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    Comparison of 3D computation and experiment for non-axisymmetric nozzles (1989)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: Three-dimensional solutions of a single expansion ramp nozzle are computed with the existing PARC computer code by solving the full Navier-Stokes equations. The computations are performed to simulate the non-axisymmetric nozzle flowfield in both the internal/external expansion regions and the exhaust plume in a quiescent ambient environment. Two different configurations of the nozzle at a pressure ratio NPR = 10 are examined. Numerical results of laminar flows are presented, and the wall pressure distributions are compared with the experimental data.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: AIAA PAPER 89-0007
    Format: text
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