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{"sheet":"(c)","index":2,"n_rows":21,"n_cols":1,"rows_kept":21,"cut":false,"hidden":false,"merged":[]}
["Copyright © 2021"]
["Max Schnoor"]
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[]
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["The spreadsheet for the Project"]
["\"Die Diederich-Methode zur Berechnung der Auftriebsverteilung am Tragflügel in Excel\""]
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["is free software: you can redistribute it and/or modify it"]
["under the terms of the GNU General Public License as published by"]
["the Free Software Foundation, License Version 3."]
[]
["The spreadsheet is distributed in the hope that it will be useful,"]
["but WITHOUT ANY WARRANTY; without even the implied warranty of"]
["MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE."]
["See the GNU General Public License for more details."]
[]
["http://www.gnu.org/licenses/ "]

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["Plot Tables "]
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["Plots for Diederich Factors"]
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[null,"The Sweep Correction Function"]
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["Plot Parameters"]
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[null,null,null,null,null,null,null,null,null,null,null,null,null,null,"Sweep Correction Function (Figure 1)"]
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[null,null,null,null,null,null,null,null,null,null,null,null,null,null,"Mason's Lift Distribution Curve (Figure 2)"]
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[null,"Scale from Mason to Diederich Graph (Figure 1 and 2 )       ",null,null,null,null,null,{"$f":"1.275/0.71","v":1.795774647887324}]
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["Plots from Figure 2"]
["Spanwise station as input",0,0.05,0.1,0.15,0.2,0.25,0.3,0.35,0.4,0.45,0.5,0.55000000000000004,0.6,0.65,0.7,0.75,0.8,0.85,0.9,0.95,1]
["Spanload calculated with CorelDRAW",70.86,70.09,69,67.91,66.045000000000002,65.311999999999998,60.606000000000002,57.186999999999998,54.079000000000001,51.747999999999998,48.018999999999998,45.066000000000003,41.491999999999997,37.295999999999999,34.343000000000004,30.303000000000001,25.952000000000002,22.222000000000001,17.094000000000001,11.343999999999999,0]
["Spanload converted to scale",{"$f":"B69*$A$72","v":0.79999999999999993},{"$f":"C69*$A$72","v":0.79130680214507487},{"$f":"D69*$A$72","v":0.77900084674005077},{"$f":"E69*$A$72","v":0.76669489133502677},{"$f":"F69*$A$72","v":0.74563928873835739},0.71499999999999997,{"$f":"H69*$A$72","v":0.68423370025402197},0.64563364380468524,0.61054473609935078,0.58422805532034994,0.54212813999435505,0.50878916172734978,0.46843917583968386,0.42106689246401352,0.38772791419700819,0.34211685012701099,0.29299463731301156,0.25088343211967262,0.19298899237933956,0.12807225515100196,0.05]
["scale"]
[{"$f":"0.8/70.86","v":1.1289867344058707E-2}]

{"sheet":"Diederich's Method","index":8,"n_rows":193,"n_cols":195,"rows_kept":193,"cut":false,"hidden":false,"merged":[]}
[]
[null,"Diederich's Method "]
[]
[]
[]
[null,"Input",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"How to use"]
[]
[null,"General Input"]
[null,"Aspect Ratio","A",8,"-"]
[null,"Taper Ratio","λ",0.3,"-",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"Beside choosing rational values for the input, the following guidelines should be taken into account"]
[null,"Quarter Chord Sweep","j0.25",20,"deg"]
[null,"Mach No","M",0.8,"-"]
[null,"Aerodynamic twist at the tip","et",-3,"deg",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●","    Only change blue values!"]
