| Autor: | V. I. Plyashechnik, V. A. Bashkin, Ivan Vladimirovich Egorov, D. V. Ivanov |
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| Rok vydání: | 2003 |
| Předmět: |
Fluid Flow and Transfer Processes
Physics Mechanical Engineering General Physics and Astronomy Reynolds number Aerodynamics Mechanics Perfect gas Numerical integration Physics::Fluid Dynamics symbols.namesake Classical mechanics symbols Supersonic speed Navier–Stokes equations Choked flow Wind tunnel |
| Zdroj: | Fluid Dynamics. 38:105-114 |
| ISSN: | 0015-4628 |
| DOI: | 10.1023/a:1023347314362 |
| Popis: | Supersonic M∞≈4 flow past a slender sharp circular cone with semi-vertex angle θc=4° at small and moderate angles of attack is investigated both theoretically and experimentally over the Reynolds number range from 1.69·104 to 13.62·106. The theoretical analysis is based on the numerical integration of the three-dimensional Navier-Stokes and Reynolds equations, while the experimental study was carried out in a wind tunnel of the Central Aerohydrodynamics Institute (TsAGI). The calculated and measured integral characteristics of the cone are compared. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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