Kids Library Home

Welcome to the Kids' Library!

Search for books, movies, music, magazines, and more.

     
Available items only
E-Books/E-Docs
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.

Publication Info. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:1767    ---  Available
Description 1 online resource (113 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series NASA technical paper ; 1767
NASA technical paper ; 1767.
Note Title from title screen (viewed on Aug. 19, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography Includes bibliographical references (pages 14-15).
Type Of Report Technical paper.
Funding National Aeronautics and Space Administration 505-31-73-01 L-13868
Subject Aerodynamics, Supersonic.
Hypersonic planes.
Supersonic wind tunnels.
Mach number.
Aerodynamics, Supersonic. (OCoLC)fst00798221
Hypersonic planes. (OCoLC)fst00965814
Mach number. (OCoLC)fst01004756
Supersonic wind tunnels. (OCoLC)fst01139019
Aerodynamic characteristics.
Aerodynamic configurations.
Angle of attack.
Hypersonic aircraft.
Supersonic aircraft.
Genre/Form Online resources.
Electronic books.
Electronic government information.
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

 
    
Available items only