[null,"Lift coefficient","CL",1,"-"]
[null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●",null,"A       >",{"$f":"4/(COS(phi_25*(PI()/180)))","v":4.2567110899036482},null,{"$f":"IF(A_w>AA15, \"correct data\", \"false data\")","v":"correct data"}]
[null,"Additional Input"]
[null,"Mean geometric chord","cg",1,"m",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●","-35° ","<  j0.25    <","35°",null,{"$f":"IF(AND(-35<phi_25, phi_25<35), \"correct data\", \"false data\")","v":"correct data"}]
[null,"Flight altitude","h",10,"km"]
[null,"Thickness ratio at the root","(t/c)r",0.15,"-",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●",null,"h       < ","20 km",null,{"$f":"IF(Altitude>20, \"false data\", \"correct data\")","v":"correct data"}]
[null,"Thickness ratio at the tip","(t/c)t",0.15,"-"]
[null,"Airfoil trailing edge angle at the root","fTE,r",14,"deg",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●",null,"M       < ",0.8,null,{"$f":"IF(Mac>0.8, \"false data\", \"correct data\")","v":"correct data"}]
[null,"Airfoil trailing edge angle at the tip","fTE,t",14,"deg"]
[null,"Maximum section lift at the root","clmax,r",1.6,"-"]
[null,"Maximum section lift at the tip","clmax,t",1,"-"]
[null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"For further use the following statements might be helpful"]
[]
[]
[null,"Output",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●","Single curves can be hidden by first clicking the graph, then the following button: "]
[]
[null,"Diederichs Lift Distribution Compared",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●","The general input is used for major changes in lift distributions while the additional input refines these results "]
[null,"Error to elliptical lift distribution ","-",{"$f":"GM168","v":8.2085128569746368E-2},"-"]
[null,"Error to Mason's lift distribution ","-",{"$f":"GM171","v":4.6000990896029812},"-",null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●","The additional output values are only representative for a correct additional input"]
[null,"Error to triangular lift distribution","-",{"$f":"GM174","v":16.644925926644348},"-"]
[null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,"●","For detailled values scroll down to the plot tables after finishing the input data or use your cursor and point on a selected curve section"]
[null,"Additional Output"]
[null,"Root chord length","cr",{"$f":"(2/(1+lam))*c_g","v":1.5384615384615383},"m"]
[null,"Tip chord length","ct",{"$f":"c_r*lam","v":0.46153846153846145},"m"]
[null,"Maximum lift coefficient of the wing","Clmax",{"$f":"GM178*C_L","v":1.0311483313309722},"-"]
[null,"Lift curve slope of the airfoil (mean value)","cl,a",{"$f":"cl_alpha_mean","v":10.108885352739374},"1/rad"]
[null,"Reynolds number","Re",{"$f":"Rey_No","v":6785094.5582645992},"-"]
[null,"Leading edge angle","j0.0",{"$f":"(LE_angle*(180/PI()))","v":23.329470216620674},"deg"]
[null,"Trailing edge angle","j1.0",{"$f":"(TE_angle*(180/PI()))","v":9.2046059693368303},"deg"]
[null,"Wingspan","b",{"$f":"A_w*c_r*(1+lam)*0.5","v":8},"m"]
[null,"Wing surface area","S",{"$f":"(b_wing/2)*c_r*(1+lam)","v":8},"m²"]
[null,"True airspeed","VTAS",{"$f":"Mac*speedofsound_h","v":239.58668647854466},"m/s"]
[null,"True airspeed","VTAS",{"$f":"Mac*speedofsound_h*3.6","v":862.51207132276079},"km/h"]
[]
[null,"Calculated Values"]
[null,"2pA/ cl,a cosj0.25","F",{"$f":"(2*PI()*A_w)/(c_l.alp*COS(phi_25*PI()/180))","v":5.2915239699979928},"-"]
[null,"Diederich's Factor","C1",{"$f":"C_one(D49)","v":0.26916506360559289},"-"]
[null,"Diederich's Factor","C2",{"$f":"C_two(D49)","v":0.49484984406251997},"-"]
[null,"Diederich's Factor","C3",{"$f":"C_three(D49)","v":0.2279890410795212},"-"]
[null,"Diederich's Factor","C4",{"$f":"C_four(D49)","v":0.38170097160573435},"-"]
