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Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed III : velocity-diagram study of two-stage and downstream-stator turbines for engine operation at constant rotative speed

机译：适用于具有高压缩机压力比和低压缩机叶尖速度的涡轮喷气发动机的涡轮机的研究III：用于恒定转速下的发动机运行的两级和下游定子涡轮机的速度图研究

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English, Robert E; Davison, Elmer H;
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年度 1952
页码 1-40
总页数 40
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. A Suitable Load Control Method for Constant Tip Speed Ratio Operation of Stand-Alone Wind Turbine-Generator Systems: Part II: Influence of Measurement Error of Inflow Wind Speed on System Performance [J] . Tetsuya Wakui, Ryohei Yokoyama Wind Engineering . 2008,第2期

机译：独立式风力发电机系统恒定叶尖速比运行的合适负载控制方法：第二部分：流入风速的测量误差对系统性能的影响
2. A Suitable Load Control Method for Constant Tip Speed Ratio Operation of Stand-alone Wind Turbine-Generator Systems (Part Ⅰ: Evaluation of Power Generation Capability and Output Fluctuation) [J] . Tetsuya Wakui, Ryohei Yokoyama Wind Engineering . 2007,第1期

机译：独立风力发电机组恒速比运行的合适负荷控制方法（第一部分：发电能力和输出波动的评估）
3. A Suitable Load Control Method for Constant Tip Speed Ratio Operation of Stand-Alone Wind Turbine-Generator Systems [J] . Wakui Tetsuya, Yokoyama Ryohei Wind Engineering . 2008,第2期

机译：独立风力发电机组恒速比运行的合适负荷控制方法
4. Resonant vibrations resulting from the re-engineering of a constant-speed 2-bladed turbine to a variable-speed 3-bladed turbine [C] . Paul A. Fleming, Alan D. Wright, Lee J. Fingersh, AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2011

机译：将恒速2叶片式涡轮机改造为变速3叶片式涡轮机产生的共振
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. Wind speed reductions by large-scale wind turbine deployments lower turbine efficiencies and set low generation limits [O] . Lee M. Miller, Axel Kleidon 2017

机译：大规模风力涡轮机部署降低了风速，降低了涡轮机效率并设定了较低的发电极限
7. A Study of the Effect of Deterioration on Compressor Surge Margin in Constant-Speed, Single-Shaft Gas Turbine Engines [O] . Robert E. Dundas 1986

机译：恒速，单轴燃气涡轮发动机压缩机喘振裕度劣化效果的研究

Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed III : velocity-diagram study of two-stage and downstream-stator turbines for engine operation at constant rotative speed

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