Experimental Study of Heat Transfer in a Critical Point of Sphere in Hypersonic Low-Density Flow,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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In an experimental study of heat transfer at the critical point of a sphere the possibility is confirmed of using underexpanded nozzles in hypersonic wind tunnels for radiation of the flow about the models over a wide range of Reynolds numbers. Experiments were carried out in a hypersonic shock tube with numbers M 32.
- Fluid Mechanics