失速(流体力学)
升力系数
俯仰力矩
自由流
攻角
阻力系数
Chord(对等)
压力系数
马赫数
雷诺数
动压
升阻比
物理
Lift(数据挖掘)
计算机科学
阻力
空气动力学
机械
数学
几何学
分布式计算
湍流
数据挖掘
出处
期刊:Journal of Aircraft
[American Institute of Aeronautics and Astronautics]
日期:1988-01-01
卷期号:25 (1): 6-17
被引量:705
摘要
Nomenclature c = chord CD =drag coefficient, D/qA CL =lift coefficient, L/qa CP = pressure coefficient, P-PW /q CM = pitching-moment coefficient, M/qA D =drag, Ib k = reduced frequency, wc/2U L =lift, Ib M =Mach number; pitching moment, ft-lb P = pressure, lb/in. q = dynamic pressure, 1 /2p U R, Re, Re, Rn = Reynolds number t time U,V = freestream velocity, ft/s x = distance a. = angle of attack, deg f =nondimensional chord length, x/c $tr transition location co = rotational frequency, rad/s p = density, lb/ft A = sweep angle, deg
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