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Effect of 40 Degree Sweepback on the Spin and Recovery Characteristics of a 1/25-scale Model of a Typical Fighter-type Airplane as Determined by Free-spinning-tunnel Tests
Document ID
19930081844
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Scher, Stanley H
Date Acquired
August 16, 2013
Publication Date
April 1, 1947
Report/Patent Number
NACA-TN-1256
Report Number: NACA-TN-1256
Accession Number
93R11134
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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