Recent content by cueca

you mean asymmetrical lift distribution without any ailerons or asymmetrical flaps deflected? (Still a symmetrical geometry but only a sideslip angle occurs) Or you mean a deformation on lift distribution due to ailerons deflected. This two models are different. Have you visualised your lift...

try NACA report 1269 by M. J. QUEIJO you may find it on ntrs.nasa.gov if it doent suits you, look to the reference page of the report. Report uses 1 chordwise panel vortex lattice method (may be said as numerical lifting line method , but lifting line can be swept.) You will have to find the...

before coding, i suggest some supplementary books or Reports * Katz, Plotkin. "Low speed aerodynamics" -for theory * Galuert, "elements of airfoil and airscrew theory" -basic book * James C. sivells, Robert H. Nelly "Method for calculating wing characteristics by ligting-line theory using...