Loads

12
Wing Page 1 Wing Data M 2.10 b 32.2 ft S 519 b/2 16.109 ft A 2.0 0.99 62 deg 32.2 ft l 0.00 0.0 ft C_D_0 0.007 m.a.c. 21.5 ft 0.044 1/deg Load Summary Load Type Magnitude dw L (unflap 88817 0 1 61034 0 0.4 6781.556 fuel 20000 0 0.4 2222.222 engine (1 3250 0.3 0.3 3250 engine (2 3250 0.1 0.1 3250 structure 2335 0 1 Load Spanwise Distribution y (ft) y/(b/2) L(y)-ellip L(y)-trap L-bar V-lift (lb) M-lift (f-lb 0.00 0.00 3510.00 5513.50 4511.75 57275.68 380304.43 6781.56 0.81 0.05 3505.61 5237.83 4371.72 52763.93 334171.72 6781.56 1.61 0.10 3492.41 4962.15 4227.28 48392.21 291673.00 6781.56 2.42 0.15 3470.29 4686.48 4078.38 44164.93 252695.48 6781.56 3.22 0.20 3439.09 4410.80 3924.94 40086.55 217122.83 6781.56 4.03 0.25 3398.55 4135.13 3766.84 36161.61 184835.11 6781.56 4.83 0.30 3348.33 3859.45 3603.89 32394.77 155708.74 6781.56 5.64 0.35 3287.99 3583.78 3435.88 28790.88 129616.36 6781.56 6.44 0.40 3216.97 3308.10 3262.54 25355.00 106426.74 6781.56 7.25 0.45 3134.53 3032.43 3083.48 22092.46 86004.56 0.00 8.05 0.50 3039.75 2756.75 2898.25 19008.98 68210.18 0.00 8.86 0.55 2931.43 2481.08 2706.25 16110.73 52899.40 0.00 9.67 0.60 2808.00 2205.40 2506.70 13404.48 39923.01 0.00 10.47 0.65 2667.37 1929.73 2298.55 10897.77 29126.37 0.00 11.28 0.70 2506.64 1654.05 2080.35 8599.23 20348.75 0.00 12.08 0.75 2321.65 1378.38 1850.01 6518.88 13422.50 0.00 12.89 0.80 2106.00 1102.70 1604.35 4668.87 8171.87 0.00 13.69 0.85 1849.01 827.03 1338.02 3064.52 4411.33 0.00 14.50 0.90 1529.98 551.35 1040.66 1726.50 1943.02 0.00 15.30 0.95 1096.00 275.68 685.84 685.84 552.41 0.00 16.11 1.00 0.00 0.00 0.00 0.00 0.00 0.00 56659.61 57891.76 57275.68 61034.00 ft 2 Meff LLE cr ct C_L_a y/(b/2)_sta y/(b/2)_end DL (flap) DL-flap 4000.00 6000.00 Column C

description

Systems

Transcript of Loads

WingWing DataM2.10b32.2ftS519ft2b/216.1090036936ftA2.0Meff0.99LLE62degcr32.2ftl0.00ct0.0ftC_D_00.007m.a.c.21.5ftC_L_a0.0441/degLoad SummaryLoad TypeMagnitudey/(b/2)_starty/(b/2)_enddwL (unflap)8881701DL (flap)6103400.46781.5555555556fuel2000000.42222.2222222222engine (1)32500.30.33250engine (2)32500.10.13250structure233501Load Spanwise Distributiony (ft)y/(b/2)L(y)-ellipL(y)-trapL-barV-lift (lb)M-lift (f-lb)DL-flapDV-flapDM-flapW-fuelV-fuelM-fuelW-structureV-structureM-structureW-engineV-engineM-engineTotal VTotal M0.000.003510.005513.504511.7557275.68380304.436781.5661034.00245799.23-2222.22-20000.00-80545.02-144.95-1521.97-8989.750-6500.00-26177.1390287.71510391.760.810.053505.615237.834371.7252763.93334171.726781.5654252.44196639.39-2222.22-17777.78-64436.01-137.70-1377.02-7763.880-6500.00-20941.7081361.57437669.511.610.103492.414962.154227.2848392.21291673.006781.5647470.89152941.74-2222.22-15555.56-50116.90-130.45-1239.32-6654.75-3250-6500.00-15706.2872568.22372136.822.420.153470.294686.484078.3844164.93252695.486781.5640689.33114706.31-2222.22-13333.33-37587.68-123.21-1108.87-5656.540-3250.00-10470.8567162.07313686.733.220.203439.094410.803924.9440086.55217122.836781.5633907.7881933.08-2222.22-11111.11-26848.34-115.96-985.66-4763.400-3250.00-7853.1458647.56259591.034.030.253398.554135.133766.8436161.61184835.116781.5627126.2254622.05-2222.22-8888.89-17898.89-108.71-869.70-3969.500-3250.00-5235.4350279.24212353.344.830.303348.333859.453603.8932394.77155708.746781.5620344.6732773.23-2222.22-6666.67-10739.34-101.46-760.99-3269.00-3250-3250.00-2617.7142061.78171855.925.640.353287.993583.783435.8828790.88129616.366781.5613563.1116386.62-2222.22-4444.44-5369.67-94.22-659.52-2656.06000.0037250.02137977.256.440.403216.973308.103262.5425355.00106426.746781.566781.565462.21-2222.22-2222.22-1789.89-86.97-565.30-2124.85000.0029349.02107974.217.250.453134.533032.433083.4822092.4686004.560.000.000.000.000.000.00-79.72-478.33-1669.53000.0021614.1284335.038.050.503039.752756.752898.2519008.9868210.180.000.000.000.000.000.00-72.47-398.61-1284.25000.0018610.3766925.938.860.552931.432481.082706.2516110.7352899.400.000.000.000.000.000.00-65.23-326.14-963.19000.0015784.5951936.219.670.602808.002205.402506.7013404.4839923.010.000.000.000.000.000.00-57.98-260.91-700.50000.0013143.5739222.5110.470.652667.371929.732298.5510897.7729126.370.000.000.000.000.000.00-50.73-202.93-490.35000.0010694.8428636.0211.280.702506.641654.052080.358599.2320348.750.000.000.000.000.000.00-43.48-152.20-326.90000.008447.0320021.8512.080.752321.651378.381850.016518.8813422.500.000.000.000.000.000.00-36.24-108.71-204.31000.006410.1713218.1912.890.802106.001102.701604.354668.878171.870.000.000.000.000.000.00-28.99-72.47-116.75000.004596.398055.1213.690.851849.01827.031338.023064.524411.330.000.000.000.000.000.00-21.74-43.48-58.37000.003021.034352.9614.500.901529.98551.351040.661726.501943.020.000.000.000.000.000.00-14.49-21.74-23.35000.001704.761919.6715.300.951096.00275.68685.84685.84552.410.000.000.000.000.000.00-7.25-7.25-5.84000.00678.59546.5716.111.000.000.000.000.000.000.000.000.000.000.000.000.000.000.000000.000.0056659.6157891.7657275.6861034.00-20000.00-1514.73

