AE1222-II Tutorial 1 - Test 2-2 q2
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Naam OEW [N] 105422.47 Gulfstream G280 107424.99 Cessna Citation X 98305.782 Bombardier Learjet 85 106090.3 Dassault Falcon 2000LX 104373.16 Embraer Legacy 600 133806.84 Dassault Falcon 2000S 110093.38 Gulfstream G150 67167.707 Bombardier Challenger 605 120768.89 Cessna Citation TEN 99924.86 Range [m] 6482000 Time [s] 28800 Velocity[m/s] 225.06944 Acceleration of Gravity [m/s^2] 9.80665 Cruise Height [m] Temperature (kelvin) Mach # 0 0.65 Cj cruise - new calc cj cruise [kg/Ns] 1.84E-05 cj loiter [lbs/hr/lbs] 0.5 cj loiter [kg/Ns] 1.415E-05 Weight Passenger + luggage[kg] 95 Oswald factor 0.75 Zero-lift drag coefficient 0.026 Aspect Ratio 9 (L/D) cruise 12.366329 (L/D) loiter 14.279406 E (loiter time / Endurence) [s] 2700 Fuel-Weigth Estimation Method:(bussiness jet) W5/W4 (cruise) 0.6569687 W1/Wto (engine start) 0.99 W2/W1 (taxi) 0.995 W3/W2 (take-off) 0.995 W4/W3 (climb) 0.98 W9/W8 (Loiter phase) 0.9741032 W10/W9 (Descend) 0.99 W11/W10 (Landing,Taxi, Shutdown) 0.992 Mff 0.6036761 Wf [N] 178096.85 We [N] 257336.59 WPLtot [N] 13974.476 hawker Beechcraft Hawker 4000 cj cruise [lbs/hr/lbs]
description
aerospace excel file
Transcript of AE1222-II Tutorial 1 - Test 2-2 q2
Naam OEW [N] MTOW [N]105422.47 175704.767385
Gulfstream G280 107424.99 176149.989295Cessna Citation X 98305.782 160580.951755Bombardier Learjet 85 106090.3 163249.34122Dassault Falcon 2000LX 104373.16 187714.97164Embraer Legacy 600 133806.84 220639.81835Dassault Falcon 2000S 110093.38 182377.212045Gulfstream G150 67167.707 116098.96802Bombardier Challenger 605 120768.89 214404.75028Cessna Citation TEN 99924.86 162805.099975
Range [m] 6482000Time [s] 28800Velocity[m/s] 225.06944Acceleration of Gravity [m/s^2] 9.80665Cruise Height [m]Temperature (kelvin)Mach # 0
0.65Cj cruise - new calccj cruise [kg/Ns] 1.8395E-05cj loiter [lbs/hr/lbs] 0.5cj loiter [kg/Ns] 1.415E-05Weight Passenger + luggage[kg] 95Oswald factor 0.75Zero-lift drag coefficient 0.026Aspect Ratio 9 1% extra (L/D)(L/D) cruise 12.366329 12.4899919536585(L/D) loiter 14.279406E (loiter time / Endurence) [s] 2700
Fuel-Weigth Estimation Method:(bussiness jet)W5/W4 (cruise) 0.6569687 0.659707146408695W1/Wto (engine start) 0.99W2/W1 (taxi) 0.995W3/W2 (take-off) 0.995W4/W3 (climb) 0.98W9/W8 (Loiter phase) 0.9741032W10/W9 (Descend) 0.99W11/W10 (Landing,Taxi, Shutdown) 0.992Mff 0.6036761 0.606192374093653
Wf [N] 178096.85 176966.107732687We [N] 257336.59WPLtot [N] 13974.476
hawker Beechcraft Hawker 4000
cj cruise [lbs/hr/lbs]
WTO [N] 449371.97 426933.17465092 Effect [%]MTOW [kN] 449.37197 426.93317465092 -4.9933673OEW [kN] 257.33659Wfuel [kN] 178.09685
a = 0.5558b = 7539.7
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100000
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f(x) = 0.555757975364976 x + 7539.66810658814R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7539.66810658814R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
Naam OEW [N] MTOW [N]105458.48 175764.789
