文献
J-GLOBAL ID:202102277262467493
整理番号:21A3221261
ファンブレード境界層遷移とプロファイル損失に及ぼす表面うねりの影響-第2部:実験的評価と応用【JST・京大機械翻訳】
Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss-Part II: Experimental Assessments and Applications
著者 (6件):
Lee Jinwook
(Gas Turbine Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139)
,
Ramaswamy Vaishnavi
(Gas Turbine Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139)
,
Spakovszky Zoltan S.
(Gas Turbine Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139)
,
Greitzer Edward M.
(Gas Turbine Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139)
,
Drela Mark
(Gas Turbine Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139)
,
Talbotec Jerome
(Safran Aircraft Engines Etablissement de Villaroche sud Rond-point Rene Ravaud - Reau, 77550 Moissy-Cramayel CEDEX, France)
資料名:
Journal of Turbomachinery
(Journal of Turbomachinery)
巻:
144
号:
2
ページ:
Null
発行年:
2022年
JST資料番号:
D0839B
ISSN:
0889-504X
CODEN:
JOTUEI
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
アメリカ合衆国 (USA)
言語:
英語 (EN)