文献
J-GLOBAL ID:202202265892923326
整理番号:22A1170590
出力ベース適応メッシュを持つ多重ソルバを用いた多要素翼流れ解の比較【JST・京大機械翻訳】
Comparing Multi-Element Airfoil Flow Solutions Using Multiple Solvers with Output-Based Adapted Meshes
著者 (12件):
Galbraith Marshall C.
(Massachusetts Institute of Technology, Cambridge, Massachusetts 02139)
,
Ursachi Carmen-Ioana
(Massachusetts Institute of Technology, Cambridge, Massachusetts 02139)
,
Chandel Durgesh
(Massachusetts Institute of Technology, Cambridge, Massachusetts 02139)
,
Allmaras Steven R.
(Massachusetts Institute of Technology, Cambridge, Massachusetts 02139)
,
Darmofal David L.
(Massachusetts Institute of Technology, Cambridge, Massachusetts 02139)
,
Glasby Ryan S.
(University of Tennessee, Knoxville, Tennessee 37996)
,
Stefanski Douglas L.
(University of Tennessee, Knoxville, Tennessee 37996)
,
Taylor Erwin J.
(University of Tennessee, Knoxville, Tennessee 37996)
,
Holst Kevin R.
(University of Tennessee, Knoxville, Tennessee 37996)
,
Hereth Ethan A.
(University of Tennessee, Knoxville, Tennessee 37996)
,
Mukhopadhaya Jayant
(Stanford University, Stanford, California 94305)
,
Alonso Juan J.
(Stanford University, Stanford, California 94305)
資料名:
AIAA Journal (American Institute of Aeronautics and Astronautics)
(AIAA Journal (American Institute of Aeronautics and Astronautics))
巻:
60
号:
4
ページ:
2629-2643
発行年:
2022年
JST資料番号:
C0248C
ISSN:
1533-385X
CODEN:
AIAJAH
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)