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Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000.

机译：对NACA 0012翼型在M = 0.3和雷诺数为540,000时可压缩，稳定和振荡流的分离气泡行为的实验和计算分析。

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Approved for public release; distribution is unlimited

机译：批准公开发布；发行是无限的

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Van Dyken Robert D.;
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年度 1997
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1. Separation and Reattachment Points of a NACA0012 Airfoil in a Periodic Flow under Low Reynolds Number [J] . Hirohisa YAMANISHI, Yohsuke TANAKA, Shigeru MURATA Advanced Experimental Mechanics . 2016,第2期

机译：低雷诺数下NACA0012翼型在周期性流动中的分离和重新附着点
2. Localization of Flow Separation and Transition Over a Pitching NACA0012 Airfoil at Transitional Reynolds Numbers Using Hot-Films [J] . Poels Allison, Rudmin Daniel, Benaissa Azemi, Journal of Fluids Engineering: Transactions of the ASME . 2015,第12期

机译：使用热膜在过渡雷诺数下的俯仰NACA0012翼型流分离和过渡的局部化
3. Numerical study of the effect of suction at a compressible and high Reynolds number flow to control the flow separation over Naca 2415 airfoil [J] . Fatahian Esmaeel, Nichkoohi Ali Lohrasbi, Fatahian Hossein Progress in computational fluid dynamics . 2019,第3期

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4. Linear Stability Analysis of Laminar Separation Bubble over NACA0012 airfoil at Low Reynolds Numbers [C] . Egambaravel J., Rinku Mukherjee AIAA SciTech forum;Aerospace sciences meeting . 2014

机译：低雷诺数下NACA0012翼型层流分离气泡的线性稳定性分析
5. Localisation of flow separation and transition over a pitching NACA0012 airfoil at transitional Reynolds number. [D] . Rudmin, Daniel. 2013

机译：流分离和过渡在过渡雷诺数的俯仰NACA0012机翼上的定位。
6. Correction: Computational analysis of the oscillatory behavior at the translation level induced by mRNA levels oscillations due to finite intracellular resources [O] . Yoram Zarai, Tamir Tuller 2019

机译：校正：因细胞内资源有限而引起的mRNA水平振荡诱导的翻译水平振荡行为的计算分析
7. Computational investigations of a NACA 0012 airfoil in low Reynolds number flows [O] . Nowak Lisa M. 1992

机译：低雷诺数流的NACA 0012机翼的计算研究

Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000.

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