Approximate relation derived for surface velocity potential of wings when they are contained within Mach cone from vortex; this relation is applied to obtain pressure distributions, lift and rag coefficients, center of pressure, and rolling moments as function of angle of yaw for delta wing.
Effects of yawing thin pointed wings at supersonic speeds
Nat Advisory Committee Aeronautics -- Tech Note
1947
17 pages
9 Supp sheets
Report
Englisch
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Rolling and yawing moments for swept-back wings in sideslip at supersonic speeds
Engineering Index Backfile | 1951
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