A two-element high-lift airfoil in disturbed flow conditions

Author:

Klein S.,Scholz P.,Radespiel R.

Funder

Deutsche Forschungsgemeinschaft

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference19 articles.

1. Hahn, D., Scholz, P., Semaan, R., Radespiel, R., Müller-Eigner, R.: Erzeugung definierter Querwirbel in einer geschlossenen Messstrecke,’ 60. Deutscher Luft- und Raumfahrtkongress, DGLR, Bremen (2011)

2. Klein, S., Hoppmann, D., Scholz, P., Radespiel, R.: High-lift airfoil interacting with a vortical disturbance: wind-tunnel measurements. AIAA J. 53(6), 1681–1692 (2015)

3. Klein, S., Scholz, P., Radespiel, R.: Interaction of three-dimensional disturbances with the flow around a two-element high-lift airfoil, 4th Symposium “Simulation of Wing and Nacelle Stall”. TU Braunschweig, Braunschweig (2014)

4. Ham, N.D.: Some conclusions from an investigation of blade–vortex interaction. J. Am. Helicopter Soc. 20, 26–31 (1975)

5. Patel, M.H., Hancock, G.J.: Some experimental results of the effect of a streamwise vortex on a two-dimensional wing. Aeronaut. J. 78(760), 151–155 (1974)

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