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Aerodynamic Characteristics of a Revised Target Drone Vehicle at Mach Numbers from 1.60 to 2.86An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the aerodynamic characteristics of a revised target drone vehicle through a Mach number range from 1.60 to 2.86. The vehicle had canard surfaces and a swept clipped-delta wing with twin tip-mounted vertical tails.
Document ID
19980223973
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Blair, A. B., Jr. (NASA Langley Research Center Hampton, VA United States)
Babb, C. Donald (NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1968
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-5824
NASA-TM-SX-1532
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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