Three-Dimensional Wing Flow Computations Using Implicit Weno Euler Solvers | Zendy

JawYen Yang | Zendy; RueyHor Yen | Zendy; Yeu-Ching Perng | Zendy

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Three-Dimensional Wing Flow Computations Using Implicit Weno Euler Solvers

Author(s) -

JawYen Yang,

RueyHor Yen,

Yeu-Ching Perng

Publication year - 2002

Publication title -

journal of aircraft

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.64

H-Index - 94

eISSN - 1533-3868

pISSN - 0021-8669

DOI - 10.2514/2.2913

Subject(s) - wing , computation , euler's formula , euler equations , flow (mathematics) , computational fluid dynamics , aerodynamics , computer science , potential flow , mechanics , mathematics , aerospace engineering , physics , mathematical analysis , engineering , algorithm

ENGINEERING NOTES are short manuscripts describing new developments or important results of a preliminary nature. These Notes cannot exceed 6 manuscript pages and 3 gures; a page of text may be substituted for a gure and vice versa. After informal review by the editors, they may be published within a few months of the date of receipt. Style requirements are the same as for regular contributions (see inside back cover).

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