Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /

Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /

Bibliographic Details
Main Author: Blair, A. B.
Corporate Authors: Langley Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington : U.S. National Aeronautics and Space Administration ; 1976.
Series:NASA technical memorandum ; NASA TM X-3376.
Subjects:
Aerodynamics, Supersonic.
Airplanes > Wings, Triangular.
Stability of space vehicles.

Evans: US Documents (Annex 5th floor)

Holdings details from Evans: US Documents (Annex 5th floor)
Call Number: NAS 1.15:X-3376
 
Call Number Status Get It
NAS 1.15:X-3376 Available