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
  1. 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.
Published by
  1. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Author
  1. Pittman, Jimmy L.

Available online

Details

Additional authors
  1. Riebe, Gregory D.
  2. Langley Research Center.
  3. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Description
  1. 1 online resource (113 pages) : illustrations.
Series statement
  1. NASA technical paper ; 1767
Uniform title
  1. NASA technical paper ; 1767.
Subject
  1. Aerodynamic characteristics
  2. Aerodynamic configurations
  3. Angle of attack
  4. Hypersonic aircraft
  5. Supersonic aircraft
Call number
  1. GPO Internet NAS 1.60:1767
Note
  1. Title from title screen (viewed on Aug. 19, 2016).
  2. "December 1980."
  3. "Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography (note)
  1. Includes bibliographical references (pages 14-15).
Type of report (note)
  1. Technical paper.
Funding (note)
  1. National Aeronautics and Space Administration
Author
  1. Pittman, Jimmy L., author.
Title
  1. 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
  1. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Type of content
  1. text
Type of medium
  1. computer
Type of carrier
  1. online resource
Series
  1. NASA technical paper ; 1767
  2. NASA technical paper ; 1767.
Bibliography
  1. Includes bibliographical references (pages 14-15).
Type of report
  1. Technical paper.
Funding
  1. National Aeronautics and Space Administration 505-31-73-01 L-13868
Connect to:
  1. https://purl.fdlp.gov/GPO/gpo71373
Added author
  1. Riebe, Gregory D., author.
  2. Langley Research Center.
  3. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Other form:
  1. 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
  2. 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.
  1. 0830-H-15 (online)
Sudoc no.
  1. NAS 1.60:1767
View in legacy catalog