Unswept Wings: lift and induced drag coefficients (calculation)
Calculation template
[navalapp_app charts=’lifting_line’ tabs=’yes’ delft=’no’ overview=’no’ aero=’no’ wing=’yes’ calculate_button=’yes’ levels=’1,2,6,3,4,5′]
How does it work?
This calculation template uses Prandtl’s classical Lifting-line Theory.
All the results are available for angles of attack from 0 to 15 degrees and are presented in chart and table formats:
- Wing / Appendage coefficients: CL, CDi, e (Oswald’s efficiency factor);
Standalone wing (Gap = Yes)
Wing attached to a solid surface (Gap = No)
See also:
- Unswept Wings: coefficients and forces (calculation).
- Unswept Wings: coefficients, forces, circulation, lift per unit span, and downwash (calculation).
References:
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