Welcome to the Kids' Library!

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

Available items only

Previous Record Next Record

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.

Connect to
Connect to http://purl.fdlp.gov/GPO/gpo71373

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