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Aerodynamic characteristics of a family of multistage missiles at a mach number of 6.0

E. Leon Morrisette, David J. Romeo

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Abstract

Wind tunnel investigation of aerodynamic characteristics of cone-cylinder-flare multistage missile configurations at supersonic speed

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Wind tunnel investigation of aerodynamic characteristics of cone-cylinder-flare multistage missile configurations at supersonic speed

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Available abstract

Wind tunnel investigation of aerodynamic characteristics of cone-cylinder-flare multistage missile configurations at supersonic speed

Key concepts: Mach number, Aerodynamics, Aeronautics, Aerospace engineering, Computer science, Engineering

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