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EMWET_stuff.txt
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*******************************************
EMWET Student Version 1.5
Copyright <C> 2010 Ali Elham, TU Delft
ATTENTION: Student vesion is a simplified version of EMWET.
*******************************************
Geometry Generation ...
Weight Estimation ...
iteration 1...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 10.9115 10.6558 2.3014 1.3253
0.0652 6.3300 9.9463 9.7064 2.2634 1.2268
0.1087 5.7563 10.0649 9.8165 2.2702 1.2059
0.1522 5.1826 10.0246 9.7714 2.2385 1.3188
0.1957 4.6090 9.9295 9.6729 2.4076 1.3130
0.2391 4.0353 10.4611 10.1877 2.5166 1.3775
0.2826 3.4616 11.3898 11.0895 2.6947 1.4896
0.3261 2.8879 12.9209 12.5765 3.0078 1.6936
0.3696 2.3143 16.4412 15.9985 4.0916 2.2882
0.4130 2.1762 15.8153 15.3881 4.0379 2.2455
0.4565 2.1195 14.2507 13.8654 3.7616 2.0997
0.5000 2.0628 12.7075 12.3635 3.4900 1.9580
0.5435 2.0060 11.0979 10.7972 3.1904 1.8271
0.5870 1.9493 9.6180 9.3571 2.9169 1.6887
0.6304 1.8926 8.1764 7.9544 2.6410 1.5476
0.6739 1.8359 6.7852 6.6007 2.3627 1.4025
0.7174 1.7792 5.4622 5.3136 2.0816 1.2528
0.7609 1.7224 4.2784 4.1076 1.7989 1.0980
0.8043 1.6657 3.6555 2.9992 1.5220 0.9368
0.8478 1.6090 2.9883 2.0067 1.2468 0.8000
0.8913 1.5523 2.2759 1.1692 0.9620 0.8000
0.9348 1.4956 1.5430 0.8000 0.8000 0.8000
0.9783 1.4388 0.8000 0.8000 0.8000 0.8000
Wing Weight 5612.3856 kg
iteration 2...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 12.0141 11.7325 2.5823 1.4548
0.0652 6.3300 10.9325 10.6688 2.5425 1.3647
0.1087 5.7563 11.0392 10.7667 2.5542 1.3445
0.1522 5.1826 10.9603 10.6835 2.5314 1.4488
0.1957 4.6090 10.8290 10.5491 2.7171 1.4629
0.2391 4.0353 11.3736 11.0763 2.8356 1.5324
0.2826 3.4616 12.3445 12.0190 3.0337 1.6549
0.3261 2.8879 13.9593 13.5872 3.3870 1.8790
0.3696 2.3143 17.7344 17.2568 4.5764 2.5157
0.4130 2.1762 16.9954 16.5364 4.4979 2.4617
0.4565 2.1195 15.2446 14.8324 4.1634 2.2912
0.5000 2.0628 13.5306 13.1644 3.8373 2.1256
0.5435 2.0060 11.8567 11.5354 3.5140 1.9642
0.5870 1.9493 10.1428 9.8677 3.1621 1.8116
0.6304 1.8926 8.5802 8.3472 2.8427 1.6499
0.6739 1.8359 7.0849 6.8923 2.5249 1.4857
0.7174 1.7792 5.6754 5.5209 2.2086 1.3184
0.7609 1.7224 4.3647 4.2459 1.8933 1.1477
0.8043 1.6657 3.7078 3.0851 1.5903 0.9726
0.8478 1.6090 3.0237 2.0533 1.2904 0.8000
0.8913 1.5523 2.2972 1.1907 0.9894 0.8000
0.9348 1.4956 1.5532 0.8000 0.8000 0.8000
0.9783 1.4388 0.8000 0.8000 0.8000 0.8000
Wing Weight 5983.7666 kg
iteration 3...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 11.9047 11.6256 2.5544 1.4419
0.0652 6.3300 10.8346 10.5733 2.5148 1.3510
0.1087 5.7563 10.9425 10.6724 2.5260 1.3307
0.1522 5.1826 10.8674 10.5929 2.5023 1.4359
0.1957 4.6090 10.7396 10.4621 2.6863 1.4480
0.2391 4.0353 11.2830 10.9880 2.8038 1.5170
0.2826 3.4616 12.2496 11.9267 2.9999 1.6385
0.3261 2.8879 13.8560 13.4866 3.3491 1.8606
0.3696 2.3143 17.6055 17.1314 4.5277 2.4931
0.4130 2.1762 16.8778 16.4219 4.4517 2.4402
0.4565 2.1195 15.1457 14.7361 4.1231 2.2721
0.5000 2.0628 13.4487 13.0847 3.8025 2.1089
0.5435 2.0060 11.7902 11.4707 3.4844 1.9498
0.5870 1.9493 10.0907 9.8170 3.1376 1.7994
0.6304 1.8926 8.5400 8.3082 2.8226 1.6397
0.6739 1.8359 7.0551 6.8634 2.5088 1.4774
0.7174 1.7792 5.6542 5.5004 2.1960 1.3119
0.7609 1.7224 4.3508 4.2323 1.8840 1.1427
0.8043 1.6657 3.7027 3.0766 1.5835 0.9690
0.8478 1.6090 3.0202 2.0487 1.2860 0.8000
