Summary
In the presented work the influence of the new defined parameter d = D/δ on the shock system of a double ramp configuration was investigated, with D describing the distance between the two ramp kinks. Oil the basis of the experimental and numerical investigations the functional dependency of the most important parameter of the Free Interaction Concept, the upstremn interaction length l 0 on the parameter d, could clearly be shown. Therefore an enlargement of the free interaction concept is suggested with respect to the double ramp parameter d. Moreover, through the investigations of the flat plate/double ramp configuration a critical minimum of the first ramp length was found for the investigated R/m-ranges, to realise the wished two shock compression.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Delery, J., Marvin, J.: Shock-Wave Boundary-Layer Interactions. AGARDograph 280, pp. 51–85, 1986.
Fedorova, N.N., Fedorchenko, I.A., Shuelein, A.: Experimental and Numerical Study of Oblique Shock Wave / Turbulent Boundary-Layer Interaction at M=5. Computational Fluid Dynamics, Vol. 10, No. 3, pp. 376–381, 2001.
Gaisbauer, U.: Untersuchungen zur Stoß-Grenzschicht-Wechselwirkung an einer Doppelrampe unter verschiedenen Randbedingungen. Dissertation, Universität Stuttgart, 2004.
Gaisbauer, U., Knauss, H., Wagner, S., Kharlamova, Y.V., Fedorova, N.N.: Shock/Turbulent Boundary-Layer Interaction on a Double Ramp Configuration-Experiments and Computations. Proceedings of XI International Conference on the Methods of Aerophysical Research, ICMAR, Vol. 3, pp. 56–62, 2002.
Gaisbauer, U., Knauss, H., Weiss, J., Wagner, S.: Measurement Techniques for Detection of Low Disturbance and Transition Localization in a Short Duration Wind Tunnel. Proceedings of X International Conference on the Methods of Aerophysical Research, ICMAR, Vol. 2, pp. 54–67, 2000.
Knauss, H., Riedel, R., Wagner, S.: The Shock Wind Tunnel of Stuttgart University-A Facility for Testing Hypersonic Vehicles. AIAA-Paper 99-4959, 1999.
Schlaich, F.: Experimentelle Untersuchungen zur Wechselwirkung zwischen Stoß und turbulenter Grenzschicht an einer Doppelrampe im Überschall. Dissertation, Universität Stuttgart, 1996.
Settles, G.S.: An experimental study of compressible turbulent boundary-layer separation at high Reynoldsnumber. Ph.D. Thesis, Princeton University, 1975.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2006 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Gaisbauer, U., Knauss, H., Fedorova, N.N., Kharlamova, Y.V. (2006). Experimental and Numerical Investigations of Shock/Turbulent Boundary Layer Interaction on a Double Ramp Configuration. In: Rath, HJ., Holze, C., Heinemann, HJ., Henke, R., Hönlinger, H. (eds) New Results in Numerical and Experimental Fluid Mechanics V. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 92. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-33287-9_37
Download citation
DOI: https://doi.org/10.1007/978-3-540-33287-9_37
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-33286-2
Online ISBN: 978-3-540-33287-9
eBook Packages: EngineeringEngineering (R0)