Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
By: Ira J. Walker, Peter F. Covell And Dana K. Forrest.
Contributors: Covell, Peter F.; Forrest, Dana K.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA technical memorandum -- 4413.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; National Technical Information Service, distributor]
Published: 1993
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Canard configurations.; Delta wings.; Hypersonic vehicles.; Hypersonics.; Mach number.; Research vehicles.; Stabilizers (Fluid dynamics).; Tail assemblies.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0058-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 2 microfiches.