[null,"Jone's edge velocity factor","E",{"$f":"1+((2*lam)/(A_w*(1+lam)))","v":1.0576923076923077},"-"]
[null,"Factor","ao,1",{"$f":"-((C_1*(1+(2*lam))/(3*(1+lam)))+((C_2+C_3)*4/(3*PI())))","v":-0.41720904377297724},"-"]
[null,"Prandtl's compressibility correction","b",{"$f":"SQRT(1-POWER(Mac,2))","v":0.59999999999999987},"-"]
[null,"Effective sweep angle","jb",{"$f":"ATAN(TAN(phi_25*PI()/180)/bet)*180/PI()","v":31.241714555956111},"deg"]
[null,"Theory lift curve slope of the airfoil at the root","cl,a,r,theory",{"$f":"(2*PI())+(4.7*D19*(1+(0.00375*fi_TE.r)))","v":7.0251978071795858},"1/rad"]
[null,"Theory lift curve slope of the airfoil at the tip","cl,a,t,theory",{"$f":"(2*PI())+(4.7*D20*(1+(0.00375*fi_TE.t)))","v":7.0251978071795858},"1/rad"]
[null,"Lift curve slope of the airfoil at the root","cl,a,r",{"$f":"cl_alph_root","v":10.108885352739327},"1/rad"]
[null,"Lift curve slope of the airfoil at the tip","cl,a,t",{"$f":"cl_alpha_tip","v":10.108885352739327},"1/rad"]
[null,"Kinematic viscosity in flight altitude ","ν",{"$f":"kin_vis","v":3.5310736559553995},"E-5*m²/s"]
[null,"Speed of sound in flight altitude","a",{"$f":"SoSOUND","v":299.48335809818082},"m/s"]
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[null,"Plot Tables"]
[]
[null,"Diederichs sweep correction function","f",{"$f":"f(phi_bet,D149)","v":0.87650704507295374},{"$f":"f(phi_bet,E149)","v":0.88230386696049601},0.88931991425564061,0.89742982575275454,0.90651416594734757,0.91645928278945354,0.92715716556361694,0.93850530289548595,0.95040654088501197,0.96276894136625435,0.97550564029379327,0.98853470625574602,1.0017789991133923,1.015166028767404,1.0286278140506808,1.0421007417477945,1.0555254257410356,1.0688465662830706,1.0820128093962007,1.0949766063982311,1.1076940735549441,1.1201248518591775,1.1322319669365124,1.1439816890775643,1.1553433933968811,1.1662894201184479,1.1767949349877986,1.186837789810731,1.1963983831186309,1.2054595209604018,1.2140062778209988,1.2220258576665715,{"$f":"f(phi_bet,AJ149)","v":1.2295074551162115},1.2364421167403064,1.2428226024854989,1.2486432472262559,1.2538998224430373,1.2585893980270786,1.2627102042117724,1.2662614936306624,1.2692434035020383,1.2716568179401415,1.273503230392973,1.2747846062067101,1.2755032453167292,1.2756616450652318,1.275262363145482,1.2743078806726442,1.2728004653812324,1.2707420349491612,1.2681340204484068,1.2649772299222706,1.2612717120892538,1.2570166201735302,1.252210075862034,1.2468490333881506,1.2409291437420107,1.2344446190073932,1.2273880968252331,1.2197505049837389,1.211520926135115,1.2026864626388796,1.1932321015318128,1.1831405796244832,{"$f":"f(phi_bet,BP149)","v":1.1723922487243994},1.1609649409857676,1.1488338343858338,1.1359713183278677,1.1223468593707198,1.107926867085,1.0926745600358709,1.0765498318924211,1.0595091176636704,1.0415052600611749,1.0224873759882236,1.0024007231556602,0.9811865668243005,0.95878204667396327,0.93512004379909464,0.9101290478310109,0.8837330241867446,0.85585128144450173,0.82639833884569891,0.79528379392364967,0.76241219025882268,0.72768288536071513,0.69098991867634674,0.65222187972533152,0.61126177636158785,0.56798690316162304,0.52226870993946384,0.51755738122638961,0.51282014123571129,0.50805685150249635,0.5032673729484487,0.49845156588059591,{"$f":"f(phi_bet,CV149)","v":0.49360928998999232},0.48874040435038502,0.48384476741692656,0.47892223702484149,0.47397267038814384,0.46899592409829638,0.46399185412292293,0.45896031580448376,0.45390116385897183,0.44881425237459793,0.44369943481049451,0.43855656399538762,0.43338549212629474,0.42818607076721932,0.42295815084783372,0.41770158266217888,0.41241621586734634,0.40710189948217368,0.40175848188593144,0.39638581081702845,0.39098373337167369,0.38555209600260892,0.38009074451775132,0