Computational Aeroelastic Analysis of the Ares I Crew Launch Vehicle During Ascent
Flexible Launch Vehicle Stability Analysis Using Steady and Unsteady Computational Fluid Dynamics
An Aeroelastic Analysis of a Thin Flexible Membrane AIAA Paper 2007-2316 CD-ROM Number 7
Developing an Accurate CFD Based Gust Model for the Truss Braced Wing Aircraft
Computation of Shock Buffet Onset for a Conventional and Supercritical Airfoil