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  • 1
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    A multistage time-stepping scheme for the thin-layer Navier-Stokes equations (1986)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: A finite-volume scheme for numerical integration of the Euler equations was extended to allow solution of the thin-layer Navier-Stokes equations in two and three dimensions. The extended algorithm, which is based on a class of four-stage Runge-Kutta time-stepping schemes, was made numerically efficient through the following convergence acceleration technique: (1) local time stepping, (2) enthalpy damping, and (3) residual smoothing. Also, the high degree of vectorization possible with the algorithm has yielded an efficient program for vector processors. The scheme was evaluated by solving laminar and turbulent flows. Numerical results have compared well with either theoretical or other numerical solutions and/or experimental data.
    Keywords: AERODYNAMICS
    Type: Langley Symposium on Aerodynamics, Volume 1; p 109-135
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Numerical solutions of the Navier-Stokes equations for transonic afterbody flows (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The time dependent Navier-Stokes equations in mass averaged variables are solved for transonic flow over axisymmetric boattail plume simulator configurations. Numerical solution of these equations is accomplished with the unsplit explict finite difference algorithm of MacCormack. A grid subcycling procedure and computer code vectorization are used to improve computational efficiency. The two layer algebraic turbulence models of Cebeci-Smith and Baldwin-Lomax are employed for investigating turbulence closure. Two relaxation models based on these baseline models are also considered. Results in the form of surface pressure distribution for three different circular arc boattails at two free stream Mach numbers are compared with experimental data. The pressures in the recirculating flow region for all separated cases are poorly predicted with the baseline turbulence models. Significant improvements in the predictions are usually obtained by using the relaxation models.
    Keywords: AERODYNAMICS
    Type: NASA-TP-1784 , L-13826
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Turbulent jet mixing at high supersonic speeds. (1973)
    In:  Other Sources
    Details
    Publication Date: 2019-06-27
    Description: The results of three related studies of turbulent jet mixing are presented and discussed. The major effort was the collection of mean-flow data at a much higher free stream Mach number than was previously available. The effects of initial swirl in the injectant were found to be minimal. Numerical predictions of the non-swirling experimental case obtained using an eddy viscosity approximation are found to be in reasonable agreement with the data. Lastly, an approximate analysis of the decay of the swirling velocity is developed. This analysis is based upon an eddy viscosity model for transport in the circumferential direction adapted from wing-tip vortex work.
    Keywords: FLUID MECHANICS
    Type: Zeitschrift fuer Flugwissenschaften; 21; May 1973
    Format: text
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