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    Afterbody External Aerodynamic and Performance Prediction at High Reynolds Numbers (1999)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: This CFD experiment concludes that the potential difference between the flow between a flight Reynolds number test and a sub-scale wind tunnel test are substantial for this particular nozzle boattail geometry. The early study was performed using a linear k-epsilon turbulence model. The present study was performed using the Girimaji formulation of a algebraic Reynolds stress turbulent simulation.
    Keywords: Aerodynamics
    Type: First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop; Part 1; 321-333; NASA/CP-1999-209690/PT1
    Format: application/pdf
    Location Call Number Expected Availability
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