Cómputo del Flujo Subsónico en Cuerpos en Presencia de Superficies Alares

Juan E. Pardi


It is my intention to mention in this Scientific Comunication the development in the Computational Mechanics field to compute pressure distribution of aerodynamics origin in rockets, missiles and general aircraft, with a fuselage in presence of wing surfaces in subsonic regime.

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Asociación Argentina de Mecánica Computacional
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ISSN 2591-3522