Current Capability of Unstructured-Grid CFD and a Consideration for the Next Step
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Publisher
Springer Berlin Heidelberg
Link
http://link.springer.com/content/pdf/10.1007/978-3-540-74384-2_5.pdf
Reference11 articles.
1. Jameson, A. and Baker, T.J.: Improvements to the Aircraft Euler Method. AIAA Paper 1987-452 (1987).
2. Nakahashi, K., Ito, Y., and Togashi, F.: Some challenges of realistic flow simulations by unstructured grid CFD. Int. J. for Numerical Methods in Fluids, 43, 769–783 (2003).
3. Pambagjo, T.E., Nakahashi, K., Matsushima, K.: An Alternate Configuration for Regional Transport Airplane. Transactions of the Japan Society for Aeronautical and Space Sciences, 45,148, 94–101 (2002).
4. Yamazaki, W., Matsushima, K. and Nakahashi, K.: Drag Reduction of a Near-Sonic Airplane by using Computational Fluid Dynamics. AIAA J., 43, 9, 1870–1877 (2005).
5. Koc, S., Kim, H.J. and Nakahashi, K.: Aerodynamic Design of Wing-Body-Nacelle-Pylon Configuration. AIAA-2005-4856, 17th AIAA CFD Conf. (2005).
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