Requirements: Ph.D. in Aerospace Engineering + experience in solid mechanics, structural dynamics and aeroelasticity
Requirements PhD in Mechanical Engineering. Experience in Fluid Dynamics, Heat Transfer, Thermodynamics, Compressible Flow, Thermo-Fluids and Numerical methods in Engineering Analysis, development of higher order codes for modeling high fidelity hypersonic ablative flows around re-entry geometries. Analytical and theoretical skills in developing robust and efficient Computational Fluid Dynamics (CFD) systems. Programming skills in C, C++, JAVA, FORTRAN, MATHEMATICA, MATLAB, OPENMPI.