.37459952407893615,0.36907827920057135,0.36352685374833527,0.35794509093789517,0.35233283333356108,0.34668992284700428,0.34101620073593952,0.33531150760282774,0.32957568339354337,{"$f":"f(phi_bet,EB149)","v":0.32380856739610836},0.31800999823934023,0.31217981389158245,0.30631785165937031,0.30042394818614182,0.29449793945092079,0.28853966076702053,0.28254894678072923,0.27652563146999792,0.27046954814315527,0.26438052943758394,0.25825840731841437,0.25210301307723204,0.24591417733076068,0.23969173001955876,0.23343550040672748,0.22714531707657959,0.22082100793335507,0.21446240019990986,0.20806932041641024,0.2016415944390372,0.19517904743865874,0.18868150389955321,0.18214878761808823,0.17558072170141659,0.16897712856618691,0.16233782993721926,0.15566264684621658,0.14895139963045559,0.14220390793147739,0.13541999069379893,0.12859946616359963,{"$f":"f(phi_bet,FH149)","v":0.12174215188740981},0.11484786471083128,0.1079164207772136,0.10094763552635447,9.394132369321477E-2,8.6897299306581036E-2,7.9815375687805501E-2,7.2695365449468502E-2,6.5537080494102465E-2,5.8340332012858542E-2,5.110493048424665E-2,4.3830685672801011E-2,3.651740662778355E-2,2.9164901681899197E-2,2.1772978449970851E-2,1.4341443827663388E-2,6.870103990151144E-3,-6.4123560914263302E-4,-8.1927702398878737E-3,-1.5784695896117622E-2,-2.3417209297546794E-2,-3.1090507890859001E-2,-3.8804789851027921E-2,-4.656025408258694E-2,-5.4357100220958625E-2,-6.2195528633736487E-2,-7.0075740421988844E-2,-7.7997937421568436E-2,-8.5962322204397756E-2,-9.3969098079771843E-2,-0.10201846909566784]
[]
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[null,"Non dimensional spanwise station","h",0,0.01,0.02,0.03,0.04,0.05,0.06,7.0000000000000007E-2,0.08,0.09,0.1,0.11,0.12,0.13,0.14000000000000001,0.15,0.16,0.17,0.18,0.19,0.2,0.21,0.22,0.23,0.24,0.25,0.26,0.27,0.28000000000000003,0.28999999999999998,0.3,0.31,0.32,0.33,0.34,0.35,0.36,0.37,0.38,0.39,0.4,0.41,0.42,0.43,0.44,0.45,0.46,0.47,0.48,0.49,0.5,0.51,0.52,0.53,0.54,0.55000000000000004,0.56000000000000005,0.56999999999999995,0.57999999999999996,0.59,0.6,0.61,0.62,0.63,0.64,0.65,0.66,0.67,0.68,0.69,0.7,0.71,0.72,0.73,0.74,0.75,0.76,0.77,0.78,0.79,0.8,0.81,0.82,0.83,0.84,0.85,0.86,0.87,0.88,0.89,0.9,0.90100000000000002,0.90200000000000002,0.90300000000000002,0.90400000000000003,0.90500000000000003,0.90600000000000003,0.90700000000000003,0.90800000000000003,0.90900000000000003,0.91,0.91100000000000003,0.91200000000000003,0.91300000000000003,0.91400000000000003,0.91500000000000004,0.91600000000000004,0.91700000000000004,0.91800000000000004,0.91900000000000004,0.92,0.92100000000000004,0.92200000000000004,0.92300000000000004,0.92400000000000004,0.92500000000000004,0.92600000000000005,0.92700000000000005,0.92800000000000005,0.92900000000000005,0.93,0.93100000000000005,0.93200000000000005,0.93300000000000005,0.93400000000000005,0.93500000000000005,0.93600000000000005,0.93700000000000006,0.93799999999999994,0.93899999999999995,0.94,0.94099999999999995,0.94199999999999995,0.94299999999999995,0.94399999999999995,0.94499999999999995,0.94599999999999995,0.94699999999999995,0.94799999999999995,0.94899999999999995,0.95,0.95099999999999996,0.95199999999999996,0.95299999999999996,0.95399999999999996,0.95499999999999996,0.95599999999999996,0.95699999999999996,0.95799999999999996,0.95899999999999996,0.96,0.96099999999999997,0.96199999999999997,0.96299999999999997,0.96399999999999997,0.96499999999999997,0.96599999999999997,0.96699999999999997,0.96799999999999997,0.96899999999999997,0.97,0.97099999999999997,0.97199999999999998,0.97299999999999998,0.97399999999999998,0.97499999999999998,0.97599999999999998,0.97699999999999998,0.97799999999999998,0.97899999999999998,0.98,0.98099999999999998,0.98199999999999998,0.98299999999999998,0.98399999999999999,0.98499999999999999,0.98599999999999999,0.98699999999999999,0.98799999999999999,0.98899999999999999,0.99,0.99099999999999999,0.99199999999999999,0.99299999999999999,0.99399999999999999,0.995,0.996,0.997,0.998,0.999,1]
