NASA Technical Note PDF Download
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Author:
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Category :
Languages : en
Pages : 534
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Author:
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ISBN:
Category :
Languages : en
Pages : 534
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Author: United States. Wright Air Development Division
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Category : Aeronautics
Languages : en
Pages : 1502
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Author: Michael H. Bertram
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Category : Fluid mechanics
Languages : en
Pages : 58
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Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 860
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author: Richard M. Wood
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 104
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Category : Government publications
Languages : en
Pages : 1274
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Author: United States. Superintendent of Documents
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Category : Government publications
Languages : en
Pages : 1284
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Author: J. Don Gray
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Category : .
Languages : en
Pages : 128
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The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced by a 9.5-degree ramp were investigated at Mach numbers from 3 through 6 measuring the longitudinal surface pressure and heat-transfer rate distributions, as well as the flow-field pressures, at several longitudinal stations. Reynolds number based on flat-plate length was varied from 0.25 to 1.0 million. The trend in the change in interaction length with Reynolds number increase indicated laminar reattachment at all test Reynolds numbers at M = 6 and transitional at the two higher Reynolds numbers at M = 3.
Author: United States. National Aeronautics and Space Administration
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ISBN:
Category :
Languages : en
Pages : 208
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