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A Transonic Wind-Tunnel Investigation of the Performance and of the Static Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane, Ted No. NACA DE 390
Document ID
19690089286
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Bielat, R. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 5, 2013
Publication Date
October 1, 1954
Publication Information
Publisher: NACA
Subject Category
Unknown
Report/Patent Number
NACA-RM-SL54J15
Accession Number
69X72806
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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