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翻訳と辞書　辞書検索 [ 開発暫定版 ] スポンサード リンク Lift coefficient ： ウィキペディア英語版 Lift coefficient The lift coefficient (CL, CN or Cz) is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. A lifting body is a foil or a complete foil-bearing body such as a fixed-wing aircraft. ''C''L is a function of the angle of the body to the flow, its Reynold number and its Mach number. The lift coefficient ''c''l refers to the dynamic lift characteristics of a two-dimensional foil section, with the reference area replaced by the foil chord.〔Abbott, Ira H., and Doenhoff, Albert E. von: ''Theory of Wing Sections''. Section 1.2〕 ==Definition of the lift coefficient ''C''L== The lift coefficient ''C''L is defined by〔〔Clancy, L. J.: ''Aerodynamics''. Section 4.15〕 :$C\_\backslash mathrm\; L\; =\; \backslash rho\; v^2S\}\}\; =\; \}\; =\; \backslash frac$ , where $L\backslash ,$ is the lift force, $\backslash rho\backslash ,$ is fluid density, $v\backslash ,$ is true airspeed, $S\backslash ,$ is the relevant plan area and $q\backslash ,$ is the fluid dynamic pressure. The lift coefficient can be approximated using the lifting-line theory,〔Clancy, L. J.: ''Aerodynamics''. Section 8.11〕 numerically calculated or measured in a wind tunnel test of a complete aircraft configuration. 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Lift coefficient」の詳細全文を読む スポンサード リンク 翻訳と辞書 : 翻訳のためのインターネットリソース Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.