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New Results in Numerical and Experimental Fluid Mechanics V pp 85–93Cite as

Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged Navier-Stokes Solver

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Summary

A selection of steady and unsteady validation results for the Reynolds-averaged Navier-Stokes solver FLM-NS with respect to an experimental delta wing test case is presented and compared to other numerical results. Having put the numerical method’s validity into evidence, the unsteady flow induced by an oscillating flap is investigated for a Fighter Type Delta Wing.

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References

  1. Baldwin B. S., Lomax H.: Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows. AIAA Paper 78-257, NASA Ames Research Center, Moffett Field, CA, USA, 1978.

    Google Scholar 

  2. Bennett R. M., Walker C. E.: Computational Test Cases for a Clipped Delta W’mg With Pitching and Trailing-Edge Control Surface Oscillations. NASA-TM-1999-209104, NASA Langley Research Center, Hampton, Virginia, 1999.

    Google Scholar 

  3. Blazek J.: Investigations of the Implicit LU-SSOR Scheme. DLR-FB 93-51, DLR, 1993.

    Google Scholar 

  4. Chakravarthy S. R.: High Resolution Upwind Formulations for the Navier-Stokes Equations. Rockwell Int. Science Center, USA, 1988.

    Google Scholar 

  5. Kroll N.: FLOWer Installation and User Handbook, Release 116. Institut für Entwurfsaerodynamik, DLR, Braunschweig, 2001.

    Google Scholar 

  6. Markmiller J.: Validierung eines zeitechten und eines small diSttLrbance Navier-Stokes Verfahrens an einem sehwingenden Deltaflügel. Diploma thesis, Technische Universität München, TUM-FLM-2003/28, 2003.

    Google Scholar 

  7. Obayashi S., Garuswamy G. P.: Navier-Stokes Computations for Oscillating Control Surfaces. Journal of Aircraft, Vol. 31, pp. 631–636, 1994.

    Article  Google Scholar 

  8. Spalart P. R., Allmaras S. R.: A one-equation turbulence model for aerodynamic flows. AIAA Paper 92-0439, 30th Aerospace Sciences Meeting & Exhibit, Reno, NV, USA, 6.-9. January, 1992.

    Google Scholar 

  9. Wilcox D. C.: Reassessment of the Scale-Determining Equation for Advanced Turbulence Models. AIAA-Joumal, Vol. 26, pp. 1299–1310, 1988.

    Article  MATH  MathSciNet  Google Scholar 

  10. ICEM-CFD Hexa, Operating Manual. ICEM CFD & Structural Engineering GmbH, 1998.

    Google Scholar 

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Author information

Authors and Affiliations

  1. Technische Universität München, Lehrstuhl für Fluidmechanik, Abteilung Aerodynamik, Boltzmannstrasse 15, 85748 Garching, Germany

    Alexander Allen, Michail Iatrou, Alexander Pechloff & Boris Laschka

Authors
  1. Alexander Allen
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  2. Michail Iatrou
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  3. Alexander Pechloff
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  4. Boris Laschka
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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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Cite this paper

Allen, A., Iatrou, M., Pechloff, A., Laschka, B. (2006). Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged Navier-Stokes Solver. 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_11

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  • DOI: https://doi.org/10.1007/978-3-540-33287-9_11

  • 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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