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    Characteristics of the Shuttle Orbiter leeside flow during a reentry condition (1992)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: A study of the leeside flow characteristics of the Shuttle Orbiter is presented for a reentry flight condition. The flow is computed using a point-implicit, finite-volume scheme known as the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA). LAURA is a second-order accurate, laminar Navier-Stokes solver, incorporating finite-rate chemistry with a radiative equilibrium wall temperature distribution and finite-rate wall catalysis. The resulting computational solution is analyzed in terms of salient flow features and the surface quantities are compared with flight data.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 92-2951
    Format: text
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