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Dynamic analysis of XB-70-1 inlet pressure fluctuations during takeoff and prior to a compressor stall at Mach 2.5

机译：XB-70-1入口压力波动的动态分析，在压缩机失速为2.5马赫时起飞前

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Inlet pressure fluctuation in XB-70 aircraft during takeoff and prior to compressor stall at Mach 2.5

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作者
Martin, R. A.;
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年度 1970
页码 1-58
总页数 58
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
B-70 AIRCRAFT; DYNAMIC PRESSURE; ENGINE INLETS; PRESSURE GRADIENTS; BOUNDARY LAYER STABILITY; SUPERSONIC COMPRESSORS;

机译：B-70飞机;动态压力;发动机进气;压力梯度;边界层稳定性;超音速压缩机;

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2. URANS analysis of the effect of realistic inlet distortions on the stall inception of a centrifugal compressor [J] . Vagnoli S., Verstraete T. Computers & Fluids . 2015,第Null期

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3. Numerical Simulation of Aerodynamic Instabilities in a Multistage High-Speed High-Pressure Compressor on Its Test-Rig-Part Ⅰ: Rotating Stall [J] . Flore Crevel, Nicolas Gourdain, Stephane Moreau Journal of turbomachinery . 2014,第10期

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5. Mean pressure measurements of micro-vortex generator at Mach 2.5. [D] . Shih, Yusi. 2010

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8. Dynamic Analysis of Xb-70-1 Inlet Pressure Fluctuations During Takeoff and Prior to a Compressor Stall at Mach 2.5 [R] . Martin, R. A. 1970

机译：Xb-70-1进气道压力波动的动态分析在起飞时和2.5马赫压缩机失速之前

Dynamic analysis of XB-70-1 inlet pressure fluctuations during takeoff and prior to a compressor stall at Mach 2.5

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