At the initial stage ofvehicle design, the contributed engineering approach provides a powerful backing for prediction jet aerodynamiccharacteristics.
为飞行器设计初期的喷流气动特性计算提供了一种适用的计算手段。
2
In this paper aerodynamiccharacteristicsof maneuvering reentry vehicle of cruciform configuration and bifurcate configuration are compared by means of the wind tunnel test results.
利用典型状态的风洞试验结果对十字布局与叉字布局再入机动飞行器的气动特性进行了分析与比较。
3
Aerodynamiccharacteristics and wind pressure distribution ofvehicle-bridge coupled system is stud-ied based on numerical simulation by computational fluid dynamic method.