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Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds

机译：在高超音速下，利用层状边界层将热传递到钝头形状

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作者
Reller, John O , Jr;
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年度 1957
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Laminar-turbulent transition in supersonic boundary layers with surface heat transfer: A numerical study [J] . Shadloo M. S., Hadjadj A. Numerical Heat Transfer, Part A. Application: An International Journal of Computation and Methodology . 2017,第1a6期

机译：具有表面传热的超音速边界层中的层压湍流转变：数值研究
2. Investigation of Laminar-Turbulent Transition in Supersonic Boundary Layers in an Axisymmetric Aerophysical Flight Complex and in a Model in a Wind Tunnel in the Presence of Heat Transfer and Suction of Air [J] . A. I. Leontiev, A. M. Pavlyuchenko High temperature: English translation of teplofizika vysokikh temperatur . 2008,第4期

机译：存在传热和空气吸入的轴对称航空物理飞行复合体和风洞模型中超音速边界层的层流湍流过渡研究
3. Laminar-to-turbulent transition in supersonic boundary layer: Effects of initial perturbation and wall heat transfer [J] . Sharma S., Shadloo M. S., Hadjadj A. Numerical Heat Transfer, Part A. Application: An International Journal of Computation and Methodology . 2018,第7a12期

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4. Flow Structure and Heat Transfer Characterization of a Blunt-Fin-Induced Shock-Wave/Laminar Boundary-Layer Interaction [C] . Jorge Castro Maldonado, James A. S. Thrcadgill, Stuart A. Craig, AIAA SciTech Forum and Exposition . 2021

机译：钝化冲击波/层边界层相互作用的流动结构和传热表征
5. Flow Structure and Heat Transfer Characterization of a Blunt-Fin-Induced Shock-Wave/Laminar Boundary-Layer Interaction [D] . Castro Maldonado, Jorge Alberto. 2021

机译：钝化冲击波/层边界层相互作用的流动结构和传热表征
6. Boundary layer control by a fish: Unsteady laminar boundary layers of rainbow trout swimming in turbulent flows [O] . Kazutaka Yanase, Pentti Saarenrinne 2016

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7. Laminar boundary layer separation and near wake flow for a smooth blunt body at supersonic and hypersonic speeds [O] . Grange Jean-Marie 1966

机译：层流边界层分离和近尾流在超音速和高超音速下为平滑钝体提供

Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds

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