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Aerodynamics of Supersonic Aircraft

W. D. Middleton, J. L. Lundry, Roger G. Coleman

Abstract

An integrated system for the analysis of supersonic configurations consists of an executive driver and eight basic computer programs that build up force coefficients of an selected configuration. System employs modified linearized theory for calculation of surface pressures and employs supersonic-area-rule concepts in combination with linearized theory for calculation of aerodynamic force coefficients.

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Available abstract

Key concepts: Supersonic speed, Aerodynamics, Aerospace engineering, Aerodynamic force, Engineering, Control theory (sociology), Computer science, Mechanics