Three dimensional flow simulations with the finite element technique over a multi-stage rocket

Author:

Scalabrin L.1,Azevedo J.,Teixeira P.,Awruch A.

Affiliation:

1. Inst. Tecnologico de Aeronautica, Sao Jose dos Campos, Brazil

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Numerical simulations of three-dimensional flow over a multi-stage rocket using finite volumes;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2015-03-20

2. Computational Aeroelastic Analysis of the Ares I Crew Launch Vehicle During Ascent;Journal of Spacecraft and Rockets;2012-07

3. Flexible Launch Stability Analysis Using Steady and Unsteady Computational Fluid Dynamics;Journal of Spacecraft and Rockets;2012-07

4. A Quasi-Steady Flexible Launch Vehicle Stability Analysis Using Steady CFD with Unsteady Aerodynamic Enhancement;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

5. Computational Aeroelastic Analysis of the Ares Crew Launch Vehicle During Ascent;28th AIAA Applied Aerodynamics Conference;2010-06-28

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