! ------------ AirfoilInfo v1.00.x Input File ---------------------------------- ! Sample airfoil data ! Individual tables must include alpha from -180 to 180 degrees. ! Multiple tables should contain the same quantity and values for Alpha, and the secondary parameter must be monotonically increasing. ! ------------------------------------------------------------------------------ 1 InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default = 3] 1.0 NonDimArea ! Non-dimensional area of the airfoil (area/chord^2) (Set to 1.0 if unsure or unneeded) 0 NumCoords ! Number of coordinates in the airfoil shape file. Set to zero if not included. 4 NumTabs ! Number of airfoil tables in this file. Each table must have lines for Re and Ctrl. ! ------------------------------------------------------------------------------ ! data for Table 1 ! ------------------------------------------------------------------------------ 5687500 Re ! Reynolds number in millions. -0.349066 Ctrl ! Control setting False InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefs below this line. !........................................ ! Table of aerodynamic coefficients. 181 NumAlf ! Number of data lines in the following CoeffData table ! Alpha Cl Cd Cm ! (deg) (-) (-) (-) -180.0 -2.95975 0.67098 0.00000 -178.0 -2.95464 0.56489 0.00000 -176.0 -2.94953 0.46819 0.00000 -174.0 -2.94442 0.38094 0.00000 -172.0 -2.93931 0.30317 0.00000 -170.0 -2.93420 0.23485 0.00000 -168.0 -2.92910 0.17592 0.00000 -166.0 -2.92399 0.12626 0.00000 -164.0 -2.91888 0.08572 0.00000 -162.0 -2.91377 0.05412 0.00000 -160.0 -2.90866 0.03121 0.00000 -158.0 -2.90355 0.01674 0.00000 -156.0 -2.89845 0.01038 0.00000 -154.0 -2.89334 0.01179 0.00000 -152.0 -2.88823 0.02062 0.00000 -150.0 -2.88312 0.03644 0.00000 -148.0 -2.87801 0.05883 0.00000 -146.0 -2.87290 0.08734 0.00000 -144.0 -2.86780 0.12148 0.00000 -142.0 -2.86269 0.16076 0.00000 -140.0 -2.85758 0.20467 0.00000 -138.0 -2.85247 0.25267 0.00000 -136.0 -2.84736 0.30422 0.00000 -134.0 -2.84225 0.35879 0.00000 -132.0 -2.83715 0.41581 0.00000 -130.0 -2.83204 0.47473 0.00000 -128.0 -2.82693 0.53501 0.00000 -126.0 -2.82182 0.59608 0.00000 -124.0 -2.81671 0.65742 0.00000 -122.0 -2.81161 0.71849 0.00000 -120.0 -2.80650 0.77877 0.00000 -118.0 -2.80139 0.83777 0.00000 -116.0 -2.79628 0.89498 0.00000 -114.0 -2.79117 0.94997 0.00000 -112.0 -2.78606 1.00228 0.00000 -110.0 -2.78096 1.05150 0.00000 -108.0 -2.77585 1.09725 0.00000 -106.0 -2.77074 1.13917 0.00000 -104.0 -2.76563 1.17694 0.00000 -102.0 -2.76052 1.21028 0.00000 -100.0 -2.75541 1.23892 0.00000 -98.0 -2.75031 1.26266 0.00000 -96.0 -2.74520 1.28131 0.00000 -94.0 -2.74009 1.29473 0.00000 -92.0 -2.73498 1.30282 0.00000 -90.0 -2.72987 1.30553 0.00000 -88.0 -2.72476 1.30282 0.00000 -86.0 -2.71966 1.29473 0.00000 -84.0 -2.71455 1.28131 0.00000 -82.0 -2.70944 1.26266 0.00000 -80.0 -2.70433 1.23892 0.00000 -78.0 -2.69922 1.21028 0.00000 -76.0 -2.69411 1.17694 0.00000 -74.0 -2.68901 1.13917 0.00000 -72.0 -2.68390 1.09725 0.00000 -70.0 -2.67879 1.05150 0.00000 -68.0 -2.67368 1.00228 0.00000 -66.0 -2.66857 0.94997 0.00000 -64.0 -2.66346 0.89498 0.00000 -62.0 -2.65836 0.83777 0.00000 -60.0 -2.65325 0.77877 0.00000 -58.0 -2.64814 0.71849 0.00000 -56.0 -2.64303 0.65742 0.00000 -54.0 -2.63792 0.59608 0.00000 -52.0 -2.63282 0.53501 0.00000 -50.0 -2.62771 0.47473 0.00000 -48.0 -2.62260 0.41581 0.00000 -46.0 -2.61749 0.35879 0.00000 -44.0 -2.61238 0.30422 0.00000 -42.0 -2.60727 0.25267 0.00000 -40.0 -2.60217 0.20467 0.00000 -38.0 -2.59706 0.16076 0.00000 -36.0 -2.59195 0.12148 0.00000 -34.0 -2.58684 0.08734 0.00000 -32.0 -2.58173 0.05883 0.00000 -30.0 -2.57662 0.03644 0.00000 -28.0 -2.57152 0.02062 0.00000 -26.0 -2.56641 0.01179 0.00000 -24.0 -2.56130 0.01038 0.00000 -22.0 -2.55619 0.01674 0.00000 -20.0 -2.55108 0.03121 0.00000 -18.0 -2.54597 0.05412 0.00000 -16.0 -2.54087 0.08572 0.00000 -14.0 -2.46608 0.01000 0.00000 -12.0 -2.25664 0.01000 0.00000 -10.0 -2.04720 0.01000 0.00000 -8.0 -1.83776 0.01000 0.00000 -6.0 -1.62832 0.01000 0.00000 -4.0 -1.41888 0.01000 0.00000 -2.0 -1.20944 0.01000 0.00000 0.0 -1.00000 0.01000 0.00000 2.0 -0.79056 0.01000 0.00000 4.0 -0.58112 0.01000 0.00000 6.0 -0.37168 0.01000 0.00000 8.0 -0.16224 0.01000 0.00000 10.0 0.04720 0.01000 0.00000 12.0 0.25664 0.01000 0.00000 14.0 0.46608 0.01000 0.00000 16.0 0.67552 0.01000 0.00000 18.0 0.88496 0.01000 0.00000 20.0 1.09440 0.01000 0.00000 22.0 1.30383 0.01000 0.00000 24.0 1.51327 0.01000 0.00000 26.0 1.72271 0.01000 0.00000 28.0 1.93215 0.01000 0.00000 30.0 2.14159 0.01000 0.00000 32.0 2.35103 0.01000 0.00000 34.0 2.58684 0.08734 0.00000 36.0 2.59195 0.12148 0.00000 38.0 2.59706 0.16076 0.00000 40.0 2.60217 0.20467 0.00000 42.0 2.60727 0.25267 0.00000 44.0 2.61238 0.30422 0.00000 46.0 2.61749 0.35879 0.00000 48.0 2.62260 0.41581 0.00000 50.0 2.62771 0.47473 0.00000 52.0 2.63282 0.53501 0.00000 54.0 2.63792 0.59608 0.00000 56.0 2.64303 0.65742 0.00000 58.0 2.64814 0.71849 0.00000 60.0 2.65325 0.77877 0.00000 62.0 2.65836 0.83777 0.00000 64.0 2.66346 0.89498 0.00000 66.0 2.66857 0.94997 0.00000 68.0 2.67368 1.00228 0.00000 70.0 2.67879 1.05150 0.00000 72.0 2.68390 1.09725 0.00000 74.0 2.68901 1.13917 0.00000 76.0 2.69411 1.17694 0.00000 78.0 2.69922 1.21028 0.00000 80.0 2.70433 1.23892 0.00000 82.0 2.70944 1.26266 0.00000 84.0 2.71455 1.28131 0.00000 86.0 2.71966 1.29473 0.00000 88.0 2.72476 1.30282 0.00000 90.0 2.72987 1.30553 0.00000 92.0 2.73498 1.30282 0.00000 94.0 2.74009 1.29473 0.00000 96.0 2.74520 1.28131 0.00000 98.0 2.75031 1.26266 0.00000 100.0 2.75541 1.23892 0.00000 102.0 2.76052 1.21028 0.00000 104.0 2.76563 1.17694 0.00000 106.0 2.77074 1.13917 0.00000 108.0 2.77585 1.09725 0.00000 110.0 2.78096 1.05150 0.00000 112.0 2.78606 1.00228 0.00000 114.0 2.79117 0.94997 0.00000 116.0 2.79628 0.89498 0.00000 118.0 2.80139 0.83777 0.00000 120.0 2.80650 0.77877 0.00000 122.0 2.81161 0.71849 0.00000 124.0 2.81671 0.65742 0.00000 126.0 2.82182 0.59608 0.00000 128.0 2.82693 0.53501 0.00000 130.0 2.83204 0.47473 0.00000 132.0 2.83715 0.41581 0.00000 134.0 2.84225 0.35879 0.00000 136.0 2.84736 0.30422 0.00000 138.0 2.85247 0.25267 0.00000 140.0 2.85758 0.20467 0.00000 142.0 2.86269 0.16076 0.00000 144.0 2.86780 