Finite-difference method is used to solve system of equations governing hypersonic air wake with nonequilibrium chemistry; laminar and turbulent transports are considered; numerical results for laminar flow are compared with results of integral method; additional calculations for turbulent flow presented show some effects of oxygen-electron attachment process in far wake, and of choice of model of turbulent diffusivity; pertinence to hypersonic and space vehicle re-entry wake phenomena.
Finite-difference calculation of hypersonic wakes
AIAA J
AIAA Journal ; 2 , n 8
1964
7 pages
Article (Journal)
English
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Finite-difference calculation of hypersonic wakes
AIAA | 1964
|FINITE DIFFERENCE CALCULATION OF HYPERSONIC WAKES
AIAA | 1963
|Engineering Index Backfile | 1964
|AIAA | 1964
|NTIS | 1963
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