@inproceedings{oai:jaxa.repo.nii.ac.jp:00005745,
 author = {Grenon, Richard},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)},
 month = {Mar},
 note = {SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design 航空宇宙技術研究所 19980316-19980317 東京 日本, SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design National Aerospace Laboratory 19980316-19980317 Tokyo Japan, A numerical optimization code for the aerodynamic design of wing-body configurations has been recently developed at ONERA. This optimization code has been built by coupling the CONMIN (CONstrained MINimization) code of G.N. Vanderplaats which performs the constrained minimization of a function of N variables with as ONERA Euler code for aerodynamic computations. For this purpose, a geometry generator taking into account a great number of design variables and an automatic grid generator have also been developed. In the first part of this paper, the general organization of the ONERA optimization code is presented. In a second part, the first results from an application of this code to the design of a supersonic transport aircraft are presented and the strategy of optimization is discussed., 資料番号: AA0063609014, レポート番号: JAXA-SP-06-029E},
 pages = {88--108},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Numerical optimization in aerodynamic design with application to a supersonic transport aircraft},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}