Wall-temperature effects on the aerodynamics of a hydrogen-fueled transport concept in Mach 8 blowdown and shock tunnels/

Main Author: Penland, Jim A.
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: Marcum, Don C., Stack, Sharon H.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983
Series:NASA technical paper 2159
Subjects:
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245 1 0 |a Wall-temperature effects on the aerodynamics of a hydrogen-fueled transport concept in Mach 8 blowdown and shock tunnels/  |c Jim A. Penland, Don C. Marcum, Jr., and Sharon H. Stack 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c 1983 
300 |a 58 σ. :  |b εικ. ;  |c 28 εκ. 
490 0 |a NASA technical paper  |v 2159 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Aerodynamics, Hypersonic 
650 0 |a Boundary layer 
700 1 |a Marcum, Don C. 
700 1 |a Stack, Sharon H. 
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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