文献
J-GLOBAL ID:201702278493169831
整理番号:17A1453343
ガスタービンのための翼前縁モデルの複合角フィルム冷却に関する数値シミュレーション【Powered by NICT】
Numerical simulation on film cooling with compound angle of blade leading edge model for gas turbine
著者 (5件):
Gao Wen-jing
(School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi’an 710072, China)
,
Yue Zhu-feng
(School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi’an 710072, China)
,
Li Lei
(School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi’an 710072, China)
,
Zhao Zhe-nan
(School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi’an 710072, China)
,
Tong Fu-juan
(School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi’an 710072, China)
資料名:
International Journal of Heat and Mass Transfer
(International Journal of Heat and Mass Transfer)
巻:
115
号:
PA
ページ:
839-855
発行年:
2017年
JST資料番号:
C0390A
ISSN:
0017-9310
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
イギリス (GBR)
言語:
英語 (EN)