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The leading-edge effects on the laminar flat- plate boundary layer and the aerodynamic heating at Mach 10.4

机译：层流平板边界层的前沿效应和马赫数10.4的空气动力学加热

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Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.4

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作者
Stone, H. W.;
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年度 1969
页码 1-34
总页数 34
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC HEATING; FLAT PLATES; HYPERSONIC FLOW; LAMINAR BOUNDARY LAYER; LEADING EDGES; BOUNDARY LAYER TRANSITION; FLOW DISTRIBUTION; HEAT TRANSFER COEFFICIENTS; PRESSURE; VELOCITY DISTRIBUTION; VISCOUS FLOW;

机译：空气动力加热;平板;超音速流动; LamINaR BOUNDaRY LaYER;领先的边缘;边界层转换;流量分配;换热系数;压力;速度分布;粘性流动;

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专利

1. A Dynamical-Systems Approach to Laminar-Turbulent Transition in a Flat- Plate Boundary Layer [J] . REMPFER D. Zeitschrift fur Angewandte Mathematik und Mechanik . 1996,第S5期

机译：平板边界层中层流-湍流过渡的动力学系统方法
2. INFLUENCE OF THE PLATE LEADING-EDGE SHAPE AND THICKNESS ON THE BOUNDARY LAYER LAMINAR-TURBULENT TRANSITION IN HYPERSONIC FLOW [J] . S.V. Aleksandrov, E.A. Aleksandrova, V.Ya. Borovoy, TsAGI science journal . 2019,第5期

机译：板缘边缘形状和厚度对高辐射流动边界层层状湍流过渡的影响
3. Aerodynamic optimization of the flat-plate leading edge for experimental studies of laminar and transitional boundary layers [J] . Ronald E. Hanson, Howard P. Buckley, Philippe Lavoie Experiments in Fluids . 2012,第4期

机译：平板前缘的空气动力学优化，用于层流和过渡边界层的实验研究
4. On Instability and Structural Sensitivity of Incompressible Laminar Separation Bubbles on a Flat- Plate Boundary Layer [C] . D. Rodr? AIAA Fluid Dynamics Conference and Exhibit . 2008

机译：平板边界层上不可压缩层流分离气泡的不稳定性和结构敏感性
5. Analysis of compressible laminar boundary layers at Mach numbers up to 30 considering real gas effects. [D] . Moraes, Augusto Cesar Martins de. 1995

机译：考虑实际气体影响，分析马赫数最多为30的可压缩层流边界层。
6. MHD Free Convective Boundary Layer Flow of a Nanofluid past a Flat Vertical Plate with Newtonian Heating Boundary Condition [O] . Mohammed J. Uddin, Waqar A. Khan, Ahmed I. Ismail -1

机译：纳米流体的mHD自由对流边界层流过一垂直平板与牛顿暖气边界条件
7. Aerodynamic Heating of a Gap in the Hypersonic Laminar Boundary Layer [O] . Hironao YOKOI, Hiroto KOYAMA, Yoshiaki NAKAMURA 2013

机译：超声波层边界层中间隙的空气动力学加热

The leading-edge effects on the laminar flat- plate boundary layer and the aerodynamic heating at Mach 10.4

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