&APage &P

Wing0000000000000000000000000

#REF!y/(b/2)V [lb]

Fuselage

&APage &Pb/2L(y)

Load factor

&APage &Pb/2V & M

Sheet4

&APage &Pb/2V & M total

Sheet5Fuselage Structure AnalysisFuselage DataFuse Length126ftLoad Summary (fuselage)Load TypeMagnitudex/L_startx/L_endresultantM @C_liftdwPitching Stability(lbs)x/Lf-lb (+ cw)Fuel400000.40.70.55-20005714.2857142857x_cg70.9232142857fPayload50000.10.60.35-1250454.5454545455x_cg/L0.5628826531Structure11000010.5-1100523.8095238095S.M.0.2177409201stableEngine(s)130000.60.60.6013000Wing Struct.46000.40.80.60511.1111111111Tail Struct.48000.810.91440960M Sum-2910Tail Lift (req)-97000.90.90.9-2910-9700Wing Center of LiftL_ctr (x/L)0.6x (ft)x/LW-fuelV-fuelM-fuelW-payloadV-payloadM-payloadW-structV-structM-structW-engineV-engineM-engineW-wingV-wingM-wingW-tailV-tailM-tailL-tailVL-tailML-tailTotal VTotal M0.000.000.000.002.52E+050.000.001.58E+05-523.81-0.001.42E+0500.000.00E+0000.007.66E-1100.00-1.75E+0500.00-3.67E+050.009.35E+036.300.050.000.002.52E+050.000.001.58E+05-523.81523.811.42E+0500.000.00E+0000.007.08E-1100.00-1.75E+0500.00-3.67E+05523.819.35E+0312.600.100.000.002.52E+05-454.550.001.58E+05-523.811047.621.39E+0500.000.00E+0000.006.51E-1100.00-1.75E+0500.00-3.67E+051047.626.05E+0318.900.150.000.002.52E+05-454.55454.551.58E+05-523.811571.431.32E+0500.000.00E+0000.005.94E-1100.00-1.75E+0500.00-3.67E+052025.97-5.52E+0225.200.200.000.002.52E+05-454.55909.091.55E+05-523.812095.241.22E+0500.000.00E+0000.005.37E-1100.00-1.75E+0500.00-3.67E+053004.33-1.33E+0431.500.250.000.002.52E+05-454.551363.641.49E+05-523.812619.051.09E+0500.000.00E+0000.004.79E-1100.00-1.75E+0500.00-3.67E+053982.68-3.22E+0437.800.300.000.002.52E+05-454.551818.181.40E+05-523.813142.869.24E+0400.000.00E+0000.004.22E-1100.00-1.75E+0500.00-3.67E+054961.04-5.73E+0444.100.350.000.002.52E+05-454.552272.731.29E+05-523.813666.677.26E+0400.000.00E+0000.003.65E-1100.00-1.75E+0500.00-3.67E+055939.39-8.86E+0450.400.40-5714.290.002.52E+05-454.552727.271.15E+05-523.814190.484.95E+0400.000.00E+00-511.11111111110.003.07E-1100.00-1.75E+0500.00-3.67E+056917.75-1.26E+0556.700.45-5714.295714.292.52E+05-454.553181.829.74E+04-523.814714.292.31E+0400.000.00E+00-511.1111111111511.112.50E-1100.00-1.75E+0500.00-3.67E+0514121.50-1.70E+0563.000.50-5714.2911428.572.16E+05-454.553636.367.73E+04-523.815238.10-6.60E+0300.000.00E+00-511.11111111111022.22-3.22E+0300.00-1.75E+0500.00-3.67E+0521325.25-2.59E+0569.300.55-5714.2917142.861.44E+05-454.554090.915.44E+04-523.815761.90-3.96E+0400.000.00E+00-511.11111111111533.33-9.66E+0300.00-1.75E+0500.00-3.67E+0528529.00-3.93E+0575.600.60-5714.2922857.143.60E+04-454.554545.452.86E+04-523.816285.71-7.59E+04-130000.000.00E+00-511.11111111112044.44