Propulsion Science & Technology Inc SBIR Phase I Award, March 2019

This Phase I SBIR proposal describes the development of a hybrid modeling approach which uses both engineering solutions and high fidelity CFD solutions, to model maneuvering boost phase and reentry systems flying at angle of attack. The solution technique employs a 3D flowfield morphing technique which can be used as both a high fidelity flowfield interpolator or extrapolator to incorporate 3D spatial realism into the final solution.