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PARALLEL TURBULENT NAVIER-STOKES SOLUTIONS OF WING ALONE GEOMETRIES FOR DRAG PREDICTION

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Parallel Computational Fluid Dynamics 2007

Part of the book series: Lecture Notes in Computational Science and Engineering ((LNCSE,volume 67))

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Abstract

An in-house-developed, three dimensional structured Navier-Stokes solver (xFLOWg) is used in the transonic wing computations. Wing alone geometries are taken from Drag Prediction Workshop III (DPW3) [1], which was held on June 3-4, 2006, in San Francisco, CA. Although experimental results are not available for the test cases of DPW3, drag and lift comparison with the well-known CFD codes appears to be a satisfactory validation study.

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References

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Authors and Affiliations

  1. Design and Engineering Dept.,, TAI, Technopolis M.E.T.U, Ankara, TURKEY

    Pinar Sahin

Authors
  1. Pinar Sahin
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  2. Emre Gürdamar
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  3. Erhan Tarhan
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  4. Yüksel Ortakaya
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© 2009 Springer-Verlag Berlin Heidelberg

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Sahin, P., Gürdamar, ., Tarhan, E., Ortakaya, Y. (2009). PARALLEL TURBULENT NAVIER-STOKES SOLUTIONS OF WING ALONE GEOMETRIES FOR DRAG PREDICTION. In: Parallel Computational Fluid Dynamics 2007. Lecture Notes in Computational Science and Engineering, vol 67. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-92744-0_28

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