JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
64672021.pdf1.07 MB
titleヘリコプタの流れ場解析におけるSLAUスキームの適用
Other TitleApplication of SLAU Scheme to Helicopter CFD
Author(jpn)田辺, 安忠; 齊藤, 茂; 大谷, 一平
Author(eng)Tanabe, Yasutada; Saito, Shigeru; Otani, Ippei
Author Affiliation(jpn)宇宙航空研究開発機構; 宇宙航空研究開発機構; 東京ビジネスサービス
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Tokyo Business Service
Issue Date2010-02-26
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication titleJAXA special publication: Proceedings fo 41st Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2009
宇宙航空研究開発機構特別資料: 第41回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2009論文集
VolumeJAXA-SP-09-011
Publication date2010-02-26
Languagejpn
eng
AbstractThe flowfield around a helicopter is generally very complicated. Unsteady flow regions where the dominant flow velocities ranging from the very slow to the transonic co-exist, cause computational difficulties for numerical schemes without pre-conditioning treatment. An efficient and robust all-speed scheme SLAU is incorporated into a moving overlapping grids approach and a new CFD code named rFlow (rotor Flow solver) is developed. Comparisons and validations of the new CFD code are performed and advantageous results are obtained. The capability of this new code is shown with samples of complicated flowfields around rotary wings.
DescriptionOriginal contains color illustrations
Meeting Information: 18 June-19 June, 2009, Japan Aerospace Exploration Agency
形態: カラー図版あり
会議情報: 平成21年6月18-19日. 宇宙航空研究開発機構調布航空宇宙センター
Document TypeConference Paper
JAXA Category特別資料
ISSN1349-113X
NCIDAA11609371
SHI-NOAA0064672021
Report NoJAXA-SP-09-011
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/13804


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