Generalized linearized conical flow

W. D. Hayes, R. C. Roberts, N. Haaser
naca-tn-2667
Mar 1952


A basic theory of generalized linearized supersonic conical flow for both inside and outside the Mach cone was developed and applied to several specific problems including unsteady-flow conditions. A triangular lifting wing in pitching and rolling with both subsonic and supersonic leading edges was investigated and pressure coefficients were obtained.

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