Sheet1Design ParametersAirfoil DataAir PropertiesM2.10NameNACA 64A204Cruise Alt. (ft)55,000ftS519ft2Clmax1.03V1,925.70f/sA2.0Cla0.111/degr0.0092227644lbm/f^3LLE62dega.c.0.253cq531.0709037106lbf/f^2t/c0.04a0L-1.33degm0.0000107lbm/(f-s)l0.00Cd00.004n (cruise)0.0011601728f^2/sW c-start88,817lbf/f^2rle0.0024cW c-end53,976lbf/f^2ClminD0.1 - 0.3q c-start531.07lbf/f^2(t/c)max0.40cq c-end347.41lbf/f^2Cl c-start0.32Cl c-end0.20CalculationsSweep Anglesb32.2ftx/cLx/c (deg)Meff0.99LE0.0062.0cr32.2ft1/4C0.2554.1ct0.0fta.c0.2554.0m.a.c.21.5ft(t/c)max0.4047.2TE1.00-6.8b0.17CLa0.0441/degViscous DragCLo0.06V_eff904.0613884568f/satrim6.0degq_eff117.0499115579lbf/f^2CLtrim0.322Re_mac1.67E+07k0.1989436789sqrt(Re)4091.111706639CD0.028Cf2.54E-03L/D11.48S_wet1039.557ft2F1.4570268711Q1Total Drag7739.8101907571lbfCD00.0074230615Plotting:Spanwise Viewxy0032.2030.296629576916.109003693630.296629576916.109003693600Lift CurvesaClaCL-1.330-1.3308.03363636361.038.03363636360.4137325732

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