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Preliminary evaluation of a perforated sheet film-cooled linear in a turbojet combustor

机译：在涡轮喷气发动机燃烧室中对薄膜冷却的多孔板进行初步评估

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摘要

Performance of turbojet combustors with perforated sheet film-cooled liners compared with stepped continuous-slot film-cooled liners

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作者
Fear, J. S.;
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年度 1969
页码 1-18
总页数 18
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
COMBUSTION CHAMBERS; COMBUSTION EFFICIENCY; FILM COOLING; LININGS; TURBOJET ENGINES; INLET FLOW; JET ENGINE FUELS; OUTLETS; PRESSURE DROP; SLOTS; TEMPERATURE PROFILES;

机译：燃烧室;燃烧效率;电影冷却;衬片涡轮发动机;进水流量;喷气发动机燃料; OUTLETs;压力下降;插槽;温度曲线;

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2. Gas Turbine Engine Durability Impacts of High Fuel-Air Ratio Combustors: Near Wall Reaction Effects on Film-Cooled Backward-Facing Step Heat Transfer [J] . David W. Milanes, Daniel R. Kirk, Krzysztof J. Fidkowski, Journal of Engineering for Gas Turbines and Power . 2006,第2期

机译：燃气/空燃比高的燃烧室对燃气轮机耐久性的影响：薄膜冷却后向阶梯式换热的近壁反应效应
3. Gas Turbine Engine Durability Impacts of High Fuel-Air Ratio Combustors―Part Ⅱ: Near-Wall Reaction Effects on Film-Cooled Heat Transfer [J] . D. R. Kirk, G. R. Guenette, S. P. Lukachko, Journal of Engineering for Gas Turbines and Power . 2003,第3期

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4. DESIGN OF A NON-REACTIVE WARM RIG WITH REAL LEAN-PREMIX COMBUSTOR SWIRLERS AND FILM-COOLED FIRST STAGE NOZZLES [C] . Simone Cubeda, Tommaso Bacci, Lorenzo Mazzei, ASME Turbo Expo: Turbomachinery Technical Conference and Exposition . 2020

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7. Design, Manufacturing and Rig Test of a Small Turbojet Engine Combustor with Airblast Atomizer [O] . Ahmet Topal, Onder Turan, Sıtkı Uslu 2015

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Preliminary evaluation of a perforated sheet film-cooled linear in a turbojet combustor

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