Strong Explosion Model of Gas Dynamics of a Rocket Plume in Upper Atmosphere
An expansion of a rocket exhaust plume in the direction perpendicular to the rocket motion is studied. A comparison is made of the numerical calculations with a self-similar approximation for a strong cylindrically symmetric explosion. It is shown that if a rocket velocity, V∞, is high enough and exceeds the sum of an exhaust gas velocity, Ve and a sound velocity, Vs, (V∞>Ve+Vs), there might be formed, for a short time, a gas-dynamic hole around a rocket flight trajectory in the upper atmosphere where the plume gas concentration is less than the ambient gas concentration at a given altitude. The density and temperature profiles of the transversal plume expansion are calculated.
MOLCHANOV Alexander PLATOV Yulii
Lebedev Physical Institute of the RAS,Moscow 117924,Leninsky pr.53,Russia Pushkov Institute of Terrestrial Magnetism,Ionosphere and RadioVawes Propagation RAS,Troitsk,Moscow
国际会议
2011 International Autumn Seminar on Propellants,Explosives and Pyrotechnics(2011国际推进剂、炸药、烟火技术秋季研讨会)
南京
英文
821-824
2011-09-20(万方平台首次上网日期,不代表论文的发表时间)