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An improved method for the aerodynamic analysis of wing-body-tail configurations in subsonic and supersonic flow. Part 2: Computer program description

F. A. Woodward

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Key concepts: Aerodynamics, Wing, Supersonic speed, Choked flow, Flow (mathematics), Computer program, Mechanics, Computer science

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An improved method for the aerodynamic analysis of wing-body-tail configurations in subsonic and supersonic flow. Part 2: Computer program description — Research Paper | ScholarLens