Actively cooled plate fin sandwich structural panels for hypersonic aircraft/

Main Author: Smith, L. M.
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: Beuyukian, C. S.
Format: Book
Language:English
Published: Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979
Series:NASA contractor report NASA CR-3159
Subjects:
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040 |a GR-KoDPT  |b gre  |e AACR2 
100 1 |a Smith, L. M.  |q (Lee Mark) 
245 1 0 |a Actively cooled plate fin sandwich structural panels for hypersonic aircraft/  |c L.M. Smith and C.S. Beuyukian 
260 |a Washington, D.C.:  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c 1979 
300 |a ix, 164 σ. :  |b εικ. ;  |c 27 εκ. 
490 0 |a NASA contractor report  |v NASA CR-3159 
500 |a "Prepared for Langley Research Center under Contract NAS1-13382." 
504 |a Περιέχει βιβλιογραφικές παραπομπές 
650 0 |a Hypersonic planes 
650 0 |a Aerodynamic heating 
650 0 |a Airplanes  |x Motors 
700 1 |a Beuyukian, C. S.  |x Cooling 
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 0 |a Langley Research Center 
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