National Aerospace Laboratory
Fuji Heavy Industries Ltd
Fuji Heavy Industries Ltd
Kawasaki Heavy Industries Ltd Gifu Technical Institute
Fujitsu Ltd
National Aerospace Laboratory
National Aerospace Laboratory
Daiko Denshi Tsushin LTD
Mitsubishi Heavy Industries Ltd
Mitsubishi Heavy Industries Ltd
Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics: CFD workshop on GK airfoil and ONERA M5 geometry
巻
20
ページ
57 - 108
発行年
1993-03
会議概要（会議名, 開催地, 会期, 主催者等）
航空宇宙技術研究所 10-12 Jun. 1992 東京 日本
会議概要（会議名, 開催地, 会期, 主催者等）（英）
National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan
In the first part of this paper, description of 3D Problem is given. It consists of Problem A, B and C, concerning flow analysis around ONERA (Office National d'Etudes et de Recherches Aerospatiales) M5 configuration. Problem A is to compute the flow at freestream conditions of Mach number, 0.84, Reynolds number, 1 x 10(exp 6) and angle of attack, alpha = -1 deg, with free transition condition. Problem B is to compute the flow at freestream conditions of Much number, 0.84, Reynolds number, 6 x 10(exp 7) and angle of attack. alpha = -1 deg. with full turbulence condition. Problem C is to compute the aerodynamic characteristics of the model at freestream conditions of Mach number, 0.84, Reynolds number, 2 x 10(exp 6) and angles of attack, alpha = -3, -2, and -1 deg, and to make plots of C(sub L) - alpha, C(sub L) - C(sub D), and C(sub L) - C(sub M) curves. The output formats are specified for all computed results. Together with given problems, this subsidiary includes a collection of five papers which are presented by applicants as the analysis results of three dimensional aerodynamic problems.
3次元部門課題:ONERA M5全機形態まわりの流れの解析
nalsp0020016.pdf
(4.04MB)
