Experimental Investigation of the Transonic Airfoils DA LVA-1Ae and VA-2 with Shock Control-Reference-Cited by-同舟云学术

Experimental Investigation of the Transonic Airfoils DA LVA-1Ae and VA-2 with Shock Control

Published:1997 Issue: Volume: Page:355-378
ISSN:0179-9614
Container-title:Notes on Numerical Fluid Mechanics (NNFM)
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Author:

Rosemann H.,Knauer A.,Stanewsky E.

Publisher

Vieweg+Teubner Verlag

Link

http://link.springer.com/content/pdf/10.1007/978-3-322-90711-0_21

Reference5 articles.

1. P. Thiede, P. Krogmann, and E. Stanewsky. Active and passive shock boundary layer interaction control on supercritical airfoils. AGARD-CP-365, (Brussels, Belgium), 1984.

2. J. Delery, J. Fulker, W. Geissler, and E. Stanewsky. European shock control investigation: Objectives, approach and previous results. In Proceedings 2nd Community Aeronautics RTD Conference, Napoli (Italy), 4–5 October 1993.

3. R. D. Boehe. Transonic measurements on the airfoil VFW-F VA-2 at the DFVLR Göttingen. Report No. 8, ZKP Wing Section, November 1976. Ministry of Science and Technology Reference LFK 7511.

4. B. Binder, L. Riethmüller, S. Tusche, and R. Wulf. Modernisierung des Transsonischen Windkanals in Göttingen (Upgrading the Transonic Wind Tunnel Göttingen). In Jahrbuch der DGLR, volume 1, 1992.

5. E. Stanewsky. Shock boundary layer interaction (simulation). In Boundary Simulation and Control in Wind Tunnels, AGARD-AR-224, April 1988.

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