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XB-70 compressor-noise reduction and propulsion-system performance for choked inlet flow

机译：XB-70压缩机降噪和推进系统性能，适用于阻塞入口流量

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XB-70 compressor noise reduction and propulsion system performance for choked inlet flow

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作者
Putnam, T. W.; Smith, R. H.;
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年度 1970
页码 1-26
总页数 26
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
COMPRESSORS; NOISE REDUCTION; PROPULSION SYSTEM PERFORMANCE; AERODYNAMICS; AIR FLOW; INTAKE SYSTEMS;

机译：压缩机;减少噪音;推进系统性能;空气动力学;空气流动;进口系统;

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专利

1. Cavitation Performance of Cylindrical Choke for Unsteady Flow (2nd Report, Comparison of Difference in inlet Shape of Choke) [J] . Yuri AOYAMA, Naoto WATANABE, Masao YAMAMOTO 日本機械学会論文集. B編 . 1999,第640期

机译：圆柱状扼流圈对非恒定流的气蚀性能（第二份报告，扼流圈入口形状差异的比较）
2. Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking [J] . Hui-jun Tan, Shu Sun, Zhi-long Yin Journal of propulsion and power . 2009,第1期

机译：下游质量流窒息引起的矩形高超声速进气口的振荡流
3. Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking [J] . Hui-jun Tan∗ and Shu Sun†Zhi-long Yin‡ Journal Tables of Contents . 2009,第1期

机译：下游质量流窒息引起的矩形高超声速进气口的振荡流
4. S-DUCT DIFFUSER OFFSET-TO-LENGTH RATIO EFFECT ON AERODYNAMIC PERFORMANCE OF PROPULSION-SYSTEM INLET OF HIGH SPEED AIRCRAFT [C] . Asad Asghar, William D.E. Allan, Marc LaViolette, ASME turbo expo: turbomachinery technical conference and exposition . 2018

机译：S-导管漫射器偏移长度比对高速飞机推进系统进气气动性能的影响
5. The influence of inlet flow distortion on the performance of a centrifugal compressor and the development of an improved inlet using numerical simulations. [D] . Kim, Yunbae. 2001

机译：进口流量畸变对离心压缩机性能的影响以及使用数值模拟改进进口的发展。
6. Role of Sulfate Reduction Versus Methanogenesis in Terminal Carbon Flow in Polluted Intertidal Sediment of Waimea Inlet Nelson New Zealand [O] . Douglas O. Mountfort, Rodney A. Asher 1981

机译：怀梅阿湾受污染的潮间带沉积物中硫酸盐还原与甲烷生成的作用在最终碳流量中的作用新西兰尼尔森
7. Numerical Study on Unstart Phenomena due to Compound Choking of Scramjet Engine Inlets. (1st Report). Compound Choking of Inlets in a Shear Flow. [O] . Tetsuya SATO, Shojiro KAJI 1993

机译：扰乱发动机入口复合窒息原因的数值研究。（第一个报告）。在剪切流中的入口复合窒息。

XB-70 compressor-noise reduction and propulsion-system performance for choked inlet flow

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