Two-Dimensional Low-Reynolds Number Wind Tunnel Results for Airfoil NACA 0018

By W. A. Timmer. 2008

191 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/9fb947216d7fac57d9314ef29e13d934e459c44e

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. Mirjam Snellen
2. F. Avallone
3. S. van der Zwaag
4. A. R. Carpio
5. R. M. Martínez
6. D. Ragni

In Computational Mechanics

1. Mirjam Snellen
2. F. Avallone
3. S. van der Zwaag
4. A. R. Carpio
5. R. M. Martínez
6. D. Ragni

Citations in the corpus

• Experimental characterization of the turbulent boundary layer over a porous trailing edge for noise abatement (2019, methodology): “A stethoscope probe [31,37,38] is employed to confirm that the boundary layer flow downstream the strip location is turbulent; a detailed description of the system employed in the present experiment is presented in Lentink et al.”