Using normalized coordinates, equations governing inviscid, isentropic expansions of perfect gases through convergent-divergent nozzles can be solved as inverse power expansions in normalized throat wall radius of curvature; solution for complete nozzle flowfield is obtained in form of perturbation about one-dimensional flowfield; first- and second-order corrections have been worked out; solutions are obtained for choked and unchoked nozzle flows as well as for multistream nozzle expansion such as characteristically occurs in barrier cooled rocket engine. (03272)
Convergent-divergent nozzle flows
AIAA J
AIAA Journal ; 6 , n 9
1968
7 pages
Article (Journal)
English
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Convergent-divergent nozzle flows.
AIAA | 1968
|Convergent-divergent nozzle flows.
NTRS | 1968
|Convergent-divergent nozzle flows
NTRS | 1966
|