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Structural analysis of a parawing during deploymentFinite element analysis of critical stress distribution in canopy of deployed twin keel parawing, predicting failure stress levels
Document ID
19700065704
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kenner, P. M.
Date Acquired
August 5, 2013
Publication Date
September 1, 1970
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 70-1196
Report Number: AIAA PAPER 70-1196
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AERODYNAMIC DECELERATION SYSTEMS CONFERENCE
Location: DAYTON, OH
Start Date: September 14, 1970
End Date: September 16, 1970
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A41820
Funding Number(s)
CONTRACT_GRANT: NAS1-6957
Distribution Limits
Public
Copyright
Other

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