0.12148 0.00000 146.0 2.87290 0.08734 0.00000 148.0 2.87801 0.05883 0.00000 150.0 2.88312 0.03644 0.00000 152.0 2.88823 0.02062 0.00000 154.0 2.89334 0.01179 0.00000 156.0 2.89845 0.01038 0.00000 158.0 2.90355 0.01674 0.00000 160.0 2.90866 0.03121 0.00000 162.0 2.91377 0.05412 0.00000 164.0 2.91888 0.08572 0.00000 166.0 2.92399 0.12626 0.00000 168.0 2.92910 0.17592 0.00000 170.0 2.93420 0.23485 0.00000 172.0 2.93931 0.30317 0.00000 174.0 2.94442 0.38094 0.00000 176.0 2.94953 0.46819 0.00000 178.0 2.95464 0.56489 0.00000 180.0 -2.95975 0.67098 0.00000 ! ------------------------------------------------------------------------------ ! data for Table 2 ! ------------------------------------------------------------------------------ 5687500 Re ! Reynolds number in millions. -0.174533 Ctrl ! Control setting False InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefs below this line. !........................................ ! Table of aerodynamic coefficients. 181 NumAlf ! Number of data lines in the following CoeffData table ! Alpha Cl Cd Cm ! (deg) (-) (-) (-) -180.0 -2.95975 0.67098 0.00000 -178.0 -2.95464 0.56489 0.00000 -176.0 -2.94953 0.46819 0.00000 -174.0 -2.94442 0.38094 0.00000 -172.0 -2.93931 0.30317 0.00000 -170.0 -2.93420 0.23485 0.00000 -168.0 -2.92910 0.17592 0.00000 -166.0 -2.92399 0.12626 0.00000 -164.0 -2.91888 0.08572 0.00000 -162.0 -2.91377 0.05412 0.00000 -160.0 -2.90866 0.03121 0.00000 -158.0 -2.90355 0.01674 0.00000 -156.0 -2.89845 0.01038 0.00000 -154.0 -2.89334 0.01179 0.00000 -152.0 -2.88823 0.02062 0.00000 -150.0 -2.88312 0.03644 0.00000 -148.0 -2.87801 0.05883 0.00000 -146.0 -2.87290 0.08734 0.00000 -144.0 -2.86780 0.12148 0.00000 -142.0 -2.86269 0.16076 0.00000 -140.0 -2.85758 0.20467 0.00000 -138.0 -2.85247 0.25267 0.00000 -136.0 -2.84736 0.30422 0.00000 -134.0 -2.84225 0.35879 0.00000 -132.0 -2.83715 0.41581 0.00000 -130.0 -2.83204 0.47473 0.00000 -128.0 -2.82693 0.53501 0.00000 -126.0 -2.82182 0.59608 0.00000 -124.0 -2.81671 0.65742 0.00000 -122.0 -2.81161 0.71849 0.00000 -120.0 -2.80650 0.77877 0.00000 -118.0 -2.80139 0.83777 0.00000 -116.0 -2.79628 0.89498 0.00000 -114.0 -2.79117 0.94997 0.00000 -112.0 -2.78606 1.00228 0.00000 -110.0 -2.78096 1.05150 0.00000 -108.0 -2.77585 1.09725 0.00000 -106.0 -2.77074 1.13917 0.00000 -104.0 -2.76563 1.17694 0.00000 -102.0 -2.76052 1.21028 0.00000 -100.0 -2.75541 1.23892 0.00000 -98.0 -2.75031 1.26266 0.00000 -96.0 -2.74520 1.28131 0.00000 -94.0 -2.74009 1.29473 0.00000 -92.0 -2.73498 1.30282 0.00000 -90.0 -2.72987 1.30553 0.00000 -88.0 -2.72476 1.30282 0.00000 -86.0 -2.71966 1.29473 0.00000 -84.0 -2.71455 1.28131 0.00000 -82.0 -2.70944 1.26266 0.00000 -80.0 -2.70433 1.23892 0.00000 -78.0 -2.69922 1.21028 0.00000 -76.0 -2.69411 1.17694 0.00000 -74.0 -2.68901 1.13917 0.00000 -72.0 -2.68390 1.09725 0.00000 -70.0 -2.67879 1.05150 0.00000 -68.0 -2.67368 1.00228 0.00000 -66.0 -2.66857 0.94997 0.00000 -64.0 -2.66346 0.89498 0.00000 -62.0 -2.65836 0.83777 0.00000 -60.0 -2.65325 0.77877 0.00000 -58.0 -2.64814 0.71849 0.00000 -56.0 -2.64303 0.65742 0.00000 -54.0 -2.63792 0.59608 0.00000 -52.0 -2.63282 0.53501 0.00000 -50.0 -2.62771 0.47473 0.00000 -48.0 -2.62260 0.41581 0.00000 -46.0 -2.61749 0.35879 0.00000 -44.0 -2.61238 0.30422 0.00000 -42.0 -2.60727 0.25267 0.00000 -40.0 -2.60217 0.20467 0.00000 -38.0 -2.59706 0.16076 0.00000 -36.0 -2.59195 0.12148 0.00000 -34.0 -2.58684 0.08734 0.00000 -32.0 -2.58173 0.05883 0.00000 -30.0 -2.57662 0.03644 0.00000 -28.0 -2.57152 0.02062 0.00000 -26.0 -2.56641 0.01179 0.00000 -24.0 -2.56130 0.01038 0.00000 -22.0 -2.55619 0.01674 0.00000 -20.0 -2.55108 0.03121 0.00000 -18.0 -2.38496 0.01000 0.00000 -16.0 -2.17552 0.01000 0.00000 -14.0 -1.96608 0.01000 0.00000 -12.0 -1.75664 0.01000 0.00000 -10.0 -1.54720 0.01000 0.00000 -8.0 -1.33776 0.01000 0.00000 -6.0 -1.12832 0.01000 0.00000 -4.0 -0.91888 0.01000 0.00000 -2.0 -0.70944 0.01000 0.00000 0.0 -0.50000 0.01000 0.00000 2.0 -0.29056 0.01000 0.00000 4.0 -0.08112 0.01000 0.00000 6.0 0.12832 0.01000 0.00000 8.0 0.33776 0.01000 0.00000 10.0 0.54720 0.01000 0.00000 12.0 0.75664 0.01000 0.00000 14.0 0.96608 0.01000 0.00000 16.0 1.17552 0.01000 0.00000 18.0 1.38496 0.01000 0.00000 20.0 1.59440 0.01000 0.00000 22.0 1.80383 0.01000 0.00000 24.0 2.01327 0.01000 0.00000 26.0 2.22271 0.01000 0.00000 28.0 2.43215 0.01000 0.00000 30.0 2.57662 0.03644 0.00000 32.0 2.58173 0.05883 0.00000 34.0 2.58684 0.08734 0.00000 36.0 2.59195 0.12148 0.00000 38.0 2.59706 0.16076 0.00000 40.0 2.60217 0.20467 0.00000 42.0 2.60727 0.25267 0.00000 44.0 2.61238 0.30422 0.00000 46.0 2.61749 0.35879 0.00000 48.0 2.62260 0.41581 0.00000 50.0 2.62771 0.47473 0.00000 52.0 2.63282 0.53501 0.00000 54.0 2.63792 0.59608 0.00000 56.0 2.64303 0.65742 0.00000 58.0 2.64814 0.71849 0.00000 60.0 2.65325 0.77877 0.00000 62.0 2.65836 0.83777 0.00000 64.0 2.66346 0.89498 0.00000 66.0 2.66857 0.94997 0.00000 68.0 2.67368 1.00228 0.00000 70.0 2.67879 1.05150 0.00000 72.0 2.68390 1.09725 0.00000 74.0 2.68901 1.13917 0.00000 76.0 2.69411 1.17694 0.00000 78.0 2.69922 1.21028 0.00000 80.0 2.70433 1.23892 0.00000 82.0 2.70944 1.26266 0.00000 84.0 2.71455 1.28131 0.00000 86.0 2.71966 1.29473 0.00000 88.0 2.72476 1.30282 0.00000 90.0 2.72987 1.30553 0.00000 92.0 2.73498 1.30282 0.00000 94.0 2.74009 1.29473 0.00000 96.0 2.74520 1.28131 0.00000 98.0 2.75031 1.26266 0.00000 100.0 2.75541 1.23892 0.00000 102.0 2.76052 1.21028 0.00000 104.0 2.76563 1.17694 0.00000 106.0 2.77074 1.13917 0.00000 108.0 2.77585 1.09725 0.00000 110.0 2.78096 1.05150 0.00000 112.0 2.78606 1.00228 0.00000 114.0 2.79117 0.94997 0.00000 116.0 2.79628 0.89498 0.00000 118.0 2.80139 0.83777 0.00000 120.0 2.80650 0.77877 0.00000 122.0 2.81161 0.71849 0.00000 124.0 2.81671 0.65742 0.00000 126.0 2.82182 0.59608 0.00000 128.0 2.82693 0.53501 0.00000 130.0 2.83204 0.47473 0.00000 132.0 2.83715 0.41581 0.00000 134.0 2.84225 0.35879 0.00000 136.0 2.84736 0.30422 0.00000 138.0 2.85247 0.25267 0.00000 140.0 2.85758 0.20467 0.00000 142.0 2.86269 0.16076 0.00000 144.0 2.86780 0.12148 0.00000 146.0 2.87290 0.08734 0.00000 148.0 2.87801 0.05883 0.00000 150.0 2.88312 0.03644 0.00000 152.0 2.88823 0.02062 0.00000 154.0 2.89334 0.01179 0.00000 156.0 2.89845 0.01038 0.00000 