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Effectiveness of a turbojet tubular combustor in screening the turbine from foreign objects

机译：涡轮喷气管式燃烧器在从异物中筛选涡轮机的有效性

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Chiarito, Patrick T;
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年度 1955
页码 1-21
总页数 21
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Experimental Investigations on Axial Temperature Profiles, Liner Wall Temperature Distribution and Exit Gas Temperature Distribution at Different Equivalence Ratios of A Tubular Type Gas Turbine Combustors [J] . Digvijay B. Kulshreshtha, S. A. Channiwala, Saurabh B. Dikshit, International Journal of Applied Engineering Research . 2009,第3期

机译：管式燃气轮机燃烧器不同当量比的轴向温度分布，内衬壁温度分布和出口气体温度分布的实验研究
2. Influence of Combustor Swirl on Endwall Heat Transfer and Film Cooling Effectiveness at the Large Scale Turbine Rig [J] . Holger Werschnik, Jonathan Hilgert, Manuel Wilhelm, Journal of turbomachinery . 2017,第8期

机译：大型涡轮机燃烧室旋流对端壁传热和薄膜冷却效率的影响
3. The effect of effusion holes inclination angle on the adiabatic film cooling effectiveness in a three-sector gas turbine combustor rig with a realistic swirling flow [J] . Andreini Antonio, Becchi Riccardo, Facchini Bruno, International Journal of Thermal Sciences . 2017,第期

机译：具有逼真旋流的三扇区燃气轮机燃烧室中绝热膜冷却效果的倾斜角度的影响
4. COMBUSTOR-TURBINE AEROTHERMAL INTERACTION IN AN AXIAL TURBINE -INFLUENCE OF VARIED INFLOW CONDITIONS ON ENDWALL HEAT TRANSFER AND FILM COOLING EFFECTIVENESS [C] . Holger Werschnik, Jonathan Hilgert, Martin Bruschewski, ASME turbo expo: turbine technical conference and exposition . 2016

机译：轴流透平中的燃气轮机间的热相互作用-各种进水条件对端壁传热和膜冷却效率的影响
5. TURBOJET ENGINE PERFORMANCE AT HIGH TURBINE ENTRY TEMPERATURES WITH TRANSPIRATION COOLED TURBINE BLADING. [D] . GREENWOOD, STUART WILLIAM -1

机译：涡轮增压涡轮叶片在高温下的涡轮发动机性能。
6. Dispersion of Entropy Perturbations Transporting through an Industrial Gas Turbine Combustor [O] . Yu Xia, Ignacio Duran, Aimee S. Morgans, -1

机译：通过工业燃气轮机燃烧室的熵扰动的扩散
7. Soot production in a tubular gas turbine combustor [O] . Zheng Qing-ping 1994

机译：管状燃气轮机燃烧器中的烟尘产生

Effectiveness of a turbojet tubular combustor in screening the turbine from foreign objects

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