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[]
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[]
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[]
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Curve'!$H$35*C_L","v":1.3567633241329224},{"$f":"((-0.178321*T149^3)-(0.241023*T149^2)-(0.353808*T149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.3488370967459156},{"$f":"((-0.178321*U149^3)-(0.241023*U149^2)-(0.353808*U149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.3407935632245422},{"$f":"((-0.178321*V149^3)-(0.241023*V149^2)-(0.353808*V149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.332630802222817},{"$f":"((-0.178321*W149^3)-(0.241023*W149^2)-(0.353808*W149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.3243468923947537},{"$f":"((-0.178321*X149^3)-(0.241023*X149^2)-(0.353808*X149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.3159399123943663},{"$f":"((-0.178321*Y149^3)-(0.241023*Y149^2)-(0.353808*Y149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.3074079408756691},{"$f":"((-0.178321*Z149^3)-(0.241023*Z149^2)-(0.353808*Z149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.298749056492676},{"$f":"((-0.178321*AA149^3)-(0.241023*AA149^2)-(0.353808*AA149)+0.814627)*'Mason''s 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Curve'!$H$35*C_L","v":1.2246785567957745},{"$f":"((-0.178321*AI149^3)-(0.241023*AI149^2)-(0.353808*AI149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.2147909960647536},{"$f":"((-0.178321*AJ149^3)-(0.241023*AJ149^2)-(0.353808*AJ149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.2047573090095776},{"$f":"((-0.178321*AK149^3)-(0.241023*AK149^2)-(0.353808*AK149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.1945755742842608},{"$f":"((-0.178321*AL149^3)-(0.241023*AL149^2)-(0.353808*AL149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.1842438705428169},{"$f":"((-0.178321*AM149^3)-(0.241023*AM149^2)-(0.353808*AM149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.1737602764392605},{"$f":"((-0.178321*AN149^3)-(0.241023*AN149^2)-(0.353808*AN149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":1.1631228706276056},{"$f":"((-0.178321*AO149^3)-(0.241023*AO149^2)-(0.353808*AO149)+0.814627)*'Mason''s 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Curve'!$H$35*C_L","v":0.88629677634676063},{"$f":"((-0.178321*BK149^3)-(0.241023*BK149^2)-(0.353808*BK149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.87159140975672533},{"$f":"((-0.178321*BL149^3)-(0.241023*BL149^2)-(0.353808*BL149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.85668611915492965},{"$f":"((-0.178321*BM149^3)-(0.241023*BM149^2)-(0.353808*BM149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.84157898319538738},{"$f":"((-0.178321*BN149^3)-(0.241023*BN149^2)-(0.353808*BN149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.82626808053211265},{"$f":"((-0.178321*BO149^3)-(0.241023*BO149^2)-(0.353808*BO149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.8107514898191196},{"$f":"((-0.178321*BP149^3)-(0.241023*BP149^2)-(0.353808*BP149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.79502728971042258},{"$f":"((-0.178321*BQ149^3)-(0.241023*BQ149^2)-(0.353808*BQ149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.77909355886003517},{"$f":"((-0.178321*BR149^3)-(0.241023*BR149^2)-(0.353808*BR149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.76294837592197173},{"$f":"((-0.178321*BS149^3)-(0.241023*BS149^2)-(0.353808*BS149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.74658981955024639},{"$f":"((