Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63

Main Author: Pittman, Jimmy L.,
Other Authors: Riebe, Gregory D.,, Langley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch,
Format: eBook
Language: English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Physical Description: 1 online resource (113 pages) : illustrations.
Series: NASA technical paper ; 1767.
Online Access: https://purl.fdlp.gov/GPO/gpo71373
https://purl.fdlp.gov/GPO/gpo71373

CMU Gov Pub Electronic

LocationCall Number: Status
CMU Gov Pub Electronic NAS 1.60:1767 Online