Sheet1Main Wing ReferenceAir Propertiesb32.2ftCruise Alt. (ft)55,000ftm.a.c.21.5ftV1,925.70f/sS519ft2r0.0092227644lbm/f^3M2.10q531.0709037106lbf/f^2LLE62degm0.0000107lbm/(f-s)t/c0.04n (cruise)0.0011601728f^2/sl0.00Vertical TailDesign ParametersAirfoil DataCvt0.07NameNACA 64-004Lvt40.0ftClmax0.8LLE63degCla0.1111/degt/c0.04a.c.0.258cl0.30a0L0degAvt1.10Cd0.004CalculationsSweep AnglesViscous DragSvt29ft2x/cLx/c (deg)V_eff874.2495053484f/sb5.7ftLE0.0063.0q_eff109.4576292939lbf/f^2cr7.9ft1/4 chord0.2555.8M_eff0.9533800495ct2.4ft(t/c)max0.3551.9Re_mac4261022.82777323m.a.c.5.7ftTE1.000.3sqrt(Re)2064.2245100214b1.85Cf3.19E-03CLa0.0231/degS_wet58.57903695ft2F1.5724484978Q1.05Total Drag163.880lbfCD00.0105514705Spanwise Viewxy007.907.9456544725.75.56584496795.700Horizontal TailDesign ParametersAirfoil DataCht0.11NameNACA 64-004Lht50.0ftClmax0.8LLE63degCla0.1111/degt/c0.04a.c.0.258cl0.35a0L0degAht2.00Cd0.004CalculationsSweep AnglesViscous DragSht25ft2x/cLx/c (deg)V_eff874.2495053484f/sb7.0ftLE0.0063.0q_eff109.4576292939lbf/f^2cr5.2ft1/4 chord0.2559.9M_eff0.9533800495ct1.8ft(t/c)max0.3558.4Re_mac2844058.24714015m.a.c.3.8ftTE1.0045.0sqrt(Re)1686.4335881202b1.85Cf3.42E-03CLa0.0301/degS_wet49.1710461ft2F1.5024803135Q1.05Total Drag140.864lbfCD00.0108048826Spanwise Viewxy005.208.69257808393.56.87596046083.500

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