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机译:基于实验和计算流体力学的低雷诺数NACA 0021翼型截面的静态和动态分析
Tech Univ Berlin, Hermann Fottinger Inst, Chair Fluid Dynam, Muller Breslau Str 8, D-10623 Berlin, Germany;
Univ Firenze, Dept Ind Engn, Via Santa Marta 3, I-50139 Florence, Italy;
Univ Firenze, Dept Ind Engn, Via Santa Marta 3, I-50139 Florence, Italy;
Tech Univ Berlin, Hermann Fottinger Inst, Chair Fluid Dynam, Muller Breslau Str 8, D-10623 Berlin, Germany;
Tech Univ Berlin, Hermann Fottinger Inst, Chair Fluid Dynam, Muller Breslau Str 8, D-10623 Berlin, Germany;
Tech Univ Berlin, Hermann Fottinger Inst, Chair Fluid Dynam, Muller Breslau Str 8, D-10623 Berlin, Germany;
Univ Pisa, DESTEC, I-56122 Pisa, Italy;
Univ Firenze, Dept Ind Engn, Via Santa Marta 3, I-50139 Florence, Italy;
Tech Univ Berlin, Hermann Fottinger Inst, Chair Fluid Dynam, Muller Breslau Str 8, D-10623 Berlin, Germany;
Tech Univ Berlin, Hermann Fottinger Inst, Chair Fluid Dynam, Muller Breslau Str 8, D-10623 Berlin, Germany;
机译:动态攻角变化和低雷诺数下NACA 0021机翼的实验分析
机译:用于风力涡轮机分析的低雷诺数下NACA 0021翼型截面通过180度迎角的实验分析
机译:关于改善低雷诺数对称翼型数值分析的前景,LES方法的高攻击角度:NaCA0021简介的情况
机译:基于实验和CFD的低雷诺数NACA 0021机翼截面的静态和动态分析
机译:低雷诺数的弧形Naca 65(1)-412翼型的直接数值模拟:流动分离,稳定性和拉格朗日空气动力学
机译:关于具有非恒定流的等离子作动器的翼型的计算流体动力学模拟的数据
机译:在攻击变化动态角度下Naca 0021翼型的实验分析和低雷诺数
机译:ames高雷诺数装置中NaCa 0012翼型的静态和动态压力测量