Flow visualization; High temperature gases; Intake systems; V/stol aircraft; Wind tunnel tests; Exhaust gases; Data bases; Nozzle flow; Scale models; Supersonic speed; Thrust;
机译:美国国家航空航天局刘易斯9英寸乘15英尺低速风洞测得的背景噪声水平
机译:带有流动可视化功能的NASA Lewis 9-×15英尺低速风洞中先进STOVL概念的热气吸入测试
机译:在Nasa Lewis 9- 15英尺低速风洞中进行热气体摄取测试,采用先进的sTOVL概念,具有流动可视化