Perturbation field induced by line vortex in supersonic stream and downwash behind supersonic lifting surface, examined to establish approximate methods for determining downwash behind supersonic wings.
Line-vortex theory for calculation of supersonic downwash
Nat Advisory Committee Aeronautics -- Report
1950
16 pages
Diagrs, Graphs
Report
English
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Line vortex theory for calculation of supersonic downwash
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