Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70̊ swept delta wing / Louis E. Clark and Christine B. Richie ; Langley Research Center.

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Online Access: Search for the full-text version of this title in HathiTrust
Main Author: Clark, Louis E.
Corporate Authors: United States. National Aeronautics and Space Administration, Langley Research Center
Other Authors: Richie, Christine B.
Format: Government Document Book
Language:English
Published: Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977.
Series:NASA technical memorandum ; X-3475.
Subjects:

MARC

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245 1 0 |a Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70̊ swept delta wing /  |c Louis E. Clark and Christine B. Richie ; Langley Research Center. 
260 |a Washington :  |b National Aeronautics and Space Administration ;  |a Springfield, Va. :  |b For sale by the National Technical Information Service,  |c 1977. 
300 |a 58 pages :  |b illustrations ;  |c 27 cm. 
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490 1 |a NASA technical memorandum ; NASA TM X-3475. 
500 |a Issued May 1977. 
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