Gulfstream G280 107461.68 176210.163Cessna Citation X 98339.364 160635.807Bombardier Learjet 85 106126.54 163305.108Dassault Falcon 2000LX 104408.81 187779.096Embraer Legacy 600 133852.55 220715.19Dassault Falcon 2000S 110130.98 182439.513Gulfstream G150 67190.652 116138.628Bombardier Challenger 605 120810.15 214477.992Cessna Citation TEN 99958.995 162860.715
Range [m] 9000000Time [s]Velocity[m/s] 231Acceleration of Gravity [m/s^2] 9.81
1% extra Cjcj cruise [kg/Ns] 0.0000126 0.000012726cj loiter [lbs/hr/lbs]cj loiter [kg/Ns]Weight Passenger + luggage[kg]Oswald factorZero-lift drag coefficientAspect Ratio(L/D) cruise 12.5(L/D) loiter 12.5E (loiter time / Endurence) [s]
Fuel-Weigth Estimation Method:(bussiness jet)W5/W4 (cruise) 0.68027 0.67765422816239W1/Wto (engine start) 0.97W2/W1 (taxi) 1W3/W2 (take-off) 1W4/W3 (climb) 1W9/W8 (Loiter phase) 1W10/W9 (Descend) 0.98W11/W10 (Landing,Taxi, Shutdown) 1Mff 0.6466647 0.644178109291168
Wf [N] 157569.71 158678.599985977We [N] 255434.12WPLtot [N] 100000WTO [N] 445949.52 450490.833594061 Effect [%]MTOW [kN] 445.94952 450.490833594061 1.0183479OEW [kN] 255.43412Wfuel [kN] 157.56971
hawker Beechcraft Hawker 4000
cj cruise [lbs/hr/lbs]
a = 0.4b = 10000
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7542.24369439403R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7542.24369439403R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
Naam OEW [N] MTOW [N]105422.47 175704.767385
Gulfstream G280 107424.99 176149.989295Cessna Citation X 98305.782 160580.951755Bombardier Learjet 85 106090.3 163249.34122Dassault Falcon 2000LX 104373.16 187714.97164Embraer Legacy 600 133806.84 220639.81835Dassault Falcon 2000S 110093.38 182377.212045Gulfstream G150 67167.707 116098.96802Bombardier Challenger 605 120768.89 214404.75028Cessna Citation TEN 99924.86 162805.099975
Range [m] 6482000Time [s] 28800 1 % extra v [m/s]Velocity[m/s] 225.06944 227.320138888889Acceleration of Gravity [m/s^2] 9.80665
0.65cj cruise [kg/Ns] 1.8395E-05cj loiter [lbs/hr/lbs] 0.5cj loiter [kg/Ns] 1.415E-05Weight Passenger + luggage[kg] 95Oswald factor 0.75Zero-lift drag coefficient 0.026Aspect Ratio 9(L/D) cruise 12.366329(L/D) loiter 14.279406E (loiter time / Endurence) [s] 2700
Fuel-Weigth Estimation Method:(bussiness jet)W5/W4 (cruise) 0.6569687 0.659707146408695W1/Wto (engine start) 0.99W2/W1 (taxi) 0.995W3/W2 (take-off) 0.995W4/W3 (climb) 0.98W9/W8 (Loiter phase) 0.9741032W10/W9 (Descend) 0.99W11/W10 (Landing,Taxi, Shutdown) 0.992Mff 0.6036761 0.606192374093653
Wf [N] 178096.85 176966.107732687We [N] 257336.59WPLtot [N] 13974.476WTO [N] 449371.97 426933.17465092 Effect [%]MTOW [kN] 449.37197 426.93317465092 -4.9933673OEW [kN] 257.33659Wfuel [kN] 178.09685
hawker Beechcraft Hawker 4000
cj cruise [lbs/hr/lbs]
a = 0.5558b = 7539.7
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7539.66810658814R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7539.66810658814R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
Naam OEW [N] MTOW [N]105458.48 175764.789
Gulfstream G280 107461.68 176210.163Cessna Citation X 98339.364 160635.807Bombardier Learjet 85 106126.54 163305.108Dassault Falcon 2000LX 104408.81 187779.096Embraer Legacy 600 133852.55 220715.19Dassault Falcon 2000S 110130.98 182439.513Gulfstream G150 67190.652 116138.628Bombardier Challenger 605 120810.15 214477.992Cessna Citation TEN 99958.995 162860.715
