@inproceedings{38ed53a08bbe4a71ad6656e52d9754d9,
title = "Aerodynamic optimization of multi-element airfoil",
abstract = "In this paper, aerodynamic design of high-lift multi-element airfoil is conducted based on a gradient-based optimization method utilizing CFD and sensitivity analysis method. For flow analysis, a 2-D unstructured Navler-Stokes solver Is applied, and a solution-adaptive grid is generated for accuracy enhancement. For efficient calculation of objective function gradient, a discrete adjoint code is applied. Utilizing the above methods, aerodynamic optimization system is developed. As a design example, lift of the 30P30N airfoil is maximized.",
author = "Haruka Nakayama and Kim, {Hyoung Jin} and Kisa Matsushima and Kazuhiro Nakahashi and Keizo Takenaka",
year = "2006",
doi = "10.2514/6.2006-1051",
language = "English",
isbn = "1563478072",
series = "Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "12612--12626",
booktitle = "Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting",
note = "44th AIAA Aerospace Sciences Meeting 2006 ; Conference date: 09-01-2006 Through 12-01-2006",
}