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Steady/oscillatory, supersonic/hypersonic inviscid flow past oscillating wings and wedge combinations at arbitrary angles of attack.

机译：稳定/振荡，超音速/超人的无粘性流以任意迎角流过摆动的机翼和楔形组合。

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http://archive.org/details/steadyoscillator00your

机译：HTTP://archive.org/details/steady oscillator00有人

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Youroukos Evangelos Vlassios;
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年度 1981
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正文语种 en_US
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专利

1. Steady supersonic flow past an almost straight wedge with large vertex angle [J] . Zhang YQ. Journal of Differential Equations . 2003,第1期

机译：稳定的超音速流经过具有大顶角的几乎笔直的楔形
2. Gas-Kinetic Harmonic Balance Method for Unsteady Supersonic/Hypersonic Flows with Oscillating Motions [J] . Zhou Di, Lu Zhiliang, Guo Tongqing, AIAA Journal . 2020,第1期

机译：波动运动的非定常超音速/超人流的气动力学谐波平衡方法
3. Acoustic Leading-Edge Receptivity for Supersonic/Hypersonic Flows over a Blunt Wedge [J] . Cerminara Adriano, Sandham Neil D. AIAA Journal . 2017,第12期

机译：钝器上超音速/超人流的声学前沿接收
4. SOME ASPECTS OF THREE DIMENSIONAL SUPERSONIC/HYPERSONIC INVISCID BLUNT BODY FLOW COMPUTATIONS EMPLOYING HIGH RESOLUTION TVD SCHEMES BASED ON ROE'S RIEMANN SOLVER [C] . S. K. Saxena, K. Ravi AIAA applied aerodynamics conference . 1994

机译：三维超音速/超音速体外钝性钝体流量计算，采用基于Roe的Riemann求解器的高分辨率TVD方案
5. Numerical Simulations of Inviscid Supersonic and Hypersonic Flows [D] . Han, Ryan Mathew. 2020

机译：物质超声波和超音速流动的数值模拟
6. Analytical solutions for two-dimensional Stokes flow singularities in a no-slip wedge of arbitrary angle [O] . Darren G. Crowdy, Samuel J. Brzezicki -1

机译：任意角度防滑楔中二维斯托克斯流奇点的解析解
7. On hypersonic flow around winged-vehicles at high angles of attack. [O] . Michiru YASUHARA, Kiyoshi TSUBOI, Nobuhiko FUKUDA, 1985

机译：在高角度的翼型车辆周围的超声波流动。

Steady/oscillatory, supersonic/hypersonic inviscid flow past oscillating wings and wedge combinations at arbitrary angles of attack.

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