NASA NACA-RM-E53E28-1953
在马赫数为3.12且雷诺数为2x10(指数6)至14x10(指数6)时,支架干扰对回转体压力分布影响的实验研究
Experimental investigation of the effects of support interference on the pressure distribution of a body of revolution at a Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 14 x 10(exp 6)