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Project SQUID: Stability of the Laminar Boundary Layer with Injection of Cool Gas at the Wall

机译：项目sQUID：与长城酷气的注射液层流边界层的稳定性

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作者
Lees, L.;
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年度 1948
页码 p.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
Laminar boundary layer; Stability; Flat plate models; Fluid mechanics; Fluid flow; Compressible flow; Fluid dynamics; Equations;

机译：层流边界层;稳定性;平板模式;流体力学;流体流动;可压缩流动;流体动力学;方程;
入库时间 2022-08-29 10:03:38

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专利

1. Effect of wall-cooling on Mack-mode instability in high speed fiat-plate boundary layers [J] . Shaolong ZHANG, Jianxin LIU, Jisheng LUO 应用数学和力学（英文版） . 2016,第009期

机译：壁冷却对高速平板边界层中Mack模式不稳定性的影响
2. STABILITY CHARACTERISTICS OF LAMINAR BOUNDARY LAYERS OVER COMPLIANT WALLS [J] . 力学学报：英文版 . 1989,第002期

机译：柔顺墙壁层边界层的稳定性特性
3. Nonuniform multiple slot injection (suction) or wall enthalphy into a steady compressible laminar boundary layer [J] . Roy S. Acta Mechanica . 2000,第1a2期

机译：非均匀的多缝注入（吸力）或壁焓进入稳定的可压缩层流边界层
4. LAMINAR FLOW CONTROL OF A HIGH-SPEED BOUNDARY LAYER BY LOCALIZED WALL HEATING OR COOLING [C] . Fedorov A.V., Soudakov V.G., Egorov I.V., Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：局部壁面加热或冷却控制高速边界层的层流
5. An experimental investigation of wall cooling effects on hypersonic boundary layer stability in a quiet wind tunnel. [D] . Blanchard, Alan Edward. 1995

机译：在安静的风洞中壁冷却对高超音速边界层稳定性影响的实验研究。
6. Boundary layer control by a fish: Unsteady laminar boundary layers of rainbow trout swimming in turbulent flows [O] . Kazutaka Yanase, Pentti Saarenrinne 2016

机译：鱼的边界层控制：虹鳟在湍流中游荡的不稳定层流边界层
7. Prediction of heat transfer from laminar boundary layers, with emphasis on large free- stream velocity gradients and highly cooled walls [O] . Witte A. B., Back L. H. 1965

机译：从层流边界层传热的预测，重点是大的自由流速度梯度和高度冷却的壁
8. STABILITY OF LAMINAR BOUNDARY LAYER NEAR A STAGNATION POINT OVER AN IMPERMEABLE WALL AND A WALL COOLED BY NORMAL FLUID INJECTION [R] . Morris Morduchow, Richard G. Grape, Richard P. Shaw 1957

机译：通过正常流体注入冷却的墙壁和墙壁上的一个平行点附近的层流边界层的稳定性

Project SQUID: Stability of the Laminar Boundary Layer with Injection of Cool Gas at the Wall

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