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
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.
References
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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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).
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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© 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
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Online ISBN: 978-3-322-86570-0
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