首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >CALCULATION OF OPTIMAL SURFACE ROUGHNESS WITH RESPECT TO LIFT/DRAG FORCES ACTING ON WIND TURBINE BLADE
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CALCULATION OF OPTIMAL SURFACE ROUGHNESS WITH RESPECT TO LIFT/DRAG FORCES ACTING ON WIND TURBINE BLADE

机译:关于风轮机叶片升力/阻力的最佳表面粗糙度的计算

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Roughness on the surface of turbine blades induced by icing, dirt, erosion or manufacturing imperfections changes the aerodynamic configurations of wind turbines and reduces the power generation efficiency. In this work, a modified NACA0024 aerofoil is adopted to study effects of surface roughness on lift/drag forces. Three Reynolds numbers, 1000, 2000 and 5000 and a range of angles of attack [0°,20°] are studied. Since the magnitude of the roughness is small, it can be modelled as non-zero velocity boundary conditions imposed on the smooth surface without roughness. The flow with surface roughness can be therefore decomposed as the sum of a flow without roughness and a flow induced by roughness (or the velocity boundary conditions). The first flow can be obtained by solving the Navier-Stokes (NS) equation while the second one is governed by the linearized NS equation. Correspondingly the lift and drag forces acting on the aerofoil can be also decomposed as the sum of a force without considering roughness and a force induced by roughness. Instead of studying a particular type or distribution of roughness, we calculate the optimal roughness, which changes aerodynamic forces most effectively. This optimal roughness is obtained through a sensitivity study by solving an adjoint equation of the linearized NS equation. It is found that the optimal roughness with respect to both drag and lift forces is concentrated around the trailing edge and upper leading edge of the aerofoil and the lift is much more sensitive to roughness than the drag. Then the optimal roughness with a small magnitude is added to the smooth aerofoil geometry and this new geometry is tested through direct numerical simulations (DNS). It is found that the optimal roughness with a small magnitude (e-norm, defined as the square integration of the roughness around the surface, 0.001) induces over 10% change of the lift. Comparing the forces acting on the smooth surface and on the rough surface, it is noticed that the roughness changes the pressure force significantly while has little influence on the viscous forces. The pressure distribution is further inspected to study mechanisms of the effects of roughness on forces.
机译:由于结冰,污垢,腐蚀或制造缺陷而导致的涡轮机叶片表面粗糙度,改变了风力涡轮机的空气动力学结构并降低了发电效率。在这项工作中,采用改良的NACA0024翼型来研究表面粗糙度对升力/阻力的影响。研究了三个雷诺数1000、2000和5000,以及攻角范围[0°,20°]。由于粗糙度的大小很小,因此可以将其建模为施加在没有粗糙度的光滑表面上的非零速度边界条件。因此,具有表面粗糙度的流动可以分解为没有粗糙度的流动和由粗糙度引起的流动(或速度边界条件)的总和。可以通过求解Navier-Stokes(NS)方程来获得第一个流,而第二个流则由线性化的NS方程控制。相应地,作用在翼型上的升力和阻力也可以分解为力的总和,而不考虑粗糙度和由粗糙度引起的力。我们无需研究特定的粗糙度类型或分布,而是计算最佳粗糙度,它可以最有效地改变空气动力。通过求解线性化NS方程的伴随方程,可以通过敏感性研究获得最佳粗糙度。发现相对于阻力和升力而言的最佳粗糙度集中在翼型的后缘和上前缘周围,并且升力比阻力对粗糙度更敏感。然后,将较小幅度的最佳粗糙度添加到平滑的机翼几何形状中,并通过直接数值模拟(DNS)测试此新几何形状。已经发现,小幅度的最佳粗糙度(电子范数,定义为表面周围粗糙度的平方积分,0.001)会引起升力的10%以上的变化。比较作用在光滑表面和粗糙表面上的力,可以看出,粗糙度显着改变了压力,而对粘性力的影响很小。进一步检查压力分布以研究粗糙度对力的影响机理。

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