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Flight Determination of the Longitudinal Stability Characteristics of a 0.133-Scale Rocket-Powered Model of the Consolidated Vultee XFY-1 Airplane without Propellers at Mach Numbers from 0.73 to 1.19, TED No. NACA DE 369A flight test has been conducted to determine the longitudinal stability and control,characteristics of a 0.133-scale model of the Consolidated Vultee XFY-1 airplane without propellers for the Mach number range between 0.73 and 1.19.
Document ID
20050030055
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Hastings, Earl E., Jr. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Mitcham, Grady L. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 22, 2013
Publication Date
February 3, 1954
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-SL54B03A
Report Number: NACA-RM-SL54B03A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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