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Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Longitudinal Stability and Control of the Model Equipped with a Supersonic-Type Elliptical Wing-Root InletNo abstract available
Document ID
19930088338
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Kelly, H Neale (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Cancro, Patrick A (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 16, 2013
Publication Date
July 21, 1954
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-SL54F28
Accession Number
93R17628
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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