Effect of Rib Turbulator Orientation on the Discharge Coefficient of Suction Hole in the Internal Passage
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Effect of Rib Turbulator Orientation on the Discharge Coefficient of Suction Hole in the Internal Passage
Vol. 18, Issue 2, (2003)
作者机构:
西北工业大学航空动力与热力工程系,陕西,西安,710072
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Published:2003
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QIU Yun, ZHU Hui-ren, NI Meng, et al. Effect of Rib Turbulator Orientation on the Discharge Coefficient of Suction Hole in the Internal Passage[J]. 2003, 18(2).
DOI:
QIU Yun, ZHU Hui-ren, NI Meng, et al. Effect of Rib Turbulator Orientation on the Discharge Coefficient of Suction Hole in the Internal Passage[J]. 2003, 18(2).DOI:
Effect of Rib Turbulator Orientation on the Discharge Coefficient of Suction Hole in the Internal Passage
Measurement of suction holes' discharge coefficients Cd in an internal passage with rib turbulators and suction holes are presented.The internal passage is a rectangular channel with two opposite ribbed walls
the aspect ratio is 0.5
and the rib turbulators are arranged in a staggered way on the two wider walls.The cylindrical suction holes are 45° inclined and perpendicularly oriented
they are placed on one ribbed wall.Tests were run by varying rib tubulators' angles as 45°
60°
90° and 120°
with Reynolds numbers Re changing from 40000 to 80000 and suction ratios (SR) changing from 0.30 to 0.60.Influences of rib tuburlators angles
Reynolds number and suction ratio on Cdare studied. Results indicate:(1) Cdincreases a little along the internal passage;(2) increasing rib turbulator's angle leads to higher Cd
and the maximum Cdis obtained when the rib angle is 120°;(3) varying suction ratio contributes no remarkable effect on changing discharge coefficients;(4) Reynolds number also has no obvious influence on discharge coefficients.