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Design and performance of a digital electronic normal shock position sensor for mixed- compression inlets

机译：用于混合压缩入口的数字电子正常冲击位置传感器的设计和性能

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摘要

Digital electronic normal shock position sensor for mixed compression inlets

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作者
Cole, G. L.; Crosby, M. J.; Neiner, G. H.;
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年度 1969
页码 1-29
总页数 29
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
DIGITAL SYSTEMS; PRESSURE SENSORS; SHOCK MEASURING INSTRUMENTS; SHOCK WAVE PROFILES; SUPERSONIC INLETS; ANALOG CIRCUITS; COWLINGS; ELECTRONIC EQUIPMENT; FLOW MEASUREMENT; GRAPHS (CHARTS); STATIC PRESSURE; SUPERSONIC TEST APPARATUS; TESTS;

机译：数字系统;压力传感器;冲击测量仪器;冲击波轮廓;超音速入口;模拟电路;整流罩;电子设备;流量测量;图表（图表）;静压力;超级测试设备;试验;

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1. A quasi one-dimensional bleed flow rate model for terminal normal shock stability in mixed compression supersonic inlet [J] . Li Qiushi, Lv Yongzhao, Li Shaobin Proceedings of the Institution of Mechanical Engineers, Part C. Journal of mechanical engineering science . 2014,第14期

机译：混合压缩超声速进气道终端法向冲击稳定性的准一维泄放流模型
2. Canonical Normal Shock Wave/Boundary-Layer Interaction Flows Relevant to External Compression Inlets [J] . Eric Loth, Neil Titchener, Holger Babinsky, AIAA Journal . 2013,第9期

机译：与外部压缩入口有关的规范法向冲击波/边界层相互作用流
3. Model for Predicting Performance of Cooling Fans for Thermal Design of Electronic Equipment (Modeling and Evaluation of Effects from Electronic Enclosure and Inlet Sizes) [J] . Takashi Fukue, Masaru Ishizuka, Shinji Nakagawa, Heat transfer . 2011,第4期

机译：电子设备热设计中的冷却风扇性能预测模型（电子外壳和入口尺寸的影响的建模和评估）
4. Passive Device Flow Control for Normal Shock/Boundary Layer Interactions in External Compression Inlets [C] . Trajaen J. Troia, Amish A. Patel, Dick Crouse, AIAA fluid dynamics conference and exhibit . 2011

机译：用于外部压缩进气口中正常冲击/边界层相互作用的被动设备流量控制
5. Hypersonic mixed-compression inlet shock-induced combustion ramjets. [D] . Alexander, Derrick. 2006

机译：高超声速混合压缩进气口冲击诱发的燃烧冲压发动机。
6. Computational reader design and statistical performance evaluation of an in-silico imaging clinical trial comparing digital breast tomosynthesis with full-field digital mammography [O] . Rongping Zeng, Frank W. Samuelson, Diksha Sharma, 2020

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7. Control of shock wave-boundary layer interactions by bleed in supersonic mixed compression inlets [O] . Fukuda, M. K., Hingst, W. G., Reshotko, E. 1975

机译：通过超声速混合压缩入口中的排气控制冲击波边界层相互作用
8. Design and Performance of a Digital Electronic Normal Shock Position Sensor for Mixed- Compression Inlets [R] . Cole, G. L., Crosby, M. J., Neiner, G. H. 1969

机译：混合压缩进气道数字电子正常冲击位置传感器的设计与性能

Design and performance of a digital electronic normal shock position sensor for mixed- compression inlets

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