158.0 2.90355 0.01674 0.00000 160.0 2.90866 0.03121 0.00000 162.0 2.91377 0.05412 0.00000 164.0 2.91888 0.08572 0.00000 166.0 2.92399 0.12626 0.00000 168.0 2.92910 0.17592 0.00000 170.0 2.93420 0.23485 0.00000 172.0 2.93931 0.30317 0.00000 174.0 2.94442 0.38094 0.00000 176.0 2.94953 0.46819 0.00000 178.0 2.95464 0.56489 0.00000 180.0 -2.95975 0.67098 0.00000 ! ------------------------------------------------------------------------------ ! data for Table 3 ! ------------------------------------------------------------------------------ 5687500 Re ! Reynolds number in millions. 0 Ctrl ! Control setting False InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefs below this line. !........................................ ! Table of aerodynamic coefficients. 181 NumAlf ! Number of data lines in the following CoeffData table ! Alpha Cl Cd Cm ! (deg) (-) (-) (-) -180.0 -2.95975 0.67098 0.00000 -178.0 -2.95464 0.56489 0.00000 -176.0 -2.94953 0.46819 0.00000 -174.0 -2.94442 0.38094 0.00000 -172.0 -2.93931 0.30317 0.00000 -170.0 -2.93420 0.23485 0.00000 -168.0 -2.92910 0.17592 0.00000 -166.0 -2.92399 0.12626 0.00000 -164.0 -2.91888 0.08572 0.00000 -162.0 -2.91377 0.05412 0.00000 -160.0 -2.90866 0.03121 0.00000 -158.0 -2.90355 0.01674 0.00000 -156.0 -2.89845 0.01038 0.00000 -154.0 -2.89334 0.01179 0.00000 -152.0 -2.88823 0.02062 0.00000 -150.0 -2.88312 0.03644 0.00000 -148.0 -2.87801 0.05883 0.00000 -146.0 -2.87290 0.08734 0.00000 -144.0 -2.86780 0.12148 0.00000 -142.0 -2.86269 0.16076 0.00000 -140.0 -2.85758 0.20467 0.00000 -138.0 -2.85247 0.25267 0.00000 -136.0 -2.84736 0.30422 0.00000 -134.0 -2.84225 0.35879 0.00000 -132.0 -2.83715 0.41581 0.00000 -130.0 -2.83204 0.47473 0.00000 -128.0 -2.82693 0.53501 0.00000 -126.0 -2.82182 0.59608 0.00000 -124.0 -2.81671 0.65742 0.00000 -122.0 -2.81161 0.71849 0.00000 -120.0 -2.80650 0.77877 0.00000 -118.0 -2.80139 0.83777 0.00000 -116.0 -2.79628 0.89498 0.00000 -114.0 -2.79117 0.94997 0.00000 -112.0 -2.78606 1.00228 0.00000 -110.0 -2.78096 1.05150 0.00000 -108.0 -2.77585 1.09725 0.00000 -106.0 -2.77074 1.13917 0.00000 -104.0 -2.76563 1.17694 0.00000 -102.0 -2.76052 1.21028 0.00000 -100.0 -2.75541 1.23892 0.00000 -98.0 -2.75031 1.26266 0.00000 -96.0 -2.74520 1.28131 0.00000 -94.0 -2.74009 1.29473 0.00000 -92.0 -2.73498 1.30282 0.00000 -90.0 -2.72987 1.30553 0.00000 -88.0 -2.72476 1.30282 0.00000 -86.0 -2.71966 1.29473 0.00000 -84.0 -2.71455 1.28131 0.00000 -82.0 -2.70944 1.26266 0.00000 -80.0 -2.70433 1.23892 0.00000 -78.0 -2.69922 1.21028 0.00000 -76.0 -2.69411 1.17694 0.00000 -74.0 -2.68901 1.13917 0.00000 -72.0 -2.68390 1.09725 0.00000 -70.0 -2.67879 1.05150 0.00000 -68.0 -2.67368 1.00228 0.00000 -66.0 -2.66857 0.94997 0.00000 -64.0 -2.66346 0.89498 0.00000 -62.0 -2.65836 0.83777 0.00000 -60.0 -2.65325 0.77877 0.00000 -58.0 -2.64814 0.71849 0.00000 -56.0 -2.64303 0.65742 0.00000 -54.0 -2.63792 0.59608 0.00000 -52.0 -2.63282 0.53501 0.00000 -50.0 -2.62771 0.47473 0.00000 -48.0 -2.62260 0.41581 0.00000 -46.0 -2.61749 0.35879 0.00000 -44.0 -2.61238 0.30422 0.00000 -42.0 -2.60727 0.25267 0.00000 -40.0 -2.60217 0.20467 