Author:
Neumann Jens,Friedewald Diliana,Hennings Holger
Publisher
Springer Science and Business Media LLC
Subject
Aerospace Engineering,Transportation
Reference25 articles.
1. Klein, A., Lutz, T., Krämer, E., Richter, K., Gardner, A.D., Altmikus, A.R.M.: Numerical comparison of dynamic stall for two-dimensional airfoils and an airfoil in the DNW–TWG. J. Am. Helicopter Soc. 57, 1–13 (2012)
2. G. Dietz, G. Schewe, F. Kießling, M. Sinapius. Limit-cycle oscillation experiment at a transport aircraft wing model. In: Proceedings of the International Forum on Aeroelasticity and Structural Dynamics (IFASD), Amsterdam, The Netherlands, June 4–6 (2003)
3. T. Gerhold, M. Galle, O. Friedrich, J. Evans. Calculation of complex three-dimensional configurations employing the DLR TAU-code. In: 35th Aerospace Sciences Meeting and Exhibit, AIAA Paper, vol. 0167 (1997)
4. Krumbein, A.:
$$e^n$$
e
n
transition prediction for 3d wing configurations using database methods and a local, linear stability code. Aerosp. Sci. Technol. 12, 592–598 (2008)
5. Krimmelbein, N., Radespiel, R.: Transition prediction for three-dimensional flows using parallel computation. Comput. Fluids 38, 121–136 (2009)
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