Source-sink method of R. T. JONES used to determine wave drag coefficients at zero angle of attack of family of unswept wings with diamond airfoil section; charts presented permit rapid determination of drag coefficient at any supersonic Mach number, aspect ratio, and taper.
Effect of aspect ratio and taper on pressure drag at supersonic speeds of unswept wings at zero lift
Nat Advisory Committee Aeronautics -- Tech Note
1947
22 pages
10 Supp Plates
Report
Englisch
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