-1.93E+0400.00-1.75E+0500.00-3.67E+0535732.76-5.73E+0581.900.65-5714.29-11428.57-1.08E+050.000.000.00E+00-523.81-4190.48-1.16E+0500.000.00E+00-511.1111111111-2044.44-3.22E+040-4800.00-1.75E+050-9700.00-3.67E+05-32163.49-7.98E+0588.200.70-5714.29-5714.29-3.60E+040.000.000.00E+00-523.81-3666.67-8.91E+0400.000.00E+00-511.1111111111-1533.33-1.93E+040-4800.00-1.45E+050-9700.00-3.06E+05-25414.29-5.95E+0594.500.750.000.000.00E+000.000.000.00E+00-523.81-3142.86-6.60E+0400.000.00E+00-511.1111111111-1022.22-9.66E+030-4800.00-1.15E+050-9700.00-2.44E+05-18665.08-4.35E+05100.800.800.000.000.00E+000.000.000.00E+00-523.81-2619.05-4.62E+0400.000.00E+00-511.1111111111-511.11-3.22E+03-960-4800.00-8.47E+040-9700.00-1.83E+05-17630.16-3.17E+05107.100.850.000.000.00E+000.000.000.00E+00-523.81-2095.24-2.97E+0400.000.00E+0000.000.00E+00-960-3840.00-5.44E+040-9700.00-1.22E+05-15635.24-2.06E+05113.400.900.000.000.00E+000.000.000.00E+00-523.81-1571.43-1.65E+0400.000.00E+0000.000.00E+00-960-2880.00-3.02E+04-9700-9700.00-6.11E+04-14151.43-1.08E+05119.700.950.000.000.00E+000.000.000.00E+00-523.81-1047.62-6.60E+0300.000.00E+0000.000.00E+00-960-1920.00-1.21E+0400.000.00E+00-2967.62-1.87E+04126.001.000.000.000.00E+000.000.000.00E+00-523.81-523.810.00E+000.000.000.0E+0000-960-9600000-1483.810.00E+00-40000.00-5000.00-11000.00-13000-4600-4800-9700

&APage &P

Sheet5

&APage &Px/LV & M Total

Sheet6Acceleration (Intercept)Sustained Turn RateH (f)6,000H (f)55,000Mach No.0.8Mach No.2.1W/S (lb/f^2)170y-dot0.78deg/sV (f/s)866.88V (f/s)1925.7rho (lbm/f^3)0.0644752294rho (lbm/f^3)0.0092227644q (lbf/f^2)752.3587831548q (lbf/f^2)531.0709037106n0.8301565936n1.2895119789Instantaneous Turn RateClimbH (f)55,000CD_00.007Mach No.2.1C_L1.2y-dot0.94deg/sg (deg)11V (f/s)1925.7G (rad)0.1908089954rho (lbm/f^3)0.0092227644T/W_min0.2654442619q (lbf/f^2)531.0709037106T/W_actual0.265445n1.4009520775T/W - G0.0746360046n +6.4258230208n -6.3689206289Highest aH (f)55,000Max q (dive)Mach No.2.1H (f)55,000CL1.00Mach No.2.1W/S (lb/f^2)157CL0.20W/S (lb/f^2)157V (f/s)1925.7rho (lbm/f^3)0.0092227644V_dive (f/s)2888.55q (lbf/f^2)531.0709037106rho (lbm/f^3)0.0092227644n3.3826172211q_dive (lbf/f^2)1194.9095333488n1.5221777495Gust Loads (cruise)W/S (lb/f^2)157.00H (f)55,000Mach No.2.1V (f/s)2888.55rho (lbm/f^3)0.0092227644CLa2.51/radUhat (f/s)30Table 10.2m628.7613k0.9910u (f/s)29.7292Dn0.20n_peak1.20Design CriteriaF.S.1.5load limit3.38des. load5.07

&APage &P

Sheet7

&APage &P

Sheet8

&APage &P

Sheet9

&APage &P

Sheet10

&APage &P

Sheet11

&APage &P

Sheet12

&APage &P

Sheet13

&APage &P

Sheet14

&APage &P

Sheet15

&APage &P

Sheet16

&APage &P

&APage &P

&APage &P

&APage &P


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