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Gust-tunnel Investigation of a Wing Model with Semichord Line Swept Back 60 Degrees
Document ID
19930082852
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pierce, Harold B
Date Acquired
August 16, 2013
Publication Date
October 1, 1950
Report/Patent Number
NACA-TN-2204
Accession Number
93R12142
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ACCELERATIONS, GUST
LOADS, GUST - WINGS, SWEPTBACK
WIND TUNNEL TESTS - NACA - GUST

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