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Inlet-air distortion effects on stall, surge, and acceleration margin of a turbojet engine equipped with variable compressor inlet guide vanes

机译：入口 - 空气变形对配备有可变压缩机入口导叶的涡轮喷气发动机的失速，喘振和加速裕度的影响

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Harry, David P , III; Lubick, Robert J;
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年度 1955
页码 1-51
总页数 51
原文格式 PDF
正文语种 eng
中图分类工业技术;
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专利

1. Introduction of Circumferentially Nonuniform Variable Guide Vanes in the Inlet Plenum of a Centrifugal Compressor for Minimum Losses and Flow Distortion [J] . Ismail Sezal, Nan Chen, Christian Aalburg, Journal of turbomachinery . 2016,第9期

机译：引入周向非均匀可变导叶在离心式压缩机的入口进气口中，以最大程度地减少损失和流量畸变
2. The effects of radial inlet with splitters on the performance of variable inlet guide vanes in a centrifugal compressor stage [J] . J Tan, X Wang, D Qi, Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science . 2011,第9期

机译：带有分离器的径向进气口对离心压缩机级可变进气口导向叶片性能的影响
3. The effects of radial inlet with splitters on the performance of variable inlet guide vanes in a centrifugal compressor stage [J] . J. Tan, X. Wang, D. Qi, Proceedings of the Institution of Mechanical Engineers, Part C. Journal of mechanical engineering science . 2011,第9期

机译：带有分离器的径向进气口对离心压缩机级可变进气口导向叶片性能的影响
4. An experimental study of stall in two axial compressor stages with variable inlet guide and stator vanes [C] . V Cyrus European conference on turbomachinery . 1999

机译：带有可变入口导向和定子叶片的轴向压缩机两级失速的实验研究
5. Experimental investigation of vane clocking effects on stall performance and unsteady vane boundary layer development in a multistage compressor. [D] . Smith, Natalie Rochelle. 2011

机译：叶片计时对多级压缩机失速性能和不稳定边界层发展的实验研究。
6. Enhanced compressor distortion tolerance using asymmetric inlet guide vane stagger [O] . Schulmeyer Andreas 1989

机译：使用不对称入口导叶交错增强压缩机变形容差

Inlet-air distortion effects on stall, surge, and acceleration margin of a turbojet engine equipped with variable compressor inlet guide vanes

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