Function File: clq = calcwing (wing, varargin)

Runs the automatic calculation of a wing's aerodynamic characteristics for a whole range of angles of attack. The wing argument specifies the wing geometry (as returned from makewing), and any following arguments must be in "option name", option_value pairs. Valid options are:

• "start" Initial angle of attack (0)
• "limit" Maximum angle of attack (22)
• "psep" The minimum past-separation local angle to terminate (0)
• "sstep" Initial angle step (0.5)
• "mstep" Minimum angle step (1e-2)
• "maxit" Maximum number of corrector iterations (250)
• "minit" Minimum number of corrector iterations (4)
• "tol" Minimum tolerance to achieve in corrector.
• "silent" Suppress verbose output (false)
• "use_fsolve" Use fsolve as a corrector (false) (experimental).