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Tests of a 45 Degree Sweptback-wing Model in the Langley Gust Tunnel
Document ID
19930082210
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pierce, Harold B
Date Acquired
August 16, 2013
Publication Date
February 1, 1948
Report/Patent Number
NACA-TN-1528
Report Number: NACA-TN-1528
Accession Number
93R11500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOADS, GUST - WINGS, SWEPTBACK
INTERFERENCE - WINGS & FUSELAGES
AIRFOILS - NACA 0012
ACCELERATIONS, GUST

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