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The effects of yawing thin pointed wings at supersonic speeds

JOHN C. EVVARD

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Abstract

suMlmRY -An spjy?oximat,e relation M derived for the surface velocity potential of thin pointed.Wj.ngsat supersonic speeds when they are contained within the Mach cone from the vertex.This relation is applied to obtain the p~essure distributions, the lift and drag coefficients, a function of are presented the center of pressurej and th~rolling moments & angle of yaw for the delta wing.Theoretical curves for a Mach number of @ to illustrate the relations.'-

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suMlmRY -An spjy?oximat,e relation M derived for the surface velocity potential of thin pointed.Wj.ngsat supersonic speeds when they are contained within the Mach cone from the vertex.This relation is applied to obtain the p~essure distributions, the lift and drag coefficients, a function of are presented the center of pressurej and th~rolling moments & angle of yaw for the delta wing.Theoretical curves for a Mach number of @ to illustrate the relations.'-

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Available abstract

suMlmRY -An spjy?oximat,e relation M derived for the surface velocity potential of thin pointed.Wj.ngsat supersonic speeds when they are contained within the Mach cone from the vertex.This relation is applied to obtain the p~essure distributions, the lift and drag coefficients, a function of are presented the center of pressurej and th~rolling moments & angle of yaw for the delta wing.Theoretical curves for a Mach number of @ to illustrate the relations.'-

Key concepts: Supersonic speed, Aeronautics, Mechanics, Physics, Engineering

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