Research Catalog

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

Title
Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / Jimmy L. Pittman and Gregory D. Riebe.
Author
Pittman, Jimmy L.
Publication
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.

Available Online

https://purl.fdlp.gov/GPO/gpo71373

Details

Additional Authors
  • Riebe, Gregory D.
  • Langley Research Center.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Description
1 online resource (113 pages) : illustrations.
Series Statement
NASA technical paper ; 1767
Uniform Title
NASA technical paper ; 1767.
Subject
  • Aerodynamic characteristics
  • Aerodynamic configurations
  • Angle of attack
  • Hypersonic aircraft
  • Supersonic aircraft
Note
  • Title from title screen (viewed on Aug. 19, 2016).
  • "December 1980."
  • "Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography (note)
  • Includes bibliographical references (pages 14-15).
Type of Report (note)
  • Technical paper.
Funding (note)
  • National Aeronautics and Space Administration
Call Number
GPO Internet NAS 1.60:1767
OCLC
marcive761078951
Author
Pittman, Jimmy L., author.
Title
Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / Jimmy L. Pittman and Gregory D. Riebe.
Publisher
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA technical paper ; 1767
NASA technical paper ; 1767.
Bibliography
Includes bibliographical references (pages 14-15).
Type Of Report
Technical paper.
Funding
National Aeronautics and Space Administration 505-31-73-01 L-13868
Connect to:
https://purl.fdlp.gov/GPO/gpo71373
Added Author
Riebe, Gregory D., author.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Other Form:
Print version: Pittman, Jimmy L. Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 (OCoLC)7325143
Microfiche version: Pittman, Jimmy L. Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 (OCoLC)711544698
Gpo Item No.
0830-H-15 (online)
Sudoc No.
NAS 1.60:1767
View in Legacy Catalog