Analysis of Dynamic Stability of Space Launch Vehicles under Aerodynamic Forces Using CFD Derived Data

DOI10.1080/15502287.2010.542794zbMath1368.70034OpenAlexW2156265389MaRDI QIDQ3118310

M. Trikha, Deshabrata Roy Mahapatra, Srinivasan Gopalakrishnan

Publication date: 2 March 2012

Published in: International Journal for Computational Methods in Engineering Science and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/15502287.2010.542794

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Finite element, Rayleigh-Ritz and Galerkin methods for initial value and initial-boundary value problems involving PDEs (65M60) Orbital mechanics (70M20)

Cites Work

• Fluid dynamics of unsteady separated flow. Part I. Bodies of revolution
• Missile stability using finite elements - An unconstrained variational approach

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