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Influence of Tail Length upon the Spin-recovery Characteristics of a Trainer-type-airplane Model
Document ID
19930082437
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Klinar, Walter J
Snyder, Thomas L
Date Acquired
August 16, 2013
Publication Date
December 1, 1948
Report/Patent Number
NACA-TN-1764
Report Number: NACA-TN-1764
Accession Number
93R11727
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPINNING - RECOVERY
WIND TUNNEL TESTS - NACA - FREE-SPINNING (20') WORK CARRIED ON AT LAL
TAIL SURFACES, EXTENDED
FINS, VENTRAL
AIRPLANES, TRAINING

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