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High Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 1/16-Scale Model of the D-558-2 Research Airplane at High Subsonic Mach Number and at a Mach Number of 1.2No abstract available
Document ID
19930085883
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Osborne, Robert S (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 16, 2013
Publication Date
April 5, 1949
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L9C04
Accession Number
93R15173
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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