0.00000 -38.0 -2.59706 0.16076 0.00000 -36.0 -2.59195 0.12148 0.00000 -34.0 -2.58684 0.08734 0.00000 -32.0 -2.58173 0.05883 0.00000 -30.0 -2.57662 0.03644 0.00000 -28.0 -2.57152 0.02062 0.00000 -26.0 -2.56641 0.01179 0.00000 -24.0 -2.56130 0.01038 0.00000 -22.0 -2.30383 0.01000 0.00000 -20.0 -2.09440 0.01000 0.00000 -18.0 -1.88496 0.01000 0.00000 -16.0 -1.67552 0.01000 0.00000 -14.0 -1.46608 0.01000 0.00000 -12.0 -1.25664 0.01000 0.00000 -10.0 -1.04720 0.01000 0.00000 -8.0 -0.83776 0.01000 0.00000 -6.0 -0.62832 0.01000 0.00000 -4.0 -0.41888 0.01000 0.00000 -2.0 -0.20944 0.01000 0.00000 0.0 0.00000 0.01000 0.00000 2.0 0.20944 0.01000 0.00000 4.0 0.41888 0.01000 0.00000 6.0 0.62832 0.01000 0.00000 8.0 0.83776 0.01000 0.00000 10.0 1.04720 0.01000 0.00000 12.0 1.25664 0.01000 0.00000 14.0 1.46608 0.01000 0.00000 16.0 1.67552 0.01000 0.00000 18.0 1.88496 0.01000 0.00000 20.0 2.09440 0.01000 0.00000 22.0 2.30383 0.01000 0.00000 24.0 2.56130 0.01038 0.00000 26.0 2.56641 0.01179 0.00000 28.0 2.57152 0.02062 0.00000 30.0 2.57662 0.03644 0.00000 32.0 2.58173 0.05883 0.00000 34.0 2.58684 0.08734 0.00000 36.0 2.59195 0.12148 0.00000 38.0 2.59706 0.16076 0.00000 40.0 2.60217 0.20467 0.00000 42.0 2.60727 0.25267 0.00000 44.0 2.61238 0.30422 0.00000 46.0 2.61749 0.35879 0.00000 48.0 2.62260 0.41581 0.00000 50.0 2.62771 0.47473 0.00000 52.0 2.63282 0.53501 0.00000 54.0 2.63792 0.59608 0.00000 56.0 2.64303 0.65742 0.00000 58.0 2.64814 0.71849 0.00000 60.0 2.65325 0.77877 0.00000 62.0 2.65836 0.83777 0.00000 64.0 2.66346 0.89498 0.00000 66.0 2.66857 0.94997 0.00000 68.0 2.67368 1.00228 0.00000 70.0 2.67879 1.05150 0.00000 72.0 2.68390 1.09725 0.00000 74.0 2.68901 1.13917 0.00000 76.0 2.69411 1.17694 0.00000 78.0 2.69922 1.21028 0.00000 80.0 2.70433 1.23892 0.00000 82.0 2.70944 1.26266 0.00000 84.0 2.71455 1.28131 0.00000 86.0 2.71966 1.29473 0.00000 88.0 2.72476 1.30282 0.00000 90.0 2.72987 1.30553 0.00000 92.0 2.73498 1.30282 0.00000 94.0 2.74009 1.29473 0.00000 96.0 2.74520 1.28131 0.00000 98.0 2.75031 1.26266 0.00000 100.0 2.75541 1.23892 0.00000 102.0 2.76052 1.21028 0.00000 104.0 2.76563 1.17694 0.00000 106.0 2.77074 1.13917 0.00000 108.0 2.77585 1.09725 0.00000 110.0 2.78096 1.05150 0.00000 112.0 2.78606 1.00228 0.00000 114.0 2.79117 0.94997 0.00000 116.0 2.79628 0.89498 0.00000 118.0 2.80139 0.83777 0.00000 120.0 2.80650 0.77877 0.00000 122.0 2.81161 0.71849 0.00000 124.0 2.81671 0.65742 0.00000 126.0 2.82182 0.59608 0.00000 128.0 2.82693 0.53501 0.00000 130.0 2.83204 0.47473 0.00000 132.0 2.83715 0.41581 0.00000 134.0 2.84225 0.35879 0.00000 136.0 2.84736 0.30422 0.00000 138.0 2.85247 0.25267 0.00000 140.0 2.85758 0.20467 0.00000 142.0 2.86269 0.16076 0.00000 144.0 2.86780 0.12148 0.00000 146.0 2.87290 0.08734 0.00000 148.0 2.87801 0.05883 0.00000 150.0 2.88312 0.03644 0.00000 152.0 2.88823 0.02062 0.00000 154.0 2.89334 0.01179 0.00000 156.0 2.89845 0.01038 0.00000 158.0 2.90355 0.01674 0.00000 160.0 2.90866 0.03121 0.00000 162.0 2.91377 0.05412 0.00000 164.0 2.91888 0.08572 0.00000 166.0 2.92399 0.12626 0.00000 168.0 2.92910 0.17592 0.00000 170.0 2.93420 0.23485 0.00000 172.0 2.93931 0.30317 0.00000 174.0 2.94442 0.38094 0.00000 176.0 2.94953 0.46819 0.00000 178.0 2.95464 0.56489 0.00000 180.0 -2.95975 0.67098 0.00000 ! ------------------------------------------------------------------------------ ! data for Table 4 ! ------------------------------------------------------------------------------ 5687500 Re ! Reynolds number in millions. 