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    Thermal analysis of a hypersonic wing test structure (1989)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The three-dimensional finite element modeling techniques developed for the thermal analysis of a hypersonic wing test structure (HWTS) are described. The computed results are compared to measured test data. In addition, the results of a NASA two-dimensional parameter finite difference local thermal model and the results of a contractor two-dimensional lumped parameter finite difference local thermal model will be presented.
    Keywords: AERODYNAMICS
    Type: NASA-CR-185319 , NAS 1.26:185319
    Format: application/pdf
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