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Flow Field Study of a Supersonic Jet Exiting into a Supersonic Stream

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New Results in Numerical and Experimental Fluid Mechanics V

Summary

The paper present a numerical/experimental investigation of the flow field resulting around a generic vehiole controlled by means of a lateral jet in supersonic motion. The experimental data are acquired in the DLR wind tunnel TMK in Cologne. To obtain the numerical results, the 3-D viscous, turbulent, Reynolds-averaged hybrid Navier-Stokes Code TAU of DLR is used. Caloulations are made for free stream Maeh number of M∞=2.8 and various angles of attack. Several grids of varied density and structure and different Inrbulenee models are investigated. The CFD results in terms of surface pressure, normal force coefficients, and jet interaction are in good agreement with the results from wind-tunnel tests. On hand the numerical results it is shown important features of the interaction mechanisms between the lateral jet and the flow field originated by the motion of the vehicle.

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References

  1. Andreas Maok, Volker Hannemann; Validation of the Unstmotured DLR-TAU-Code for Hypersonio Flow; AIAA 2002-31111, 2002

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  2. H. Esch: Druckverteilungsmessungen an einem Flugköpeammapf im Obersohall Messdaten; DLR, IB 39113 97C0 3

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  3. Louis A. Cassel; Applying Jet Ineraction Technolog, Joumal of Spacecrafland Rookets, Vol.40, No 4, Juli-August 2003

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  4. P. Champigny; R. Laeau; Lateral Jet control for tactical Missiles; Proceedings of the AGARD Special; AGARD-R-74, pp. 3-1 to 3-57

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Author information

Authors and Affiliations

  1. DLR, Institute of Aerodynamics and Flow Technology, Lilienthalplatz 7, 38108, Braunschweig, Germany

    R. Adeli & J. M. A. Longo

  2. DLR, Institute of Aerodynamics and Flow Technology, Linder Höhe, 5114, Köln, Germany

    H. Emunds

Authors
  1. R. Adeli
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  2. J. M. A. Longo
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  3. H. Emunds
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Editor information

Editors and Affiliations

  1. ZARM - University of Bremen Am Fallturm/Hochschulring, D-28359, Bremen

    Hans-Josef Rath  & Carsten Holze  & 

  2. Aerospace Science and Technology, AST, DLR, Bunsenstraße 10, D-37073, Götingen

    Hans-Joachim Heinemann (Co-Managing Editor) (Co-Managing Editor)

  3. Airbus Deutschland GmbH, Hünefeldstraße 1-5, D-28199, Bremen

    Rolf Henke (Senior Project Manager) (Senior Project Manager)

  4. DLR - AE, Bunsenstraße 10, D-37073, Göttingen

    Heinz Hönlinger

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© 2006 Springer-Verlag Berlin Heidelberg

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Adeli, R., Longo, J.M.A., Emunds, H. (2006). Flow Field Study of a Supersonic Jet Exiting into a Supersonic Stream. 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_20

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  • DOI: https://doi.org/10.1007/978-3-540-33287-9_20

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-33286-2

  • Online ISBN: 978-3-540-33287-9

  • eBook Packages: EngineeringEngineering (R0)

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