NASA NTRS · 19870017696
Computational fluid dynamics and aerothermodynamics
Abstract
At the present time the efforts on this project are organized into two areas: the development of an approximate stagnation point solution and approximate flowfield studies which can be used to develop and investigate shock jump, electron temperature, radiation, vibration-dissociation coupling, and chemistry models. Progress in each area is discussed.
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Carlson, Leland A.. 1987-07-01. Computational fluid dynamics and aerothermodynamics. https://ntrs.nasa.gov/citations/19870017696
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