Range [m] 9000000Time [s]Velocity[m/s] 224Acceleration of Gravity [m/s^2] 9.81 1 % extra altitudeCruise Altitude [m] 8800 8888Temperature (kelvin) 230.95 230.378a [m/s] 304.62388 304.246413947642Mach # 0.735333 0.736245325272916
Cj cruise - new calc 1.5353E-05 1.536245325273E-05cj cruise [kg/Ns]cj loiter [lbs/hr/lbs]cj loiter [kg/Ns]Weight Passenger + luggage[kg]Oswald factorZero-lift drag coefficientAspect Ratio(L/D) cruise 15(L/D) loiter 15E (loiter time / Endurence) [s]
Fuel-Weigth Estimation Method:(bussiness jet)W5/W4 (cruise) 0.6680207 0.667860545028247W1/Wto (engine start) 0.97W2/W1 (taxi) 1W3/W2 (take-off) 1W4/W3 (climb) 1W9/W8 (Loiter phase) 1W10/W9 (Descend) 0.98W11/W10 (Landing,Taxi, Shutdown) 1Mff 0.6350204 0.634868234103852
Wf [N] 170826.63 170897.872877812We [N] 267716.21
hawker Beechcraft Hawker 4000
cj cruise [lbs/hr/lbs]
WPLtot [N] 100000WTO [N] 468044.39 468347.711727424 Effect [%]MTOW [kN] 468.04439 468.347711727424 0.0648072OEW [kN] 267.71621Wfuel [kN] 170.82663
a = 0.4b = 10000
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7542.24369439403R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7542.24369439403R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
Naam OEW [N] MTOW [N]105458.48 175764.789
Gulfstream G280 107461.68 176210.163Cessna Citation X 98339.364 160635.807Bombardier Learjet 85 106126.54 163305.108Dassault Falcon 2000LX 104408.81 187779.096Embraer Legacy 600 133852.55 220715.19Dassault Falcon 2000S 110130.98 182439.513Gulfstream G150 67190.652 116138.628Bombardier Challenger 605 120810.15 214477.992Cessna Citation TEN 99958.995 162860.715
Range [m] 9000000Time [s] 1 % extra velocityVelocity[m/s] 217 219.17Acceleration of Gravity [m/s^2] 9.81Cruise Altitude [m] 9200Temperature (kelvin) 228.35a [m/s] 302.90432Mach # 0.7163978 0.723561804949016
0.65Cj cruise - new calc 1.5164E-05 1.523561804949E-05cj cruise [kg/Ns] 1.8395E-05cj loiter [lbs/hr/lbs] 0.5cj loiter [kg/Ns] 1.415E-05Weight Passenger + luggage[kg] 95Oswald factor 0.75Zero-lift drag coefficient 0.026Aspect Ratio 9(L/D) cruise 15(L/D) loiter 15E (loiter time / Endurence) [s] 2700
Fuel-Weigth Estimation Method:(bussiness jet)W5/W4 (cruise) 0.6627787 0.664204160420535W1/Wto (engine start) 0.97W2/W1 (taxi) 1W3/W2 (take-off) 1W4/W3 (climb) 1W9/W8 (Loiter phase) 1W10/W9 (Descend) 0.98W11/W10 (Landing,Taxi, Shutdown) 1Mff 0.6300374 0.631392474895761
Wf [N] 176909.86 176261.89087148We [N] 273352.12
hawker Beechcraft Hawker 4000
cj cruise [lbs/hr/lbs]
WPLtot [N] 100000WTO [N] 478183.1 475382.788699389MTOW [kN] 478.1831 475.382788699389OEW [kN] 273.35212Wfuel [kN] 176.90986
a = 0.4b = 10000
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7542.24369439403R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
Effect [%]-0.585615896178
100000 120000 140000 160000 180000 200000 220000 2400000
20000
40000
60000
80000
100000
120000
140000
160000
f(x) = 0.555757975364976 x + 7542.24369439403R² = 0.923037597791124
MTOW/OEW
OEW [N]
MTO
W [N
]
