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Understanding Capacity Sensitivity of Cooled Transonic Nozzle Guide Vanes: A Parametric Experimental and Computational Study of the Impact of Trailing Edge Geometry

机译：理解冷却跨音调喷嘴导向叶片的容量敏感性：落后几何撞击的参数实验和计算研究

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Daniel Burdett; Frédéric Goenaga; Thomas Povey;
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1. Understanding Capacity Sensitivity of Cooled Transonic Nozzle Guide Vanes: A Parametric Experimental and Computational Study of the Impact of Trailing Edge Geometry [J] . Daniel Burdett, Frederic Goenaga, Thomas Povey Journal of turbomachinery . 2021,第5期

机译：理解冷却跨音调喷嘴导向叶片的容量敏感性：落后几何撞击的参数实验和计算研究
2. An Experimental Study on Aerodynamic Performance of Turbine Nozzle Guide Vanes With Trailing-Edge Span-Wise Ejection [J] . S. M. Aminossadati, D. J. Mee Journal of turbomachinery . 2013,第3期

机译：后缘跨明智喷射的涡轮喷嘴导流叶片气动性能的实验研究
3. Experimental and computational study of the effect of momentum-flux ratio on high-pressure nozzle guide vane endwall cooling systems [J] . Ornano Francesco, Povey Thomas Journal of turbomachinery . 2017,第12期

机译：动量-流量比对高压喷嘴导叶端壁冷却系统影响的实验和计算研究
4. EXPERIMENTAL STUDY OF THE ENDWALL HEAT TRANSFER OF A TRANSONIC NOZZLE GUIDE VANE WITH UPSTREAM JET PURGE COOLING: PART 2 - EFFECT OF COMBUSTOR-NGV MISALIGNMENT [C] . Ridge A. Sibold, Shuo Mao, Wing F. Ng, ASME Turbo Expo: Turbomachinery Technical Conference and Exposition . 2020

机译：上游喷射吹扫冷却跨声喷嘴导向叶片的端壁传热的实验研究：第2部分 - 燃烧室 - NGV未对准的影响
5. An Experimental and Numerical Investigation of Endwall Aerodynamics and Heat Transfer in a Gas Turbine Nozzle Guide Vane with Slot Film Cooling [D] . Alqefl, Mahmood Hasan. 2016

机译：槽膜冷却燃气轮机喷嘴导向叶片内壁空气动力学和传热的实验性和数值研究
6. Experimental and Computational Studies on the Scattering of an Edge-Guided Wave by a Hidden Crack on a Racecourse Shaped Hole [O] . Benjamin Steven Vien, Louis Raymond Francis Rose, Wing Kong Chiu 2017

机译：赛马场形孔中隐藏裂纹对边引导波散射的实验和计算研究
7. An investigation of the effects of nozzle guide vane trailing edge cooling on rotor heat transfer in a transonic turbine stage [O] . Gleixner Aaron J. (Aaron James) 1992

机译：喷嘴导叶后缘冷却对跨音速涡轮机转子传热影响的研究

Understanding Capacity Sensitivity of Cooled Transonic Nozzle Guide Vanes: A Parametric Experimental and Computational Study of the Impact of Trailing Edge Geometry

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