Low-Reynolds-Number Effects on Hypersonic Blunt-Body Shock Standoff
| Autor: | George R. Inger |
|---|---|
| Rok vydání: | 2004 |
| Předmět: |
Fluid Flow and Transfer Processes
Physics Hypersonic speed Astrophysics::High Energy Astrophysical Phenomena Mechanical Engineering Aerospace Engineering Reynolds number Mechanics Vorticity Condensed Matter Physics Moving shock Shock (mechanics) symbols.namesake Classical mechanics Space and Planetary Science symbols Oblique shock Bow shock (aerodynamics) Shock tube |
| Zdroj: | Journal of Thermophysics and Heat Transfer. 18:108-113 |
| ISSN: | 1533-6808 0887-8722 |
| DOI: | 10.2514/1.9157 |
| Popis: | An approximate analytical theory of the onset of viscous effects on hypersonic-body nose shock standoff distance is developed. Boundary-layer displacement, shock layer vorticity, and longitudinal curvature effects are all included, as are the influence of both shock layer density ratio and arbitrary body surface temperature |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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