Aero-structural Dynamics Experiments at High Reynolds Numbers

Author:

Ballmann Josef,Dafnis Athanasios,Baars Arndt,Boucke Alexander,Brakhage Karl-Heinz,Braun Carsten,Buxel Christian,Chen Bae-Hong,Dickopp Christian,Kämpchen Manuel,Korsch Helge,Olivier Herbert,Ray Saurya,Reimer Lars,Reimerdes Hans-Günther

Publisher

Springer Berlin Heidelberg

Reference25 articles.

1. Cole, S.R., Noll, T.E., Perry III, B.: Transonic Dynamics Tunnel Aeroelastic Testing in Support of Aircraft Development. Journal of Aircraft 40(5), 820–832 (2003)

2. Bartels, R.E., Edwards, J.W.: Cryogenic Tunnel Pressure Measurements on a Supercritical Airfoil for Several Shock Buffet Conditions, NASA TM-110272 (1997)

3. Notes On Numerical Fluid Mechanics And Multidisciplinary Design,2003

4. Ballmann, J., Dafnis, A., Braun, C., Korsch, H., Reimerdes, H.-G., Olivier, H.: The HIRENASD Project: High Reynolds Number Aerostructural Dynamics Experiments in the European Transonic Wind Tunnel (ETW). In: Proceedings of the International Council of the Aeronautical Sciences (ICAS) Congress, Hamburg, Paper-No. 2006-5.11.2 (2006)

5. Klioutchnikov, I., Ballmann, J.: DNS of Transitional Transonic Flow about a Supercritical BAC3-11 Airfoil using High-Order Shock Capturing Schemes. Direct and Large Eddy Simulation VI, pp. 737–744. Springer, Netherlands (2006)

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