Numerical analyses of the transonic nozzle inviscid flow and supersonic jet impingement on a jetTAB are presented.
采用数值分析方法分析了跨声速喷管无粘流动和超声速射流对挡流板的冲击流场。
2
By measuring the thrust and lateral forces of solid rocket motor during firing conditions, the thrust vector control performances of jetTAB TVC and movable nozzle TVC were studied.