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  • 1
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    Internal hypersonic flow (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-06-27
    Description: An approach for studying hypersonic internal flow with the aid of a thin-shock-layer approximation is discussed, giving attention to a comparison of thin-shock-layer results with the data obtained on the basis of the imposition theory or a finite-difference integration of the Euler equations. Relations in the case of strong interaction are considered together with questions of pressure distribution and aspects of the boundary-layer solution.
    Keywords: AERODYNAMICS
    Type: ASME PAPER 73-APM-DD , AD-A000739 , AFOSR-74-1643TR
    Format: text
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  • 2
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    Viscous flow over spinning cones at angle of attack. (1973)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: A numerical finite-difference method is developed for evaluating the Magnus coefficients on spinning cones in laminar flow. The merged layer, the strong interaction region, and the downstream boundary layer are all considered. The numerical method is a predictor-corrector scheme developed for three-dimensional flows with or without crossflow diffusion. This method is particularly useful in problems in which a symmetry plane does not exist. Several contributions to the Magnus force and moments are considered. These include asymmetries in displacement thickness, centrifugal force and crossflow shear, and the effects of crossflow separation and vortex formation. Comparisons are made with experimental data and other analyses.
    Keywords: AERODYNAMICS
    Type: Computational Fluid Dynamics Conference; Jul 19, 1973 - Jul 20, 1973; Palm Springs, CA
    Format: text
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    NASA TECHNICAL REPORTS
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