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A Method for Calculating the Subsonic Steady-state Loading on an Airplane with a Wing of Arbitrary Plan Form and Stiffness
Document ID
19930083851
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gray, W L (Boeing Airplane Company)
Schenk, K M (Boeing Airplane Company)
Date Acquired
August 16, 2013
Publication Date
December 1, 1953
Report/Patent Number
NACA-TN-3030
Accession Number
93R13141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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