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Part of the book series: Notes on Numerical Fluid Mechanics (NNFM) ((NONUFM,volume 55))

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Abstract

During the last years with a constant increasing activity, an increasing number of scientific meetings gathering expert researchers and engineers have taken place in the field of Computational Fluid Dynamics.

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References

  1. Jameson, A. Automatic Design of Transonic Airfoil to Reduce the Shock-Induced Pressure Drag, 31st Israel Annual Conference Aviation and Aeronautics, February 21–22, 1990.

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References

  1. Williams, B. R. “An exact test case for the plane potential flow about two adjacent lifting airfoils” ARCR amp M, 3717, 1973.

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References

  1. Voorem, J. van der, Wees, A. J. van der, and Meelker, J. H. “Transonic potential flow calculations about transport aircraft” AGARD Conf. Proc. No. 412 (1986).

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  2. Voorem, J. van der, Wees, A. J., “Inviscid drag prediction for transonic transport wings using a full-potential method” AIAA-90-0576 (1990). Published in tha AIAA Journal.

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Authors

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Jacques Periaux Gabriel Bugeda Panagiotis K. Chaviaropoulos Theo Labrujere Bruno Stoufflet

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© 1997 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden

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Periaux, J., Bugeda, G., Chaviaropoulos, P.K., Labrujere, T., Stoufflet, B. (1997). Definition of the Problems for the Analysis. In: Periaux, J., Bugeda, G., Chaviaropoulos, P.K., Labrujere, T., Stoufflet, B. (eds) EUROPT — A European Initiative on Optimum Design Methods in Aerodynamics. Notes on Numerical Fluid Mechanics (NNFM), vol 55. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-86570-0_2

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  • DOI: https://doi.org/10.1007/978-3-322-86570-0_2

  • Publisher Name: Vieweg+Teubner Verlag

  • Print ISBN: 978-3-322-86572-4

  • Online ISBN: 978-3-322-86570-0

  • eBook Packages: Springer Book Archive

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