Three dimensional flow simulations with the finite element technique over a multi-stage rocket
Author:
Affiliation:
1. Inst. Tecnologico de Aeronautica, Sao Jose dos Campos, Brazil
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-408
Reference19 articles.
1. Chimera simulations of viscous flows over a complex satellite launcher configuration
2. A Taylor-Galerkin method for convective transport problems
3. An adaptive finite element procedure for compressible high speed flows
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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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