Skip to main content
4 of 4
grammar
quiet flyer
  • 23k
  • 5
  • 47
  • 136

How can a designer maximize the glide ratio of an aircraft with low aspect ratio wings, other than by increasing the aspect ratio?

As I understand it, the gliding range is given by a lift to drag ratio—hence to increase the gliding range, I would want to increase the lift and reduce the drag as much as possible.

To that end, apparently, it seems that high AR fits both the bills. However, does that mean that I will not able to enhance the gliding range with low AR wings at all?