Irregular Phenomena of Shock Reflection Transition in a Conventional Supersonic Wind Tunnel
Experimental studies on shock wave reflection in steady flow have been made in a conventional blowdown-type supersonic wind tunnel. The transition from regular to Mach reflection occurs significantly above the von Neumann condition and below the detachment condition, but the repeatability of the tra...
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| Veröffentlicht in: | AIAA journal 2003-06, Vol.41 (6), p.1201-1204 |
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| container_title | AIAA journal |
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| creator | Sudani, Norikazu Sato, Mamoru Karasawa, Toshio Kanda, Hiroshi Toda, Nobuhiro |
| description | Experimental studies on shock wave reflection in steady flow have been made in a conventional blowdown-type supersonic wind tunnel. The transition from regular to Mach reflection occurs significantly above the von Neumann condition and below the detachment condition, but the repeatability of the transition angle is not satisfactorily achieved. It is shown that the type of disturbance in the freestream is very important to the transition phenomena. |
| doi_str_mv | 10.2514/2.2065 |
| format | Article |
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| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Instrumentation for fluid dynamics Physics Shock-wave interactions and shock effects Shock-wave interactions and shockeffects Wind tunnels |
| title | Irregular Phenomena of Shock Reflection Transition in a Conventional Supersonic Wind Tunnel |
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