-0.178321*BT149^3)-(0.241023*BT149^2)-(0.353808*BT149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.73001596839887317},{"$f":"((-0.178321*BU149^3)-(0.241023*BU149^2)-(0.353808*BU149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.71322490112186632},{"$f":"((-0.178321*BV149^3)-(0.241023*BV149^2)-(0.353808*BV149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.69621469637323952},{"$f":"((-0.178321*BW149^3)-(0.241023*BW149^2)-(0.353808*BW149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.67898343280700713},{"$f":"((-0.178321*BX149^3)-(0.241023*BX149^2)-(0.353808*BX149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.66152918907718317},{"$f":"((-0.178321*BY149^3)-(0.241023*BY149^2)-(0.353808*BY149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.64385004383778177},{"$f":"((-0.178321*BZ149^3)-(0.241023*BZ149^2)-(0.353808*BZ149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.62594407574281696},{"$f":"((-0.178321*CA149^3)-(0.241023*CA149^2)-(0.353808*CA149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.60780936344630276},{"$f":"((-0.178321*CB149^3)-(0.241023*CB149^2)-(0.353808*CB149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.58944398560225353},{"$f":"((-0.178321*CC149^3)-(0.241023*CC149^2)-(0.353808*CC149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.57084602086468306},{"$f":"((-0.178321*CD149^3)-(0.241023*CD149^2)-(0.353808*CD149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.5520135478876057},{"$f":"((-0.178321*CE149^3)-(0.241023*CE149^2)-(0.353808*CE149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.53294464532503505},{"$f":"((-0.178321*CF149^3)-(0.241023*CF149^2)-(0.353808*CF149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.51363739183098578},{"$f":"((-0.178321*CG149^3)-(0.241023*CG149^2)-(0.353808*CG149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.49408986605947164},{"$f":"((-0.178321*CH149^3)-(0.241023*CH149^2)-(0.353808*CH149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.47430014666450721},{"$f":"((-0.178321*CI149^3)-(0.241023*CI149^2)-(0.353808*CI149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.45426631230010572},{"$f":"((-0.178321*CJ149^3)-(0.241023*CJ149^2)-(0.353808*CJ149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.43398644162028172},{"$f":"((-0.178321*CK149^3)-(0.241023*CK149^2)-(0.353808*CK149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.41345861327904937},{"$f":"((-0.178321*CL149^3)-(0.241023*CL149^2)-(0.353808*CL149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.39268090593042254},{"$f":"((-0.178321*CM149^3)-(0.241023*CM149^2)-(0.353808*CM149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.37165139822841547},{"$f":"((-0.178321*CN149^3)-(0.241023*CN149^2)-(0.353808*CN149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.35036816882704225},{"$f":"((-0.178321*CO149^3)-(0.241023*CO149^2)-(0.353808*CO149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.32882929638031672},{"$f":"((-0.178321*CP149^3)-(0.241023*CP149^2)-(0.353808*CP149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.30703285954225329},{"$f":"((-0.178321*CQ149^3)-(0.241023*CQ149^2)-(0.353808*CQ149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.30483897584510306},{"$f":"((-0.178321*CR149^3)-(0.241023*CR149^2)-(0.353808*CR149)+0.814627)*'Mason''s Curve'!$H$35*C_L","v":0.30264249536923349},{"$f":"((-0.178321*CS149^3)-(0.241023*CS149^2)-(0.353808*CS149)+0.814627)*'Mason''s 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[]
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[]
