Warning: include(../../includes/header.inc): failed to open stream: No such file or directory in /opt/bitnami/apache/htdocs/support-site/wct/api/WindTurbineHeaders/IGormontHeader.php on line 7

Warning: include(): Failed opening '../../includes/header.inc' for inclusion (include_path='.:/opt/bitnami/php/lib/php') in /opt/bitnami/apache/htdocs/support-site/wct/api/WindTurbineHeaders/IGormontHeader.php on line 7

IGormont:

--------------------------------------------------------------------------
   Improved Gormont Dynamic Stall Model.
   Obtain blade lift, drag and moment coefficients.
--------------------------------------------------------------------------
   Form:
   [CL, CD, CM] = IGormont( af, bld, Reb, alpha, alphadot, W )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   af               (1,1)   Airfoil data structure
                            .reCL    (1,:) Reynolds number
                            .alphaCL (1,:) Angle of attack (deg)
                            .cL      (:,:) Lift coefficient
                            .reCD    (1,:) Drag Reynolds number
                            .alphaCD (1,:) Angle of attack (deg)
                            .cD      (:,:) Drag coefficient
                            .reCM    (1,:) Reynolds number
                            .alphaCM (1,:) Angle of attack (deg)
                            .cM      (:,:) Moment coefficient
                            .alpha0  (1,1) Angle of atack for zero lift
   bld              (1,1)   Blade data structure
                            .c       (1,1) Chord (m)
                            .H       (1,1) Blade half length (m)
                            .thknss  (1,1) Blade thickness (m)
   Reb              (1,1)   Blade Reynolds number
   alpha            (1,1)   Angle of attack (rad)
   alphadot         (1,1)   Angle of attack rate (rad/s)
   W                (1,1)   Relative wind speed (m/s)

   -------
   Outputs
   -------
   CL            (1,1)      Blade lift coefficient
   CD            (1,1)      Blade drag coefficient
   CM            (1,1)      Blade moment coefficient

--------------------------------------------------------------------------
	Reference: Gormont, R. E., "A Mathematical Model of Unsteady
              Aerodynamics and Radial Flow for Application to Helicopter
              Rotors," US Army Air Mobility R&D Lab, Report on Boeing-
              Vertol Contract DAAJ02-71-C-0045, May 1973.
--------------------------------------------------------------------------

Warning: include(../../includes/footer.inc): failed to open stream: No such file or directory in /opt/bitnami/apache/htdocs/support-site/wct/api/WindTurbineHeaders/IGormontHeader.php on line 61

Warning: include(): Failed opening '../../includes/footer.inc' for inclusion (include_path='.:/opt/bitnami/php/lib/php') in /opt/bitnami/apache/htdocs/support-site/wct/api/WindTurbineHeaders/IGormontHeader.php on line 61