injurious
发表于 2025-3-21 16:55:21
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凶兆
发表于 2025-3-21 22:22:20
and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD
国家明智
发表于 2025-3-22 00:40:20
Experiments on Shock-Wave/Boundary-Layer Interactions Produced by Two-Dimensional Ramps and Three-Diure to the recovery temperature of the real flight the model could be cooled by circulation of liquid nitrogen. The flow produced have been investigated by means of schlieren photographs, surface flow visualizations, thermosensitive painting, surface heat transfer and surface pressure measurements.
凶残
发表于 2025-3-22 06:48:40
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chuckle
发表于 2025-3-22 11:05:25
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阴谋
发表于 2025-3-22 13:30:39
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jeopardize
发表于 2025-3-22 17:27:44
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CHAR
发表于 2025-3-23 00:44:13
https://doi.org/10.1007/978-3-642-76527-8dynamics; equilibrium; experiment; finite element method; geometry; laminar flow; numerical analysis; phase
镇痛剂
发表于 2025-3-23 04:56:29
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Mammal
发表于 2025-3-23 08:51:07
Hypersonic Boundary Layer and Base Flow Workshop Test Problems 1 and 2This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the “Workshop on Hypersonic Flows for Reentry Problems, Part I”. These are defined as follows: