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CALCULATION OF COMPRESSIBLE FLOW ABOUT THREE-DIMENSIONAL INLETS WITH AUXILIARY INLETS, SLATS AND VANES BY MEANS OF A PANEL METHOD

Author(s):
Publication title:
NASA Technical Reports
Pub. Year:
1985
Issue:
NASA-CR-174975
No.:
G3/02 22236
Pt.:
NAS 1.26:174975
Paper no.:
N85-35162
Page(from):
1
Page(to):
197
Pages:
197
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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