Influence of Mach and Reynolds numbers on heat transfer to the leeward surface of a half-cone at hypersonic speed
| Autor: | P. I. Gorenbukh, M. V. Ryzhkova, V. Ya. Borovoi, M. M. Ardasheva |
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| Rok vydání: | 1977 |
| Předmět: |
Fluid Flow and Transfer Processes
Physics Hypersonic speed Angle of attack Mechanical Engineering General Physics and Astronomy Reynolds number Thermodynamics chemistry.chemical_element Mechanics Radius Mach wave Physics::Fluid Dynamics symbols.namesake Mach number chemistry Heat transfer symbols Helium |
| Zdroj: | Fluid Dynamics. 11:736-739 |
| ISSN: | 1573-8507 0015-4628 |
| DOI: | 10.1007/bf01012967 |
| Popis: | Results are given of an investigation of heat transfer on the flat surface of a blunted half-cone, washed at zero angle of attack by a helium flow at high Mach number (up to 23.5). A correlation is given for the experimental data obtained over a wide range of Mach numbers (M∞ = 3−23.5) and Reynolds numbers (Re∞a = 104−3.5·5, wherea is the nose radius). |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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