Table 5 Maximum, minimum, and range of L/D and Integral of APL
From: A Parametric study on the effects of winglet cant angle on wing aerodynamics and aeroacoustics
Parameter | Maximum | Minimum | Range |
|---|---|---|---|
L/D | \(1.79\times 10^1\) | \(2.23\times 10^0\) | \(1.56\times 10^1\) |
Integral of APL | \(5.81\times 10^3\) | \(1.11\times 10^4\) | \(5.30\times 10^3\) |
