The ultra-low Reynolds number airfoil wake

By Md. Mahbub Alam, Yu Zhou, Hang Yang, H. Guo, J. Mi. 2010

157 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/931387972342c1e40c75a7874ad9dc20d747623c

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Md. Mahbub Alam
2. X. W. Wang
3. Yu Zhou
4. Dilek Funda Kurtulus

In Computational Mechanics

1. Md. Mahbub Alam
2. X. W. Wang
3. Yu Zhou
4. Dilek Funda Kurtulus
5. David Sumner

Citations in the corpus

• On the Unsteady Behavior of the Flow around NACA 0012 Airfoil with Steady External Conditions at Re=1000 (2015, background): “In addition, previous works on low Reynolds numbers have paid little attention to the flowfield and aerodynamic properties at large angle of attack [15].”
• The wake of two side-by-side square cylinders (2011, background): “…and r.m.s. values of the streamwise velocity at 438 Md M. Alam, Y. Zhou and X. W. Wang the point corresponding to the shear layer roll-up position, where the maximum urms occurs (Alam et al. 2010), have been confirmed to approach their asymptotic values when the number of images reached 400.”