Paper
10 February 2009 Flow establishment behind blunt bodies at hypersonic speeds in a shock tunnel
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Proceedings Volume 7126, 28th International Congress on High-Speed Imaging and Photonics; 71260I (2009) https://doi.org/10.1117/12.822751
Event: 28th International Congress on High-Speed Imaging and Photonics, 2008, Canberra, Australia
Abstract
An investigation of flow establishment behind two blunt bodies, a circular cylinder and a 45° half-angle blunted-cone was conducted. Unlike previous studies which relied solely on surface measurements, the present study combines these with unique high-speed visualisation to image the establishment of the flow structure in the base region. Test flows were generated using a free-piston shock tunnel at a nominal Mach number of 10. The freestream unit Reynolds numbers considered were 3.02x105/m and 1.17x106/m at total enthalpies of 13.35MJ/kg and 3.94MJ/kg, respectively. In general, the experiments showed that it takes longer to establish steady heat flux than pressure. The circular cylinder data showed that the near wake had a slight Reynolds number effect, where the size of the near wake was smaller for the high enthalpy flow condition. The blunted-cone data showed that the heat flux and pressures reached steady states in the near wake at similar times for both high and low enthalpy conditions.
© (2009) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
G. Park, R. Hruschka, S. L. Gai, and A. J. Neely "Flow establishment behind blunt bodies at hypersonic speeds in a shock tunnel", Proc. SPIE 7126, 28th International Congress on High-Speed Imaging and Photonics, 71260I (10 February 2009); https://doi.org/10.1117/12.822751
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KEYWORDS
Heat flux

Sensors

Thin films

Image visualization

Calibration

Image enhancement

Neck

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