Zobrazeno 1 - 10 of 25 pro vyhledávání: '"E. R. van Driest"'
1
Turbulent Boundary Layer in Compressible Fluids
Autor: E. R. Van Driest
Publikováno v: Journal of Spacecraft and Rockets. 40:1012-1028
The continuity, momentum, and energy differential equations for turbulent flow of a compressible fluid are derived, and the apparent turbulent stresses and dissipation function are identified. A general formula for skin friction, including heat trans
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1117ad655b302692874477f630fb36ca
https://doi.org/10.2514/2.7048
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4
Streamlines for the Subsonic Flow of a Compressible Fluid Past a Sphere
Autor: E. R. Van Driest
Publikováno v: Journal of Applied Physics. 18:194-198
The second approximation to the velocity potential for the irrotational flow of a compressible fluid past a sphere, derived independently by Tamada and Kaplan, is used to calculate the subsonic streamlines for the flow of air at a Mach number of 0.5
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::91106403dabb337cbeca322146b7efc6
https://doi.org/10.1063/1.1697602
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7
Calculation of the Stability of the Laminar Boundary Layer in a Compressible Fluid on a Flat Plate with Heat Transfer
Autor: E. R. Van Driest
Publikováno v: Journal of the Aeronautical Sciences. 19:801-812
The amount of cooling required to stabilize completely the laminar boundary layer on a flat plate at supersonic speeds with zero pressure gradient is calculated using the Lees-Lin theory. I t is found that, above about Mach Number 9, it is impossible
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::24f71333f9a41f724e9bcdbc1cee0938
https://doi.org/10.2514/8.2492
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8
Problems of High-Speed Hydrodynamics
Autor: E. R. van Driest
Publikováno v: Journal of Engineering for Industry. 91:1-12
A hard look at the problems provoked by the quest for higher speeds of underwater craft shows that they can indeed be solved in a practical manner using the knowledge and principles derived in the evolution of the science of high-speed aerodynamics.
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::376e0ab7e9b2be3dd0a382dde66a544d
https://doi.org/10.1115/1.3591517
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9
Boundary-Layer Transition at Supersonic Speeds - Three-Dimensional Roughness Effects (Spheres)
Autor: E. R. Van Driest, C. B. Blumer
Publikováno v: Journal of the Aerospace Sciences. 29:909-916
Experiments carried out in the 12-inch supersonic wind tunnel to investigate the effect of three dimensional roughness elements (spheres) on boundary-layer transition on a 10-degree (apex angle) cone without heat transfer are described. The local Mac
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::48a8aab9dfa867625ca16f7c5db56b1a
https://doi.org/10.2514/8.9658
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