傾斜した平板に衝突する超音速噴流
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概要
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Flow fields of supersonic axisymmetric jets impinging on an inclined flat plate are experimentally studied by flow visualization with Schlieren method and pressure measurements on the plate. The experiments are carried out for plate inclinations of 22.5° and 30° and for six nozzles with Mach numbers from 1.0 to 4.07. The distances from the nozzle exit to the impingement point of jet on the plate is fixed at 43 mm. The effects of locations of shock cells on the flow state, the pressure distributions on the plate and the force added by the jet normal to the plate are presented.
- 九州大学大学院総合理工学研究科の論文
- 1993-03-01
九州大学大学院総合理工学研究科 | 論文
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