from __future__ import division # let 5/2 = 2.5 rather than 2 from scalar.units import LBF, SEC, ARCDEG, FT, IN, SLUG from scalar.units import AsUnit from Aerothon.ACWing import ACMainWing from Aerothon.DefaultMaterialsLibrary import PinkFoam, Monokote, Basswood, Balsa from Aerothon.ACWingWeight import ACSolidWing, ACRibWing # # Create the wing # Wing = ACMainWing(1) Wing.Lift_LO = 35 * LBF Wing.V_max_climb = 65 * FT / SEC Wing.V_Stall = 35 * FT / SEC Wing.Alt_LO = 920 * FT #Wing.AR = 5.0 Wing.b = 95 * IN ############################################################################### # # Geometric properties # ############################################################################### Wing.FullWing = True #Wing.UpperWing.b = 4.5*FT #Wing.LowerWing.b = 4*FT Wing.TR = [1, 0.85, 1] Wing.Gam = [0 * ARCDEG, 0 * ARCDEG, 0 * ARCDEG]
from __future__ import division # let 5/2 = 2.5 rather than 2 from scalar.units import LBF, SEC, ARCDEG, FT, IN, SLUG, OZF, OZM from scalar.units import AsUnit from Aerothon.ACWing import ACMainWing from Aerothon.DefaultMaterialsLibrary import PinkFoam, Monokote, Basswood, Balsa, Ultracote from Aerothon.ACWingWeight import ACSolidWing, ACRibWing # # Create the wing # Wing = ACMainWing(1) Wing.Lift_LO = None Wing.b = 144 * IN Wing.V_Stall = 36 * FT / SEC Wing.S = 3117 * IN**2 #Wing.Lift_LO = 55*LBF Wing.Alt_LO = 1150 * FT #Look what it typically is in marietta during the competition Wing.V_LOstall = 1.2 #added by Brock Pleiman 10/7/13 ############################################################################### # # Geometric properties # ############################################################################### Wing.FullWing = True #Wing.UpperWing.b = 4.5*FT #Wing.LowerWing.b = 4*FT #===============================================================================
from __future__ import division # let 5/2 = 2.5 rather than 2 from scalar.units import LBF, SEC, ARCDEG, FT, IN, SLUG, OZF, OZM from scalar.units import AsUnit from Aerothon.ACWing import ACMainWing from Aerothon.DefaultMaterialsLibrary import PinkFoam, Monokote, Basswood, Balsa, Ultracote from Aerothon.ACWingWeight import ACSolidWing, ACRibWing # # Create the wing # Wing = ACMainWing(1) Wing.Lift_LO = None Wing.b = 148 * IN Wing.V_Stall = 38 * FT / SEC Wing.S = 3485 * IN**2 #Wing.Lift_LO = 55*LBF Wing.Alt_LO = 1150 * FT #Look what it typically is in marietta during the competition ############################################################################### # # Geometric properties # ############################################################################### Wing.FullWing = True #Wing.UpperWing.b = 4.5*FT #Wing.LowerWing.b = 4*FT #=============================================================================== #b=150,S=3200
from __future__ import division # let 5/2 = 2.5 rather than 2 from scalar.units import LBF, SEC, ARCDEG, FT, IN, SLUG, OZF, OZM from scalar.units import AsUnit from Aerothon.ACWing import ACMainWing from Aerothon.DefaultMaterialsLibrary import PinkFoam, Monokote, Basswood, Balsa, Ultracote from Aerothon.ACWingWeight import ACSolidWing, ACRibWing # # Create the wing # Wing = ACMainWing(1) Wing.Lift_LO = None #Initially 147 inches, changed to 105 inches (0.6 total length) Wing.b = 105 * IN #96 #Initially 38 ft/sec Wing.V_Stall = 38 * FT / SEC #From Jake's Matlab calculation # Surface Area of wing Wing.S = 2147 * IN**2 #Wing.Lift_LO = 55*LBF #Was 2000 ft since last year's was in Texas Wing.Alt_LO = 200 * FT #Lakeland, FL's elevation ############################################################################### # # Geometric properties # ############################################################################### Wing.FullWing = True #Wing.UpperWing.b = 4.5*FT