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NUMERICAL COMPUTATION OF SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION IN TRANSONIC FLOW OVER AXISYMMETRIC CURVED HILL

Author(s):
kim, S. W. ( NASA )  
Publication title:
NASA Technical Reports(N89)
Pub. Year:
1989
Issue:
NASA-TM-101473
No.:
G3/34 0191958
Pt.:
NAS1.15:101473
Paper no.:
N89-21192
Page(from):
1
Page(to):
31
Pages:
31
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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