for a while i have been trying to understand the lifting line theory. this has many benefits over the basic aspect ratio corrections for the calculation of CL and CDi including:
- Non-elliptical planforms
- Twisted sections (AoA varies along span)
- Section changes along span
- Wing tips (probably - see below)
- have no nomenclature
- have errors
- after stating the method equations declare the solution too hard
- give the results for a single (not very useful) case only
- not have a worked example to compare results to.
- obviously every website has minor differences in nomenclature and assumptions
Best description of method
Example to compare your results to
Simple Matlab code
A few notes on solving Fourier terms:
- In the matlab code the line 'a=b\rhs' is matrix maths and means [An] = [b]^-1 . [RHS]
- Look up MMULT and MINVERSE in Excel help, makes solving linear equations sooo easy and makes anyone who has coded row reduction methods in excel feel stupid.
Note on wingtips analysis:
I am not sure whether this is valid or not yet. Probably valid enough for anyone satisfied with a Lifting-Line theory result.
- Design a wing with wingtips
- Fold these wingtips down so they are in plane with the wing, adding to its span
- Twist the wingtips so that they produce zero lift, independent of the wings AoA
