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A DETAILED STUDY OF EFFECTS OF ROW TRENCHED HOLES AT THE COMBUSTOR EXIT ON FILM COOLING EFFECTIVENESS

机译：在薄膜冷却效果对燃烧器出口处的行沟槽孔的影响详细研究

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Ehsan Kianpour; Nor Azwadi Che Sidik;
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1. Computational investigation of film cooling from cylindrical and row trenched cooling holes near the combustor endwall [J] . Ehsan Kianpour, Nor Azwadi Che Sidik Case Studies in Thermal Engineering . 2014,第1期

机译：燃烧室端壁附近圆柱和行开槽冷却孔的薄膜冷却计算研究
2. The Effect of Blowing Ratio on Film Cooling Effectiveness Using Cylindrical and Row Trenched Cooling Holes with Alignment Angle of 90 Degrees [J] . NorAzwadi, EhsanKianpour Mathematical Problems in Engineering: Theory, Methods and Applications . 2014,第a期

机译：使用圆柱和行沟槽冷却孔的吹吹比对薄膜冷却效能的影响，具有90度的对准角度
3. MEASUREMENT OF FILM EFFECTIVENESS FOR CYLINDRICAL AND ROW TRENCHED COOLING HOLES AT DIFFERENT BLOWING RATIOS [J] . Ehsan Kianpour, Nor Azwadi Che Sidik, Iman Golshokouh Numerical Heat Transfer, Part A. Application: An International Journal of Computation and Methodology . 2014,第7a12期

机译：在不同的吹塑比下测量圆柱和行开缝冷却孔的薄膜效率
4. Computational Investigation of Film Cooling from Cylindrical and Row Trenched Cooling Holes near the Combustor End wall [C] . Nor Azwadi Che Sidik, Ehsan Kianpour World Virtual Conference on Advanced Research in Mechanical and Materials Engineering . 2014

机译：燃烧器端壁附近的圆柱形和行沟槽冷却孔的计算研究
5. Numerical and experimental study of trenched hole film cooling with forward and backward injection angles. [D] . Gharat, Kunal M. 2013

机译：带有正向和反向喷射角的沟槽膜冷却的数值和实验研究。
6. Clinical and cost-effectiveness of internal limiting membrane peeling for patients with idiopathic full thickness macular hole. Protocol for a Randomised Controlled Trial: FILMS (Full-thickness macular hole and Internal Limiting Membrane peeling Study) [O] . Noemi Lois, Jennifer Burr, John Norrie, 2008

机译：特发性全层黄斑裂孔内膜剥脱的临床和成本效益。随机对照试验的方案：FILMS（全厚度黄斑裂孔和内部限制膜剥离研究）
7. A Detailed Study of Row-Trenched Holes at the Combustor Exit on Film-Cooling Effectiveness [O] . Ehsan Kianpour, Nor Azwadi Che Sidik 2019

机译：燃烧器出口在薄膜冷却效果上的行挖洞的详细研究

A DETAILED STUDY OF EFFECTS OF ROW TRENCHED HOLES AT THE COMBUSTOR EXIT ON FILM COOLING EFFECTIVENESS

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