Boundary Layer Transition on a Hypersonic Forebody: Experiments and Calculations

机译：高超音速前体上的边界层过渡：实验和计算

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来源
《16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference》|2009年|1-15|共15页
会议地点 Bremen(DE)
作者
E. Orlik; I. Fedioun; D. Davidenko;
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作者单位

Centre National de la Recherche Scientifique (CNRS), OrlÃ©ans, France;

Centre National de la Recherche Scientifique (CNRS), OrlÃ©ans, France;

Centre National de la Recherche Scientifique (CNRS), OrlÃ©ans, France;

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会议组织
原文格式 PDF
正文语种 eng
中图分类各类型航空器;
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机译：高超音速前体的边界层过渡：实验与计算
2. Boundary-Layer Transition on a Hypersonic Forebody: Experiments and Calculations [J] . Evgeniy Orlik, Ivan Fedioun, Dmitry Davidenko Journal of Spacecraft and Rockets . 2011,第4期

机译：高超音速前体的边界层过渡：实验和计算
3. Roughness-Induced Boundary-Layer Transition on a Hypersonic Capsule-Like Forebody Including Nonequilibrium [J] . Di Giovanni Antonio, Stemmer Christian Journal of Spacecraft and Rockets . 2019,第6期

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4. Boundary Layer Transition on a Hypersonic Forebody: Experiments and Calculations [C] . E. Orlik, I. Fedioun, D. Davidenko American Institute of Aeronautics and Astronautics/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference . 2009

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5. Numerical Investigation of the Nonlinear Transition Stages in Hypersonic Boundary Layers [D] . Meersman, John A. 2019

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6. Effect of a Roughness Element on the Hypersonic Boundary Layer Receptivity Due to Different Types of Free-Stream Disturbance with a Single Frequency [O] . Mingfang Shi, Lidan Xu, Zhenqing Wang, 2019

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7. Experiments on hypersonic boundary layer transition on blunt cones with acoustic-absorption coating [O] . A. Shiplyuk, S. Lukashevich, D. Bountin, 2012

机译：用声学吸收涂层钝性锥体过度边界层过渡的实验
8. Hypersonic Laminar Boundary Layer Transition. Part 1. Nosetip Bluntness Effects on Cone Frustum Transition. Part 2. Mach 6 Experiments of Transition on a Cone at Angle of Attack [R] . Stetson, K. F. 1986

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Boundary Layer Transition on a Hypersonic Forebody: Experiments and Calculations

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