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New Results in Numerical and Experimental Fluid Mechanics IV pp 252–259Cite as

Numerical Simulation of Turbulent Flows Inside a Hypersonic Inlet

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Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ((NNFM,volume 87))

Summary

Results of 2D and 3D numerical simulations of a mixed-compression inlet for a scramjet propulsion system under Mach 2.41 and 3.0 test conditions are presented. The computations are performed with the DLR FLOWer code solving the Reynolds averaged Navier-Stokes equations with different turbulence models. The details of corresponding inlet experiments, e.g., leading edge bluntness and tripping wires, are included in the simulation to assess their influence on the test data.

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References

  1. Turan A. Coratekin. Numerical simulation of turbulent shock/boundary-layer interactions in hypersonic flows. Fortschritt-Berichte VDI, 7 (381), 2000.

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  2. Carsten D. Herrmann and Wolfgang W. Koschel. Experimental investigation of the internal compression of a hypersonic intake. AIAA Paper 02–4130, 2002.

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  3. Norbert Kroll, Cord-Christian Rossow, Klaus Becker, and Frank Thiele. The megaflow project. Aerospace Science and Technology, 4: 223–237, 2000.

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  4. Birgit U. Reinartz, Josef Ballmann, Carsten Herrmann, and Wolfgang Koschel. Analysis of hypersonic inlet flows with internal compression. AIAA Paper 02–5230, 2002.

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  5. Birgit U. Reinartz, Joern van Keuk, Turan Coratekin, and Josef Ballmann. Computation of wall heat fluxes in hypersonic inlet flows. AIAA Paper 02–0506, 2002.

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Author information

Authors and Affiliations

  1. Mechanics Laboratory, Aachen University, RWTH Aachen, Templergraben 64, 52064, Aachen, Germany

    Birgit U. Reinartz & Josef Ballmann

Authors
  1. Birgit U. Reinartz
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  2. Josef Ballmann
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Editor information

Editors and Affiliations

  1. Lehrstuhl für Fluidmechanik, Technische Universität München, Bolzmannstr. 15, 85748, Garching, Germany

    Christian Breitsamter  & Boris Laschka  & 

  2. Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Bunsenstr. 10, 37073, Göttingen, Germany

    Hans-Joachim Heinemann

  3. Deutsche Airbus GmbH, Hünefeldstr. 1-5, 28199, Bremen, Germany

    Reinhard Hilbig

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© 2004 Springer-Verlag Berlin Heidelberg

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Cite this paper

Reinartz, B.U., Ballmann, J. (2004). Numerical Simulation of Turbulent Flows Inside a Hypersonic Inlet. In: Breitsamter, C., Laschka, B., Heinemann, HJ., Hilbig, R. (eds) New Results in Numerical and Experimental Fluid Mechanics IV. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 87. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-39604-8_32

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  • DOI: https://doi.org/10.1007/978-3-540-39604-8_32

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-53546-8

  • Online ISBN: 978-3-540-39604-8

  • eBook Packages: Springer Book Archive

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