@inproceedings{6ab342b447d14f4f97df6cd1682bbe31,
title = "Aerodynamic shape optimization of transonic airfoil and wing using response surface methodology",
abstract = "A Response Surface Methodology (RSM) for Aerodynamic Shape Optimization (ASO) using the compressible Reynolds-Averaged Navier- Stokes (RANS) equations is implemented and tested. The quadratic polynomials which cancel the second-order cross items are employed to construct RS model. This approach improves on the efficiency of using the RSM for highdimensional design optimization problems. By using present method the aerodynamic performance of the transonic airfoil and wing are greatly improved. Successful design results confirm validity and efficiency of the present design method.",
keywords = "Optimization, Response surface methodology, Transonic",
author = "Xiong, {J. T.} and Qiao, {Z. D.} and Han, {Z. H.}",
year = "2006",
language = "英语",
isbn = "9781604232271",
series = "ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006",
publisher = "International Council of The Aeronautical Sciences (ICAS)",
pages = "923--929",
booktitle = "ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006",
note = "25th Congress of the International Council of the Aeronautical Sciences 2006 ; Conference date: 03-09-2006 Through 08-09-2006",
}