摘要：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.
其他摘要：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.
