Numerical Study of the Subsonic Base Flow with a Side Support

Author:

You Yancheng,Oßwald Kai,Lüdeke Heinrich,Hannemann Volker

Publisher

Springer Berlin Heidelberg

Reference7 articles.

1. Wolf, C.C., Hornschemeyer, R., Henke, R.: Investigation on Turbulence Structures in the Wake of a Generic Rocket Configuration. In: DGLR STAB-Symposium 2010. NNFM (2010)

2. Wolf, C.C., You, Y., Hornschemeyer, R., Ludeke, H., Hannemann, V.: Base-flow sensitivity of a generic rocket forebody towards small freestream angles. In: Proceedings of the 4th EUCASS Conference, St. Petersburg (2011)

3. Mack, A., Hannemann, V.: Validation of the unstructured DLR-TAU Code for Hypersonic Flows. AIAA 2002-3111 (2002)

4. Reimann, B., Johnston, I., Hannemann, V.: DLR-TAU Code for High Enthalpy Flows. NNFM, vol. 87, pp. 99–106. Springer DE (2004)

5. Spalart, P.R., Jou, W.H., Strelets, M., Allmaras, S.R.: Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach. In: Advances in DNS/LES, pp. 137–147. Greyden Press (1997)

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