Mitsubishi Heavy Industries Ltd
Japan Defense Agency Technical Research and Development Institute
Japan Defense Agency Technical Research and Development Institute
Mitsubishi Heavy Industries Ltd
Mitsubishi Heavy Industries Ltd
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory (NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory
巻
46
ページ
151 - 156
発行年
2000-12
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 7-9 Jun. 2000 東京 日本
会議概要（会議名, 開催地, 会期, 主催者等）（英）
National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan
This paper presents the applications of CASPER (Computational Aerodynamic System for Performance Evaluation and Research) to 2D (two dimensional) airfoil stall prediction, developed by TRDIJDA (Technical Research and Development Institute of Japan Defense Agency) in collaboration with domestic aircraft manufactures. The RANS (Reynolds-Averaged Navier-Stokes) computations for flows around three airfoils were carried out, which have different stall characteristics, using unstructured grid method together with Spalart-Allmaras one-equation turbulence model. The computational results show good agreement with the experimental pressure distribution and Lift coefficient for low angles of attack, and indicate the potential to predict Cl(sub max) and the angle of attack.
CASPERを用いた翼型失速特性シミュレーション
nalsp0046028.pdf
(931.4KB)
