Artificially Induced Boundary Layer Transition On Blunt Slender Cones Using Distributed Roughness And Spherical Type Tripping Devices At Hypersonic Speeds
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Research directed toward establishing criteria for distributed roughness-type boundary-layer trips on blunt-slender cones has been conducted in the AEDC/VKF at
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Previous investigations of distributed-roughness boundary-layer trips indicated that they are superior to spherical-type trips in that equally effective distrib
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Pages: 1008
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the N