[null,"Maximum section lift of the airfoil","clmax",{"$f":"(c_l.max.t-c_l.max.r)*D149+c_l.max.r","v":1.6},1.5940000000000001,1.5880000000000001,1.5820000000000001,1.5760000000000001,1.57,1.5640000000000001,1.5580000000000001,1.552,1.546,1.54,1.534,1.528,1.522,1.516,1.51,1.504,1.498,1.492,1.486,1.48,1.4740000000000002,1.468,1.462,1.456,1.4500000000000002,1.444,1.4380000000000002,1.4319999999999999,1.4260000000000002,1.4200000000000002,1.4140000000000001,{"$f":"(c_l.max.t-c_l.max.r)*AJ149+c_l.max.r","v":1.4080000000000001},1.4020000000000001,1.3960000000000001,1.3900000000000001,1.3840000000000001,1.3780000000000001,1.3720000000000001,1.3660000000000001,1.36,1.3540000000000001,1.3480000000000001,1.3420000000000001,1.3360000000000001,1.33,1.3240000000000001,1.3180000000000001,1.3120000000000001,1.306,1.3,1.294,1.288,1.282,1.276,1.27,1.264,1.258,1.252,1.246,1.24,1.234,1.228,1.222,{"$f":"(c_l.max.t-c_l.max.r)*BP149+c_l.max.r","v":1.216},1.21,1.204,1.198,1.1919999999999999,1.1859999999999999,1.1800000000000002,1.1739999999999999,1.1680000000000001,1.1619999999999999,1.1560000000000001,1.1499999999999999,1.1440000000000001,1.1379999999999999,1.1320000000000001,1.1259999999999999,1.1200000000000001,1.1139999999999999,1.1080000000000001,1.1020000000000001,1.0960000000000001,1.0900000000000001,1.0840000000000001,1.0780000000000001,1.0720000000000001,1.0659999999999998,1.06,1.0594000000000001,1.0588,1.0582,1.0575999999999999,1.0569999999999999,{"$f":"(c_l.max.t-c_l.max.r)*CV149+c_l.max.r","v":1.0564},1.0558000000000001,1.0552000000000001,1.0546,1.0539999999999998,1.0533999999999999,1.0528,1.0522,1.0516000000000001,1.0509999999999999,1.0504,1.0497999999999998,1.0491999999999999,1.0486,1.048,1.0474000000000001,1.0468,1.0462,1.0455999999999999,1.0449999999999999,1.0444,1.0438000000000001,1.0432000000000001,1.0426,1.0419999999999998,1.0413999999999999,1.0407999999999999,1.0402,1.0396000000000001,1.0389999999999999,1.0384,1.0377999999999998,{"$f":"(c_l.max.t-c_l.max.r)*EB149+c_l.max.r","v":1.0371999999999999},1.0366,1.036,1.0354000000000001,1.0348000000000002,1.0342,1.0336000000000001,1.0329999999999999,1.0324,1.0318000000000001,1.0312000000000001,1.0306000000000002,1.03,1.0293999999999999,1.0287999999999999,1.0282,1.0276000000000001,1.0270000000000001,1.0264,1.0258,1.0251999999999999,1.0246,1.024,1.0234000000000001,1.0228000000000002,1.0222,1.0216000000000001,1.0209999999999999,1.0204,1.0198,1.0192000000000001,1.0186000000000002,{"$f":"(c_l.max.t-c_l.max.r)*FH149+c_l.max.r","v":1.018},1.0173999999999999,1.0167999999999999,1.0162,1.0156000000000001,1.0150000000000001,1.0144,1.0138,1.0131999999999999,1.0125999999999999,1.012,1.0114000000000001,1.0108000000000001,1.0102,1.0096000000000001,1.0089999999999999,1.0084,1.0078,1.0072000000000001,1.0066000000000002,1.006,1.0053999999999998,1.0047999999999999,1.0042,1.0036,1.0030000000000001,1.0024,1.0018,1.0011999999999999,1.0005999999999999,1]
[]
[null,"(clmax-clb)/cla",null,{"$f":"(D176-D159)/D157","v":1.935493864765004},{"$f":"(E176-E159)/E157","v":1.9178453431297224},1.8999162530800187,1.8817598614855475,1.8634260581358968,1.8449613771416464,1.8264090455035096,1.8078090546691956,1.7891982511714228,1.7706104427457312,1.7520765166502894,1.7336245672405202,1.7152800301801177,1.6970658209897895,1.6790024759403774,1.6611082935841621,1.6433994754843231,1.6258902649464528,1.6085930827768624,1.5915186592903683,1.5746761619658673,1.5580733183022868,1.5417165335617409,1.5256110032024048,1.5097608199022539,1.4941690751580807,1.4788379555136719,1.4637688335282113,1.4489623536424396,1.4344185131371923,1.4201367384079311,1.4061159568010608,1.3923546642741593,1.3788509891538401,1.3656027522726324,1.3526075237708555,1.3398626768516755,1.3273654387780627,1.3151129393997467,1.3031022574971209,1.2913304652278248,1.2797946709609307,1.2684920607837624,1.2574199389678176,1.2465757676835323,1.2359572062592292,1.2255621502880303,1.2153887708984319,1.2054355545202708,1.1957013434987762,1.1861853779361464,1.1768873391738197,1.1678073953704