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Failure mechanisms of laminates transversely loaded by bolt push-through /

Bibliographic Details
Main Author: Waters, William Allen
Corporate Author: Langley Research Center
Other Authors: Williams, Jerry G.
Format: Government Document Book
Language:English
Published: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
Series:NASA technical memorandum ; 87603.
Subjects:
Bolted joints.
Airplanes > Fuselage.
Airframes > Fatigue.
Adhesive bonding.
Bolts.
Composite materials.
Failure modes.
Fuselages.
Interlayers.
Laminates.
Loads (Forces)
Panels.
Stiffening.
Toughness.
Wing panels.
Online Access:https://purl.fdlp.gov/gPO/LPS85281

Internet

https://purl.fdlp.gov/gPO/LPS85281

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Call Number: NAS 1.15:87603
 
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Call Number: NAS 1.15:87603
 
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NAS 1.15:87603 Available