Sheet1Fuselage DesignFlight Regime Data:Cruise Mach2.1Cruise Alt. (ft)55,000V (f/s)1,925.70r (lbm/f^3)0.0092227644q (lbf/f^2)531.0709037106m (lbm/(f-s))0.0000107n (cruise) (f^2/s)0.0011601728Dimension Data:Form Factors:D-max (ft)9F1.0568658892L/D14Q1L (ft)126F*Q1.0568658892S (f^2)519Viscous Drag Calculations:Von-Karman Ogive Fuselage Shapex/Lx (ft)x-L/4 (ft)D (ft)P (ft)Sw(ft^2)RexCFDrag (lbf)0.000.00-31.5000.00.1012.60-18.903.395976690810.7134.42.1E+071.94E-031470.2025.20-6.305.50053935217.3217.74.2E+071.75E-032140.3037.806.307.123486985822.4282.06.3E+071.65E-032610.4050.4018.908.334707092426.2329.98.4E+071.59E-032940.5063.0031.50928.3356.31.0E+081.54E-033070.6075.60-8.334707092426.2329.91.3E+081.50E-032770.7088.20-7.123486985822.4282.01.5E+081.47E-032320.80100.80-5.50053935217.3217.71.7E+081.44E-031760.90113.40-3.395976690810.7134.41.9E+081.42E-031071126.00-00.00.02.1E+081.40E-030Totals:2284.42015Wave Drag Calculations:A_max63.6172512352CDW0.0204081633Drag (lbf)689.4953286747Total Drag:2705(lbf)Equiv. CD0.009813848

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Sheet1010.668775423617.280454019122.379094382526.184254571228.274333882326.184254571222.379094382517.280454019110.66877542360

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