AEROTHERMAL TESTS OF A 12. 5 degree CONE AT MACH 6. 7 FOR VARIOUS REYNOLDS NUMBERS, ANGLES OF ATTACK, AND NOSE SHAPES.

被引：0

作者：

Nowak, Robert J. ^{[1
]}

Albertson, Cindy W. ^{[1
]}

Hunt, L.Roane ^{[1
]}

机构：

[1] NASA, Langley Research Cent,, Hampton, VA, USA, NASA, Langley Research Cent, Hampton, VA, USA

来源：

NASA Technical Paper | 1985年

关键词：

AEROTHERMAL DATA BASE - AEROTHERMAL HEATING - CONICAL SHAPES - HIGH-SPEED VEHICLES;

D O I：

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摘要：

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