Transonic Flow Calculation around NACA-0012

Material type: 文書・図像類

Author: サキャ, アンデイエカほか

Publisher: 航空宇宙技術研究所

Publication date: 1991-12

Material Format: Digital

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Note (General)：: Two turbulence models have been used to simulate a typical flow around NACA-0012 at zero angle of attack. Those turbulence models are the Cebeci-Smith...

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Material Type: 文書・図像類
Title: Transonic Flow Calculation around NACA-0012
Author/Editor: サキャ, アンデイエカ
中村, 佳朗
保原, 充
Sakya, Andi Eka
Nakamura, Yoshiaki
Yasuhara, Michiru
Author Heading: サキャ, アンデイエカ
中村, 佳朗
保原, 充
Sakya, Andi Eka
Nakamura, Yoshiaki
Yasuhara, Michiru
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1991-12
Publication Date (W3CDTF): 1991-12
Alternative Title: NACA-0012翼周りの遷音速流の計算
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-16
No. or year of volume/issue: 16
Volume: 16
Pages: 177-184
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: eng
Target Audience: 一般
Note (General): Two turbulence models have been used to simulate a typical flow around NACA-0012 at zero angle of attack. Those turbulence models are the Cebeci-Smith Model (CSM) and the Baldwin-Lomax Model (BLM). Analysis of these models in terms of turbulent boundary layer has also been carried out in which the differences in the predicted turbulent characteristics are made clear. The computed result is compared with the experimental data obtained from the transonic tunnel at Nagoya University.
資料番号: NALSP0016028
レポート番号: NAL SP-16
Access Restrictions: 限定公開
Periodical Title (NCID): AN10097345
https://ci.nii.ac.jp/ncid/AN10097345
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