491,1.1589462496822944,1.1503051916160414,1.1418861522014103,1.1336917637250821,1.1257254248820414,1.1179913723397534,1.11049475988017,1.1032417464912301,1.0962395950319628,1.0894967834044831,1.0830231305461617,1.0768299400239139,{"$f":"(BQ176-BQ159)/BQ157","v":1.0709301645932445},1.0653385958074209,1.0600720836664304,1.0551497924331728,1.0505935001845037,1.0464279514995491,1.0426812750415009,1.0393854808310257,1.0365770559718801,1.0342976827946511,1.0325951102844608,1.0315242188937381,1.0311483313309722,1.0315408389975738,1.0327872373884437,1.0349876969285514,1.0382603428785122,1.0427454860654741,1.0486111462762859,1.0560603599381579,1.0653409925495414,1.0767591340060674,1.0906977285104362,1.1076430373127892,1.1282231466883452,1.1532655915722552,1.1560550895268136,1.1589013340631538,1.1618056772397582,1.1647695164371361,1.1677942963268917,1.1708815109466,1.1740327058873379,1.1772494806011524,1.1805334908363971,1.1838864512093823,1.1873101379215429,1.1908063916319436,1.1943771204958185,1.1980243033806368,1.2017499932721531,1.2055563208839084,1.2094454984847922,1.2134198239604643,1.2174816851258228,1.2216335643071594,1.2258780432142742,1.2302178081246213,1.2346556554035095,1.2391944973865761,1.2438373686531341,1.2485874327216913,1.2534479892017851,1.2584224814396969,1.2635145046990148,1.2687278149212697,1.2740663381161459,1.279534180435864,1.2851356389939255,1.2908752134945263,1.2967576187460437,1.302787798139756,1.308970938183768,1.3153124841919701,{"$f":"(EC176-EC159)/EC157","v":1.3218181572391174},1.3284939725055334,1.335346259149397,1.3423816818605625,1.3496072642683163,1.3570304143963301,1.3646589523819073,1.372501140703887,1.3805657171947261,1.3888619311482533,1.3973995828757551,1.4061890671107597,1.4152414207180601,1.4245683752264398,1.4341824147790887,1.4440968401826233,1.4543258398372951,1.4648845684505776,1.4757892345770796,1.4870571981942213,1.4987070797207804,1.5107588821206246,1.5232341280156265,1.5361560140695891,1.5495495853127381,1.5634419325703288,1.5778624167600299,1.5928429245586131,1.6084181608432695,1.6246259844322133,1.6415077950419967,1.6591089811227038,1.6774794404300351,1.696674187983289,1.7167540696259427,1.7377866040052292,1.759846981767649,1.7830192586147973,1.8073977892637032,1.8330889632835647,1.8602133226497009,1.8889081667360226,1.9193307864490496,1.9516625199720228,1.9861138953794524,2.0229312316281902,2.0624052275892741,2.1048823094372491,2.1507798819907307,2.2006072312611167,2.2549948209975468,2.3147364340817171,2.3808516663649799,2.4546820293797502,2.5380453929217159,2.6334981293281521,2.7448122478707759,2.8779282253551455,3.043122387328836,3.261026416540163,3.5866668270540711,4.6314047126438664,{"$f":"MIN(D178:GL178)","v":1.0311483313309722}]
[null,"Aerodynamic twist at the tip","et",{"$f":"Eps_t*PI()/180","v":-5.2359877559829883E-2},"rad","umrechnung!"]
[]
[null,"Plot for wing figure","Eta","LE",0.25,"TE"]
[null,null,0,{"$f":"C193","v":0.38461538461538458},{"$f":"0.75*C193","v":0.28846153846153844},0]
[null,null,1,{"$f":"-TAN(C191)+C193","v":-4.6662541958510051E-2},{"$f":"-TAN(phi_25*PI()/180)+0.75*C193","v":-7.5508695804663906E-2},{"$f":"-TAN(C192)","v":-0.16204715734312541}]
[]
[null,"Plot for wing root and wing tip ","x","y"]
[null,null,0,0]
[null,null,0,{"$f":"C193","v":0.38461538461538458}]
[]
[null,null,1,{"$f":"D183","v":-4.6662541958510051E-2}]
[null,null,1,{"$f":"F183","v":-0.16204715734312541}]
[null,"Leading edge Angle of wing figure",{"$f":"ATAN(TAN(phi_25*PI()/180)-(4/A_w)*(-0.25*((1-lam)/(1+lam))))","v":0.40717606802598549}]
[null,"Trailing Edge Angle of wing figure",{"$f":"ATAN(TAN(phi_25*PI()/180)-(4/A_w)*(0.75*((1-lam)/(1+lam))))","v":0.16065068051365192}]
[null,"qualitative cg representation for wing figure",{"$f":"2*2/(A_w*(1+lam))","v":0.38461538461538458}]