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Effect of bleed-system back pressure and porous area on the performance of an axisymmetric mixed-compression inlet at Mach 2.50

机译：渗流系统背压和多孔面积对机床2.50处轴对称混合压缩入口性能的影响

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摘要

Performance tests of wind tunnel model inlet for bleed system back pressure and porous area effect of axisymmetric compression

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作者
Cubbison, R. W.; Sanders, B. W.;
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年度 1968
页码 1-33
总页数 33
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
INLET FLOW; PERFORMANCE TESTS; POROSITY; PRESSURE REDUCTION; AXISYMMETRIC FLOW; COMPRESSING; GRAPHS (CHARTS); TABLES (DATA); WIND TUNNEL MODELS;

机译：进水流量;性能测试;孔隙度;减压;轴对称流动;压缩;图表（图表）;表（数据）;风洞模型;

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专利

1. Forced Oscillations in a Mixed-Compression Inlet at Mach 3.5 for Pulse Detonation Engine Systems [J] . Venkata Nori, Nelson Lerma, Jonas Gustavsson, Journal of Fluids Engineering: Transactions of the ASME . 2006,第3期

机译：脉冲爆震发动机系统的混合压缩进气中的强迫振荡（马赫数为3.5）
2. Modeling the Effect of Stability Bleed on Back-Pressure in Mixed-Compression Supersonic Inlets [J] . Lv Yongzhao, Li Qiushi, Li Shaobin Journal of Fluids Engineering: Transactions of the ASME . 2015,第12期

机译：模拟混合压缩超音速进气口中流血稳定性对背压的影响
3. Experimental Investigation of a Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Sweep-forward Highlight and Bleed Slot in an Inverted 'X'-type Layout [J] . Wan Dawei, Guo Rongwei Chinese journal of aeronautics . 2007,第4期

机译：固定几何二维混合压缩超音速进气口，前掠高光和排气槽呈倒“ X”型布局
4. CFD SIMULATIONS OF AN AXISYMMETRIC MIXED-COMPRESSION INLET WITH BLEED THROUGH DISCRETE HOLES [C] . David B. Benson, Tom I-P. Shih, David O. Davis Fluids Engineering Conference . 2003

机译：带通孔的轴对称对称压缩进气孔的CFD模拟
5. An investigation of unsteady pressure and temperature characteristics due to shock-boundary layer interactions in a mach 6 axisymmetric flowfield [D] . Flanagan, Michael John, Jr. 1991

机译：马赫6轴对称流场中由于冲击边界层相互作用而引起的非稳态压力和温度特性的研究
6. Correction: Modeling and Analysis of Unsteady Axisymmetric Squeezing Fluid Flow through Porous Medium Channel with Slip Boundary [O] . -1

机译：校正：非恒定轴对称挤压流体通过带滑动边界的多孔介质通道的建模与分析
7. Tory II-C performance as a function of flight mach number and inlet pressure recovery [O] . Moyer, J. H. 1963

机译：Tory II-C性能是飞行马赫数和入口压力恢复的函数
8. Effect of Bleed-System Back Pressure and Porous Area on the Performance of an Axisymmetric Mixed-Compression Inlet at Mach 2.50 [R] . Cubbison, R. W., Sanders, B. W. 1968

机译：排气系统背压和孔隙面积对机床2.50轴对称混合压缩进气道性能的影响

Effect of bleed-system back pressure and porous area on the performance of an axisymmetric mixed-compression inlet at Mach 2.50

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