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Effect of Pressure Gradients on Plate Response and Radiation in a Supersonic Turbulent Boundary Layer

Author(s):
Frendi, Abdelkader ( Analytical Services and Materials )  
Publication title:
NASA Technical Reports
Pub. Year:
1997
Vol.:
19970020055
Issue:
NASA-CR-201691
Pt.:
NAS 1.26:201691
Page(from):
1
Page(to):
40
Pages:
40
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

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