NASA NTRS · 19930047955
Computational flowfields for static testing of powered hypersonic aftbody models
Abstract
Two-dimensional CFD analyses are presented related to the ground testing of hypersonic, air-breathing models which feature scramjet exhaust flow simulation. CFD analysis indicates that it is possible to test aftbody powered hypersonic airbreather configurations in a static, pumped-down environment to obtain aftbody aerodynamic performance data.
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Huebner, Lawrence D.. 1993-02-01. Computational flowfields for static testing of powered hypersonic aftbody models. https://ntrs.nasa.gov/citations/19930047955
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