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  1. S

    Need help finding out whether a specified dimension wings can generate enough lift

    I am designing a STOL aircraft of Length 12ft Height 5-6ft. Wingspan 15ft Wing Breadth 2.6ft Wing Area 39sqft Aspect Ratio 5.77 The wing design will be rectangular. And the aircraft is a scaled down version of the DRACO (modified Wilga 2000). Can the wings generate enough lift to carry about...
  2. A

    Research into increasing lift without increasing wing dimensions?

    Is anyone aware of any research into increasing lift without increasing wing dimensions? I am thinking maybe along the line of micro-structures and other tricks in material types. There might not be any, but I thought I would see if anyone has come across any interesting tidbits.
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