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

Main Author: Pittman, Jimmy L.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Other Authors: Riebe, Gregory D.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Series:NASA technical paper 1767
Subjects:
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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 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c 1980 
300 |a 113 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA technical paper  |v 1767 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Aerodynamics, Supersonic 
650 0 |a Hypersonic planes 
650 0 |a Supersonic wind tunnels 
700 1 |a Riebe, Gregory D. 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Branch 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch 
710 2 |a Langley Research Center 
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