[airplane_geometry]wing_area = 317.

[airplane_geometry]wing_area = 317.36 //Square feetwing_span = 43.608 //Feetwing_root_chord = 4.86 //Feetwing_dihedral = 1.0 //Degreeswing_incidence = 2.0 //Degreeswing_twist = 0.0 //Degreesoswald_efficiency_factor= 1.0 //Measure of lift effeciency of wing (Artificially high for biplanes)wing_winglets_flag = 0 //Are winglets available?wing_sweep = 0.0 //Degrees, wing leading edgewing_pos_apex_lon = 0.85 //Feet, longitudinal distance from reference point, negative going aftwing_pos_apex_vert = 1.4 //Feet, vertical distance from reference point, positive going uphtail_area = 56.0 //Square feethtail_span = 9.6 //Feethtail_pos_lon = -16.6 //Feet, longitudinal distance from reference point, negative going afthtail_pos_vert = -1.1 //Feet, vertical distance from reference point, positive going uphtail_incidence = 0.0 //Degreeshtail_sweep = 0.0 //Degrees, horizontal tail leading edgevtail_area = 15.0 //Square feetvtail_span = 6.0 //Feet, tip to bodyvtail_sweep = 39.0 //Degrees, vertical tail leading edgevtail_pos_lon = -18.9 //Feet, longitudinal distance from reference point, negative going aftvtail_pos_vert = 1.4 //Feet, vertical distance from reference point, positive going upelevator_area = 20.0 //Square feetaileron_area = 37.3 //Square feetrudder_area = 11.8 //Square feetelevator_up_limit = 30.0 //Degreeselevator_down_limit = 20.0 //Degreesaileron_up_limit = 20.0 //Degreesaileron_down_limit = 20.0 //Degreesrudder_limit = 25.0 //Degreeselevator_trim_limit = 0.0 //Degreesspoiler_limit = 0.0 //Degreesspoilerons_available = 0 //Spoilerons Available?aileron_to_spoileron_gain = 0 //Aileron to spoileron gainmin_ailerons_for_spoilerons = 0 //Degreesmin_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activateauto_spoiler_available=0positive_g_limit_flaps_up=4.000000positive_g_limit_flaps_down=2.000000negative_g_limit_flaps_up=-1.500000negative_g_limit_flaps_down=-1.500000