科技报告详细信息
Transition Induced by Tandem Rectangular Roughness Elements on a Supersonic Flat Plate
Chou, Amanda ; King, Rudolph A ; Kegerise, Michael A
关键词: TRANSITION FLOW;    SURFACE ROUGHNESS;    SUPERSONIC FLOW;    FLAT PLATES;    LEADING EDGES;    STABILITY;    BOUNDARY LAYER FLOW;    FLOW DISTORTION;    MEAN SQUARE VALUES;    HOT-WIRE FLOWMETERS;    TEMPERATURE PROFILES;    BOUNDARY LAYER THICKNESS;    POWER SPECTRA;    SUPERSONIC WIND TUNNELS;    NASA PROGRAMS;   
RP-ID  :  NF1676L-28571
学科分类:力学,机械学
美国|英语
来源: NASA Technical Reports Server
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【 摘 要 】

The flow behind two rectangular roughness elements with a height approximately 38-41 percent of the boundary layer thickness was examined with a hot-wire probe. The rectangular roughness elements are oriented so that one element was at a plus 45-degree angle relative to the leading edge of the plate. A second roughness element was placed 7.16 millimeters downstream of the first one with either the same orientation relative to the leading edge of the plate, or an opposing orientation of minus 45 degrees from the leading edge. Mean mass-flux and total-temperature profiles of the flow field downstream of the tandem roughness elements were examined for mean-flow distortion. Using streak strength as a measure of mean-flow distortion, the tandem roughness elements had approximately the same amount of distortion, regardless of their relative orientation. Mass-flux fluctuation profiles show that the dominant mode downstream of the tandem roughness elements with the same orientation was similar to that of a single roughness element and centered at a frequency of approximately 55 kilohertz (kHz). The dominant instability downstream of the tandem roughness elements with opposing orientation was centered at a frequency of 65 kHz and grew more slowly than the instabilities behind the single roughness element.

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