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Reston, VA: American Institute of Aeronautics and Astronautics
Erscheinungsjahr
1991
Quelle
Alma/SFX Local Collection
Beschreibungen/Notizen
The hypersonic nonequilibrium flow of air over concave and convex corners is investigated. The description of the flowfield is based on the Euler equations and a chemical model that accounts for the finite rate reactions. An upwind formulation and the related space-marching technique are developed in order to achieve the numerical solution of the fluid dynamical and chemical equations, coupled together. The attention is focused on the effects of nonequilibrium chemistry on fluid dynamics. The transition from the frozen flow condition, just behind the corner, and the equilibrium flow, reached at very large distances far downstream, is characterized by intermediate strong nonequilibrium chemical processes. Such a transition promotes dissipations that, in turn, generate vorticity. (Author)