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Effects of compressor interstage bleed and adjustable inlet guide vanes on compressor stall characteristics of a high-pressure-ratio turbojet engine at altitude

机译：压缩机级间流量和可调入口导叶对高压比涡轮喷气发动机高压侧压缩机失速特性的影响

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Mallett, William E; Groesbeck, Donald E;
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年度 1956
页码 1-37
总页数 37
原文格式 PDF
正文语种 eng
中图分类工业技术;
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4. INFLUENCE OF ADJUSTABLE INLET GUIDE VANES ON THE PERFORMANCE CHARACTERISTICS OF A SHROUDED CENTRIFUGAL COMPRESSOR [C] . Yubao Tian, Yonghong Tang, Zhiheng Wang, ASME turbo expo: turbine technical conference and exposition . 2017

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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

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6. Structural and fluid-dynamic analysis of an axial compressor with adjustable inlet guide vanes [O] . Pachera Matteo 2013

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Effects of compressor interstage bleed and adjustable inlet guide vanes on compressor stall characteristics of a high-pressure-ratio turbojet engine at altitude

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