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    Numerical Computation of the Chemically Reacting Flow around the National Aero-Space Plane (1999)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This final report summarizes the research accomplished. The research performed during the grant period can be divided into the following major areas: (1) Computation of chemically reacting Supersonic combustion ramjet (scramjet) flowfields. (2) Application of a two-equation turbulence model to supersonic combustion flowfields. (3) Computation of the integrated aerodynamic and propulsive flowfields of a generic hypersonic space plane. (4) Computation of hypersonic flows with finite-catalytic walls. (5) Development of an upwind Parabolized Navier-Stokes (PNS) code for thermo-chemical nonequilibrium flows.
    Keywords: Aerodynamics
    Format: application/pdf
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