Oblique Impingement of Two Turbulent Plane Free Jets

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概要

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• This paper presents an experimental study on oblique impingement of two turbulent plane free jets. The effects of impinging angle, impinging position and velocity ratio on the deflection angle and characteristics of a jet after impingement were investigated. As a result of this study, it is found that the deflection angle is in good agreement with the result determined from consideration of total momentums of two jets, and turbulent intensity becomes maximum near the impinging point but it approaches that of a free jet as downstream distance increases, and the index of decay law of maximum velocity in similar profile region increases as impinging angle increases.

• 一般社団法人日本機械学会の論文

著者

• Okamoto Tetsushi

  College Of Science And Engineering Aoyama Gakuin University

• ENOKIDA Kouji

  College of Science and Engineering, Aoyama Gakuin University

• Enokida Kouji

  College Of Science And Engineering Aoyama Gakuin University

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• Experimental Investigation on the Boundary-Layer Flow over a Rotating Cone-Cylinder Body in a Uniform Stream
• Oblique Impingement of Two Turbulent Plane Free Jets
• Vector Control of Two-dimensional Turbulent Free Jet by Both-side Flaps
• Vector Control of Two-dimensional Turbulent Free Jet by One-side Flap

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