NASA NTRS · 19910000444
Algorithm Computes Hypersonic Flow Of Air
Abstract
Algorithm simulates three-dimensional hypersonic flow of air or another mixture of gases around blunt body. Accounts for nonequilibrium thermochemical effects via two-temperature mathematical model of molecular excitations and equations for finite-rate chemical reactions. These equations fully coupled to fluid dynamical equations.
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Palmer, Grant. 1991-09-01. Algorithm Computes Hypersonic Flow Of Air. https://ntrs.nasa.gov/citations/19910000444
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