0.174533 Ctrl ! Control setting False InclUAdata ! Is unsteady aerodynamics data included in this table? If TRUE, then include 30 UA coefs below this line. !........................................ ! Table of aerodynamic coefficients. 181 NumAlf ! Number of data lines in the following CoeffData table ! Alpha Cl Cd Cm ! (deg) (-) (-) (-) -180.0 -2.95975 0.67098 0.00000 -178.0 -2.95464 0.56489 0.00000 -176.0 -2.94953 0.46819 0.00000 -174.0 -2.94442 0.38094 0.00000 -172.0 -2.93931 0.30317 0.00000 -170.0 -2.93420 0.23485 0.00000 -168.0 -2.92910 0.17592 0.00000 -166.0 -2.92399 0.12626 0.00000 -164.0 -2.91888 0.08572 0.00000 -162.0 -2.91377 0.05412 0.00000 -160.0 -2.90866 0.03121 0.00000 -158.0 -2.90355 0.01674 0.00000 -156.0 -2.89845 0.01038 0.00000 -154.0 -2.89334 0.01179 0.00000 -152.0 -2.88823 0.02062 0.00000 -150.0 -2.88312 0.03644 0.00000 -148.0 -2.87801 0.05883 0.00000 -146.0 -2.87290 0.08734 0.00000 -144.0 -2.86780 0.12148 0.00000 -142.0 -2.86269 0.16076 0.00000 -140.0 -2.85758 0.20467 0.00000 -138.0 -2.85247 0.25267 0.00000 -136.0 -2.84736 0.30422 0.00000 -134.0 -2.84225 0.35879 0.00000 -132.0 -2.83715 0.41581 0.00000 -130.0 -2.83204 0.47473 0.00000 -128.0 -2.82693 0.53501 0.00000 -126.0 -2.82182 0.59608 0.00000 -124.0 -2.81671 0.65742 0.00000 -122.0 -2.81161 0.71849 0.00000 -120.0 -2.80650 0.77877 0.00000 -118.0 -2.80139 0.83777 0.00000 -116.0 -2.79628 0.89498 0.00000 -114.0 -2.79117 0.94997 0.00000 -112.0 -2.78606 1.00228 0.00000 -110.0 -2.78096 1.05150 0.00000 -108.0 -2.77585 1.09725 0.00000 -106.0 -2.77074 1.13917 0.00000 -104.0 -2.76563 1.17694 0.00000 -102.0 -2.76052 1.21028 0.00000 -100.0 -2.75541 1.23892 0.00000 -98.0 -2.75031 1.26266 0.00000 -96.0 -2.74520 1.28131 0.00000 -94.0 -2.74009 1.29473 0.00000 -92.0 -2.73498 1.30282 0.00000 -90.0 -2.72987 1.30553 0.00000 -88.0 -2.72476 1.30282 0.00000 -86.0 -2.71966 1.29473 0.00000 -84.0 -2.71455 1.28131 0.00000 -82.0 -2.70944 1.26266 0.00000 -80.0 -2.70433 1.23892 0.00000 -78.0 -2.69922 1.21028 0.00000 -76.0 -2.69411 1.17694 0.00000 -74.0 -2.68901 1.13917 0.00000 -72.0 -2.68390 1.09725 0.00000 -70.0 -2.67879 1.05150 0.00000 -68.0 -2.67368 1.00228 0.00000 -66.0 -2.66857 0.94997 0.00000 -64.0 -2.66346 0.89498 0.00000 -62.0 -2.65836 0.83777 0.00000 -60.0 -2.65325 0.77877 0.00000 -58.0 -2.64814 0.71849 0.00000 -56.0 -2.64303 0.65742 0.00000 -54.0 -2.63792 0.59608 0.00000 -52.0 -2.63282 0.53501 0.00000 -50.0 -2.62771 0.47473 0.00000 -48.0 -2.62260 0.41581 0.00000 -46.0 -2.61749 0.35879 0.00000 -44.0 -2.61238 0.30422 0.00000 -42.0 -2.60727 0.25267 0.00000 -40.0 -2.60217 0.20467 0.00000 -38.0 -2.59706 0.16076 0.00000 -36.0 -2.59195 0.12148 0.00000 -34.0 -2.58684 0.08734 0.00000 -32.0 -2.58173 0.05883 0.00000 -30.0 -2.57662 0.03644 