Explore: Skin (structural Member)
Discover books, insights, and more — all in one place.
Learn more about Skin (structural Member) with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “skin-%28structural-member%29”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Calculation of skin-stiffener interface stresses in stiffened composite panels
By David Cohen
“Calculation of skin-stiffener interface stresses in stiffened composite panels” Metadata:
- Title: ➤ Calculation of skin-stiffener interface stresses in stiffened composite panels
- Author: David Cohen
- Language: English
- Publisher: ➤ College of Engineering, Virginia Polytechnic Institute and State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - Blacksburg, Virginia - [Washington, DC
“Calculation of skin-stiffener interface stresses in stiffened composite panels” Subjects and Themes:
- Subjects: ➤ Composite materials - Interfaces - Panels - Skin (Structural member) - Stiffening - Stress analysis
Edition Identifiers:
- The Open Library ID: OL18079815M - OL18006577M - OL15411148M - OL14980316M
Access and General Info:
- First Year Published: 1987
- 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 Calculation of skin-stiffener interface stresses in stiffened composite panels at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Skin/stiffener interface stresses in composite stiffened panels
By James Ting-Shun Wang
“Skin/stiffener interface stresses in composite stiffened panels” Metadata:
- Title: ➤ Skin/stiffener interface stresses in composite stiffened panels
- Author: James Ting-Shun Wang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Lockheed-Georgia Company
- Publish Date: 1984
- Publish Location: Hampton, Va - Marietta, Ga
“Skin/stiffener interface stresses in composite stiffened panels” Subjects and Themes:
- Subjects: ➤ Buckling (Mechanics) - Composite materials - Composite structures - Interlayers - Panels - Skin (Structural member) - Stiffening - Stress analysis
Edition Identifiers:
- The Open Library ID: OL16156991M
Access and General Info:
- First Year Published: 1984
- 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 Skin/stiffener interface stresses in composite stiffened panels at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures
By Karen E. Jackson
“Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures” Metadata:
- Title: ➤ Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures
- Author: Karen E. Jackson
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures” Subjects and Themes:
- Subjects: ➤ Testing - Transport aircraft - Aluminum - Abrasion - Airplanes - Skin (Structural member) - Runways - Graphite-epoxy composites - Aluminum compounds - Fuselage - Epoxy compounds - Panels - Crash landing - Skid landings
Edition Identifiers:
- The Open Library ID: OL16116666M
Access and General Info:
- First Year Published: 1985
- 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 Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Fatigue debonding characterization in composite skin/stringer configurations
By Michael K. Cvitkovich
“Fatigue debonding characterization in composite skin/stringer configurations” Metadata:
- Title: ➤ Fatigue debonding characterization in composite skin/stringer configurations
- Author: Michael K. Cvitkovich
- 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
“Fatigue debonding characterization in composite skin/stringer configurations” Subjects and Themes:
- Subjects: ➤ Debonding (Materials) - Delaminating - Fatigue tests - Crack initiation - Skin (Structural member) - Composite structures - Graphite-epoxy composites - Flanges - Bonded joints - Resin matrix composites
Edition Identifiers:
- The Open Library ID: OL15482784M
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.
Online Borrowing:
Online Marketplaces
Find Fatigue debonding characterization in composite skin/stringer configurations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5A proof of concept experiment for reducing skin friction by using a micro-blowing technique
By Danny P. Hwang
“A proof of concept experiment for reducing skin friction by using a micro-blowing technique” Metadata:
- Title: ➤ A proof of concept experiment for reducing skin friction by using a micro-blowing technique
- Author: Danny P. Hwang
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“A proof of concept experiment for reducing skin friction by using a micro-blowing technique” Subjects and Themes:
- Subjects: Skin friction - Friction reduction - Porous plates - Blowing - Skin (Structural member)
Edition Identifiers:
- The Open Library ID: OL15497461M
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.
Online Borrowing:
Online Marketplaces
Find A proof of concept experiment for reducing skin friction by using a micro-blowing technique at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Stressed skin
skin is a rigid construction in which the skin or covering takes a portion of the structural load, intermediate between monocoque, in which the skin assumes
Monocoque
MON-ə-ko(h)k), also called structural skin, is a structural system in which loads are supported by an object's external skin, in a manner similar to an
Ectodysplasin A receptor
in the development of ectodermal tissues such as the skin. It is structurally related to members of the TNF receptor superfamily. EDAR and other genes
Structural insulated panel
stress-skinned panels, it was suggested stronger skins could take all the structural load and eliminate the frame altogether. Thus in 1947, structural insulated
National Institute of Arthritis and Musculoskeletal and Skin Diseases
muscles, and skin. Basic research involves a wide variety of scientific disciplines, including immunology, genetics, molecular biology, structural biology
Buckling
In structural engineering, buckling is the sudden change in shape (deformation) of a structural component under load, such as the bowing of a column under
Discrimination based on skin tone
a structural system of oppression that benefited individuals of European descent over individuals of African descent. Biological differences in skin color
Spar (aeronautics)
while on the ground. Other structural and forming members such as ribs may be attached to the spar or spars, with stressed skin construction also sharing
Ehlers–Danlos syndrome
disorders. Symptoms often include loose joints, joint pain, stretchy, velvety skin, and abnormal scar formation. These may be noticed at birth or in early childhood
Stringer
skin of an aircraft is fastened Stringer (slag), an inclusion, possibly leading to a defect, in cast metal Stringer (stairs), the structural member in