A rapid computation of a sequence of transonic flow solutions has to be performed in many areas of aerodynamic technology. The employment of low-cost vector array processors makes the conduction of such calculations economically feasible. However, for a full utilization of the new hardware, the developed algorithms must take advantage of the special characteristics of the vector array processor. The present investigation has the objective to develop an efficient algorithm for solving transonic flow problems governed by mixed partial differential equations on an array processor.
Implicit, nonswitching, vector-oriented algorithm for steady transonic flow
AIAA Journal ; 21
1983-11-01
Sonstige
Keine Angabe
Englisch
Nonswitching Guidance Law for Trajectory Shaping Control
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