@inproceedings{fb0534bfb60047168a7bd0a883fb1766,
title = "CFD analysis of unsteady aerodynamics of airfoils for rotor applications",
abstract = "The NLR 7223-62 airfoil is a high speed airfoil with peaky leading edge contour. The high lift performance needed for helicopter applications is achieved by an inverse camber at the trailing edge. In this paper, unsteady flow fields of this airfoil are computed using CFD based on RANS. Several turbulence models are investigated for Mach numbers up to 0.7. The CFD results are compared with experimental results.",
author = "E. Dumlupinar and Murthy, {V. R.}",
year = "2006",
doi = "10.2514/6.2006-3375",
language = "English (US)",
isbn = "1563478102",
series = "Collection of Technical Papers - 36th AIAA Fluid Dynamics Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "1296--1305",
booktitle = "Collection of Technical Papers - 36th AIAA Fluid Dynamics Conference",
note = "36th AIAA Fluid Dynamics Confernce ; Conference date: 05-06-2006 Through 08-06-2006",
}