NASA NTRS · 19890014894
Thermal analysis of a hypersonic wing test structure
Abstract
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.
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Sandlin, Doral R., Swanson, Neil J., Jr.. 1989-04-01. Thermal analysis of a hypersonic wing test structure. https://ntrs.nasa.gov/citations/19890014894
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