Technical Information Service, distributor] - NASA Ames Resarch Center, Dryden Flight Research Facility
- Publish Date: 1991
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Thermal behavior of a titanium honeycomb-core sandwich panel” Subjects and Themes:
- Subjects: ➤ Titanium - Aerodynamic heating - Airframes - Temperature effects - Honeycomb cores - Thermal stresses - Stress analysis - Finite element method
Edition Identifiers:
- The Open Library ID: OL17725161M - OL17633882M
- Online Computer Library Center (OCLC) ID: 57137031
Access and General Info:
- First Year Published: 1991
- 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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3Facesheet 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
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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4Evaluation 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
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:
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5Bonding and sealing evaluations for cryogenic tanks
By David E. Glass
“Bonding and sealing evaluations for cryogenic tanks” Metadata:
- Title: ➤ Bonding and sealing evaluations for cryogenic tanks
- Author: David E. Glass
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“Bonding and sealing evaluations for cryogenic tanks” Subjects and Themes:
- Subjects: ➤ Bonding - Cryogenic fluid storage - Adhesion tests - Honeycomb cores - Sealing - Reusable launch vehicles - Bonded joints
Edition Identifiers:
- The Open Library ID: OL15492294M
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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6An 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
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:
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Honeycomb structure
honeycomb cores is typically higher (at same weight) compared to other sandwich core structures such as, for instance, foam cores or corrugated cores
Sandwich-structured composite
patent the first use of honeycomb structures for structural applications. 1915 Hugo Junkers patents the first honeycomb cores for aircraft application
Northrop YF-17
a Nomex honeycomb core with composite facesheets. The rear of the aircraft had twin all-moving stabilators of aluminum over a honeycomb core, and twin
Pickleball
and Selkirk, use advanced materials like carbon fiber and polymer honeycomb cores to enhance control, power, and spin. One common paddle material is
Bugatti EB 110
(quotes) for aluminium skins with aluminium honeycomb core and an alternative with carbon-fibre skins and honeycomb core. Stanzani viewed the carbon-aluminium
Empacher
Empacher uses a vacuum bag technique to bond the outer layers with the honeycomb core. Combining kevlar and epoxy resin creates a tear and impact resistant
Honeycomb mirror
A honeycomb mirror is a large mirror usually used as the primary mirror in astronomical reflecting telescopes whose face is supported by a ribbed structure
Saturn V
employing facing sheets of 2014 aluminum alloy and fiberglass/phenolic honeycomb core to prevent heat transfer and retain the cryogenic properties of the
FORTE
graphite-reinforced epoxy. It consists of three decks with aluminum honeycomb cores, and composite facing to support the onboard instruments. FORTE "Los
Airframe
attaching stiffeners, such as hat sections to sheet, and face sheets to honeycomb cores. Also, adhesive bonding has withstood adverse exposures such as sea-water