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Procedure for automating aircraft wing structural designAircraft wings automated preliminary structural design and weight determination procedures based on external shape, aerodynamic loads and fuel mass interaction
Document ID
19710042577
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Giles, G. L.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Subject Category
Structural Mechanics
Meeting Information
Meeting: CONFERENCE ON ELECTRONIC COMPUTATION
Location: LAFAYETTE, IN
Start Date: August 31, 1970
End Date: September 2, 1970
Sponsors: AMERICAN SOCIETY OF CIVIL ENGINEERS
Accession Number
71A23274
Distribution Limits
Public
Copyright
Other

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