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  • 1
    Publication Date: 2019-07-13
    Description: Report discusses numerical simulations of flow of air about integrated space shuttle (complete space shuttle assembly including orbiter, solid rocket boosters, and external tank) in ascent. Updated version of report described in "Computed Flow About The Integrated Space Shuttle" (ARC-12685). Goal of studies to improve understanding of, and ability to predict how integrated space shuttle performs during both nominal and aborted ascent under various conditions.
    Keywords: MECHANICS
    Type: ARC-13163 , NASA Tech Briefs (ISSN 0145-319X); 20; 4; P. 80
    Format: text
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  • 2
    Publication Date: 2019-07-12
    Description: Report discusses research on dual-potential formulation of Navier-Stokes equations. Purpose of study to extend capability of dual-potential method to computation of unsteady flows of viscous, compressible fluids.
    Keywords: MECHANICS
    Type: ARC-12720 , NASA Tech Briefs (ISSN 0145-319X); 16; 2; P. 83
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  • 3
    Publication Date: 2019-07-12
    Description: Report discusses numerical simulations of flow of air about integrated Space Shuttle in ascent. Goal: to improve understanding of, and ability to predict, how integrated Space Shuttle will perform during both nominal and aborted ascent under various conditions. These and other numerical simulations intended both to supplement wind-tunnel data, corrupted to some extent by scaling and wall-interference effects, and to compensate for scarcity of valid flight data.
    Keywords: MECHANICS
    Type: ARC-12685 , NASA Tech Briefs (ISSN 0145-319X); 15; 10; P. 80
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  • 4
    Publication Date: 2019-07-12
    Description: Report describes some experiences in numerical simulation of compressible, viscous flows by finite-difference approximations of Navier-Stokes equations. Focuses upon viscous/inviscid-interaction approach, in which flow mathematically modeled with interacting zones, within each of which different model of viscous or inviscid flow applies. Reduces task of computation by taking advantage of simpler models and coarser grids in some of zones.
    Keywords: MECHANICS
    Type: ARC-12115 , NASA Tech Briefs (ISSN 0145-319X); 15; 4; P. 85
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  • 5
    Publication Date: 2019-07-12
    Description: Perturbation technique yields accurate flow solutions using as few as one-fourth number of grid points required by finite-difference methods. Technique originally developed to solve Euler equations of two-dimensional, steady, inviscid transonic flow about airfoils, applicable to arbitrary equation sets and higher dimensions. New perturbations scheme used in design cycle where potential solutions generated routinely; Euler perturbation method used in second-cut analysis. Method also used to couple other equation sets.
    Keywords: MECHANICS
    Type: ARC-11550 , NASA Tech Briefs (ISSN 0145-319X); 10; 5; P. 98
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