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.

Bibliographic Details
Main Authors: Pittman, Jimmy L., (Author), Riebe, Gregory D., (Author)
Corporate Author: Langley Research Center.
Format: Book Government Document
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Series:NASA technical paper ; 1767.
Subjects:
Online Access:CONNECT
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100 1 |a Pittman, Jimmy L.,  |e author. 
245 1 0 |a Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /  |c Jimmy L. Pittman and Gregory D. Riebe. 
264 1 |a [Washington, D.C.] :  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c December 1980. 
300 |a 1 online resource (113 pages) :  |b illustrations. 
336 |a text  |b txt  |2 rdacontent. 
337 |a computer  |b c  |2 rdamedia. 
338 |a online resource  |b cr  |2 rdacarrier. 
490 1 |a NASA technical paper ;  |v 1767. 
500 |a Title from title screen (viewed on Aug. 19, 2016). 
500 |a "December 1980." 
500 |a "Performing Organization: NASA Langley Research Center"--Report documentation page. 
504 |a Includes bibliographical references (pages 14-15). 
513 |a Technical paper. 
536 |a National Aeronautics and Space Administration  |d 505-31-73-01  |d L-13868. 
650 7 |a Aerodynamic characteristics.  |2 nasat. 
650 7 |a Aerodynamic configurations.  |2 nasat. 
650 7 |a Angle of attack.  |2 nasat. 
650 7 |a Hypersonic aircraft.  |2 nasat. 
650 7 |a Supersonic aircraft.  |2 nasat. 
700 1 |a Riebe, Gregory D.,  |e author. 
710 2 |a Langley Research Center. 
710 1 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch,  |e issuing body. 
776 0 8 |i Print version:  |a Pittman, Jimmy L.  |t Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63  |w (OCoLC)7325143. 
776 0 8 |i Microfiche version:  |a Pittman, Jimmy L.  |t Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63  |w (OCoLC)711544698. 
830 0 |a NASA technical paper ;  |v 1767. 
856 4 0 |z CONNECT  |u http://purl.fdlp.gov/GPO/gpo71373 
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910 |a DWS