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Detached-Eddy Simulation of Supersonic Flow Past Cylindrical Aft Body with and without Base Bleed

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New Results in Numerical and Experimental Fluid Mechanics VII

Summary

In the present work supersonic base flows with and without base bleed are studied to investigate the influence of the bleed on the flow field. To this end, simulations are performed using detached-eddy simulation. To evaluate the performance of DES, numerical predictions are compared with computations based on RANS and experimental data for the base flow without bleed. To understand the influence of the bleed on the flow and the base pressure distribution, predictions of the base flow with bleed are compared with numerical data of the case without bleed.

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References

  1. 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, 1st AFSOR Int. Conf. on DNS/LES. Greyden Press, Col (1997)

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  2. Herrin, J.L., Dutton, J.C.: Supersonic Base Flow Experiments in the Near Wake of a Cylindrical Afterbody. AIAA Journal 32(1), 77–83 (1994)

    Article  Google Scholar 

  3. Mathur, T., Dutton, J.C.: Base Bleed Experiments With a Cylindrical Afterbody in Supersonic Flow. AIAA Paper No. 95-0062 (1995)

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  4. Mack, A., Hannemann, V.: Validation of the Unstructured DLR TAU-Code for Hypersonic Flows. AIAA Paper No. 2002-3111 (2002)

    Google Scholar 

  5. Simon, F., Deck, S., Guillen, P.: Reynolds-Averaged Navier-Stokes/Large-Eddy Simulation of Supersonic Base Flow. AIAA Journal 44(11), 2578–2590 (2006)

    Article  Google Scholar 

  6. Mathur, T., Dutton, J.C.: Base Bleed Experiments With a Cylindrical Afterbody in Supersonic Flow. J. Spacecrafts and Rockets 33, 30–37 (1996)

    Article  Google Scholar 

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© 2010 Springer-Verlag Berlin Heidelberg

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Togiti, V., Breuer, M., Lüdeke, H. (2010). Detached-Eddy Simulation of Supersonic Flow Past Cylindrical Aft Body with and without Base Bleed. In: Dillmann, A., Heller, G., Klaas, M., Kreplin, HP., Nitsche, W., Schröder, W. (eds) New Results in Numerical and Experimental Fluid Mechanics VII. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 112. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-14243-7_9

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  • DOI: https://doi.org/10.1007/978-3-642-14243-7_9

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-14242-0

  • Online ISBN: 978-3-642-14243-7

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