0.00000 -28.0 -2.43215 0.01000 0.00000 -26.0 -2.22271 0.01000 0.00000 -24.0 -2.01327 0.01000 0.00000 -22.0 -1.80383 0.01000 0.00000 -20.0 -1.59440 0.01000 0.00000 -18.0 -1.38496 0.01000 0.00000 -16.0 -1.17552 0.01000 0.00000 -14.0 -0.96608 0.01000 0.00000 -12.0 -0.75664 0.01000 0.00000 -10.0 -0.54720 0.01000 0.00000 -8.0 -0.33776 0.01000 0.00000 -6.0 -0.12832 0.01000 0.00000 -4.0 0.08112 0.01000 0.00000 -2.0 0.29056 0.01000 0.00000 0.0 0.50000 0.01000 0.00000 2.0 0.70944 0.01000 0.00000 4.0 0.91888 0.01000 0.00000 6.0 1.12832 0.01000 0.00000 8.0 1.33776 0.01000 0.00000 10.0 1.54720 0.01000 0.00000 12.0 1.75664 0.01000 0.00000 14.0 1.96608 0.01000 0.00000 16.0 2.17552 0.01000 0.00000 18.0 2.38496 0.01000 0.00000 20.0 2.55108 0.03121 0.00000 22.0 2.55619 0.01674 0.00000 24.0 2.56130 0.01038 0.00000 26.0 2.56641 0.01179 0.00000 28.0 2.57152 0.02062 0.00000 30.0 2.57662 0.03644 0.00000 32.0 2.58173 0.05883 0.00000 34.0 2.58684 0.08734 0.00000 36.0 2.59195 0.12148 0.00000 38.0 2.59706 0.16076 0.00000 40.0 2.60217 0.20467 0.00000 42.0 2.60727 0.25267 0.00000 44.0 2.61238 0.30422 0.00000 46.0 2.61749 0.35879 0.00000 48.0 2.62260 0.41581 0.00000 50.0 2.62771 0.47473 0.00000 52.0 2.63282 0.53501 0.00000 54.0 2.63792 0.59608 0.00000 56.0 2.64303 0.65742 0.00000 58.0 2.64814 0.71849 0.00000 60.0 2.65325 0.77877 0.00000 62.0 2.65836 0.83777 0.00000 64.0 2.66346 0.89498 0.00000 66.0 2.66857 0.94997 0.00000 68.0 2.67368 1.00228 0.00000 70.0 2.67879 1.05150 0.00000 72.0 2.68390 1.09725 0.00000 74.0 2.68901 1.13917 0.00000 76.0 2.69411 1.17694 0.00000 78.0 2.69922 1.21028 0.00000 80.0 2.70433 1.23892 0.00000 82.0 2.70944 1.26266 0.00000 84.0 2.71455 1.28131 0.00000 86.0 2.71966 1.29473 0.00000 88.0 2.72476 1.30282 0.00000 90.0 2.72987 1.30553 0.00000 92.0 2.73498 1.30282 0.00000 94.0 2.74009 1.29473 0.00000 96.0 2.74520 1.28131 0.00000 98.0 2.75031 1.26266 0.00000 100.0 2.75541 1.23892 0.00000 102.0 2.76052 1.21028 0.00000 104.0 2.76563 1.17694 0.00000 106.0 2.77074 1.13917 0.00000 108.0 2.77585 1.09725 0.00000 110.0 2.78096 1.05150 0.00000 112.0 2.78606 1.00228 0.00000 114.0 2.79117 0.94997 0.00000 116.0 2.79628 0.89498 0.00000 118.0 2.80139 0.83777 0.00000 120.0 2.80650 0.77877 0.00000 122.0 2.81161 0.71849 0.00000 124.0 2.81671 0.65742 0.00000 126.0 2.82182 0.59608 0.00000 128.0 2.82693 0.53501 0.00000 130.0 2.83204 0.47473 0.00000 132.0 2.83715 0.41581 0.00000 134.0 2.84225 0.35879 0.00000 136.0 2.84736 0.30422 0.00000 138.0 2.85247 0.25267 0.00000 140.0 2.85758 0.20467 0.00000 142.0 2.86269 0.16076 0.00000 144.0 2.86780 0.12148 0.00000 146.0 2.87290 0.08734 0.00000 148.0 2.87801 0.05883 0.00000 150.0 2.88312 0.03644 0.00000 152.0 2.88823 0.02062 0.00000 154.0 2.89334 0.01179 0.00000 156.0 2.89845 0.01038 0.00000 158.0 2.90355 0.01674 0.00000 160.0 2.90866 0.03121 0.00000 162.0 2.91377 0.05412 0.00000 164.0 2.91888 0.08572 0.00000 166.0 2.92399 0.12626 0.00000 168.0 2.92910 0.17592 0.00000 170.0 2.93420 0.23485 0.00000 172.0 2.93931 0.30317 0.00000 174.0 2.94442 0.38094 0.00000 176.0 2.94953 0.46819 0.00000 178.0 2.95464 0.56489 0.00000 180.0 -2.95975 0.67098 0.00000