Supersonic and hypersonic flow of inviscid ideal gas over conical delta wings using three dimensional method of characteristics
A method for determining the complete flow field around conical wings at supersonic/ hypersonic speeds.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, FLUID AND PLASMA DYNAMICS CONFERENCE ; 1969 ; SAN FRANCISCO, CALIF.
1969-06-01
Conference paper
No indication
English
Charts for conical part of downwash field of swept wings at supersonic speeds
Engineering Index Backfile | 1948
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