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Aerodynamic characteristics of two blunt, half-cone wedge entry configurations at Mach numbers from 2.30 to 4.63

Gerald V. Foster

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Abstract

Aerodynamic characteristics of two blunt half cone wedge entry configurations at supersonic speeds

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Aerodynamic characteristics of two blunt half cone wedge entry configurations at supersonic speeds

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Available abstract

Aerodynamic characteristics of two blunt half cone wedge entry configurations at supersonic speeds

Key concepts: Mach number, Wedge (geometry), Aerodynamics, Cone (formal languages), Sonic boom, Physics, Blunt, Angle of attack

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Aerodynamic characteristics of two blunt, half-cone wedge entry configurations at Mach numbers from 2.30 to 4.63 — Research Paper | ScholarLens