0.8913 1.5523 2.2951 1.1886 0.9867 0.8000
0.9348 1.4956 1.5522 0.8000 0.8000 0.8000
0.9783 1.4388 0.8000 0.8000 0.8000 0.8000
Wing Weight 5947.171 kg
iteration 4...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 11.9154 11.6362 2.5572 1.4432
0.0652 6.3300 10.8442 10.5827 2.5175 1.3524
0.1087 5.7563 10.9520 10.6817 2.5287 1.3321
0.1522 5.1826 10.8765 10.6018 2.5052 1.4372
0.1957 4.6090 10.7484 10.4707 2.6893 1.4495
0.2391 4.0353 11.2919 10.9967 2.8070 1.5186
0.2826 3.4616 12.2590 11.9358 3.0033 1.6401
0.3261 2.8879 13.8662 13.4965 3.3528 1.8624
0.3696 2.3143 17.6182 17.1437 4.5325 2.4953
0.4130 2.1762 16.8894 16.4332 4.4563 2.4423
0.4565 2.1195 15.1554 14.7456 4.1271 2.2740
0.5000 2.0628 13.4568 13.0925 3.8059 2.1106
0.5435 2.0060 11.7968 11.4771 3.4874 1.9512
0.5870 1.9493 10.0958 9.8220 3.1400 1.8006
0.6304 1.8926 8.5440 8.3120 2.8245 1.6407
0.6739 1.8359 7.0580 6.8662 2.5104 1.4782
0.7174 1.7792 5.6563 5.5024 2.1972 1.3125
0.7609 1.7224 4.3522 4.2336 1.8849 1.1432
0.8043 1.6657 3.7032 3.0774 1.5842 0.9694
0.8478 1.6090 3.0206 2.0492 1.2864 0.8000
0.8913 1.5523 2.2953 1.1888 0.9870 0.8000
0.9348 1.4956 1.5523 0.8000 0.8000 0.8000
0.9783 1.4388 0.8000 0.8000 0.8000 0.8000
Wing Weight 5950.7781 kg
Solution is converged
*******************************************
EMWET Student Version 1.5
Copyright <C> 2010 Ali Elham, TU Delft
ATTENTION: Student vesion is a simplified version of EMWET.
*******************************************
Geometry Generation ...
Weight Estimation ...
iteration 1...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 10.9115 10.6558 2.3014 1.3253
0.0652 6.3300 9.9463 9.7064 2.2634 1.2268
0.1087 5.7563 10.0649 9.8165 2.2702 1.2059
0.1522 5.1826 10.0246 9.7714 2.2385 1.3188
0.1957 4.6090 9.9295 9.6729 2.4076 1.3130
0.2391 4.0353 10.4611 10.1877 2.5166 1.3775
0.2826 3.4616 11.3898 11.0895 2.6947 1.4896
0.3261 2.8879 12.9209 12.5765 3.0078 1.6936
0.3696 2.3143 16.4412 15.9985 4.0916 2.2882
0.4130 2.1762 15.8153 15.3881 4.0379 2.2455
0.4565 2.1195 14.2507 13.8654 3.7616 2.0997
0.5000 2.0628 12.7075 12.3635 3.4900 1.9580
0.5435 2.0060 11.0979 10.7972 3.1904 1.8271
0.5870 1.9493 9.6180 9.3571 2.9169 1.6887
0.6304 1.8926 8.1764 7.9544 2.6410 1.5476
0.6739 1.8359 6.7852 6.6007 2.3627 1.4025
0.7174 1.7792 5.4622 5.3136 2.0816 1.2528
0.7609 1.7224 4.2784 4.1076 1.7989 1.0980
0.8043 1.6657 3.6555 2.9992 1.5220 0.9368
0.8478 1.6090 2.9883 2.0067 1.2468 0.8000
0.8913 1.5523 2.2759 1.1692 0.9620 0.8000
0.9348 1.4956 1.5430 0.8000 0.8000 0.8000
0.9783 1.4388 0.8000 0.8000 0.8000 0.8000
Wing Weight 5612.3856 kg
iteration 2...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 12.0141 11.7325 2.5823 1.4548
0.0652 6.3300 10.9325 10.6688 2.5425 1.3647
0.1087 5.7563 11.0392 10.7667 2.5542 1.3445
0.1522 5.1826 10.9603 10.6835 2.5314 1.4488
0.1957 4.6090 10.8290 10.5491 2.7171 1.4629
0.2391 4.0353 11.3736 11.0763 2.8356 1.5324
0.2826 3.4616 12.3445 12.0190 3.0337 1.6549
0.3261 2.8879 13.9593 13.5872 3.3870 1.8790
0.3696 2.3143 17.7344 17.2568 4.5764 2.5157
0.4130 2.1762 16.9954 16.5364 4.4979 2.4617
0.4565 2.1195 15.2446 14.8324 4.1634 2.2912
0.5000 2.0628 13.5306 13.1644 3.8373 2.1256
0.5435 2.0060 11.8567 11.5354 3.5140 1.9642
0.5870 1.9493 10.1428 9.8677 3.1621 1.8116
0.6304 1.8926 8.5802 8.3472 2.8427 1.6499
0.6739 1.8359 7.0849 6.8923 2.5249 1.4857
0.7174 1.7792 5.6754 5.5209 2.2086 1.3184
0.7609 1.7224 4.3647 4.2459 1.8933 1.1477
0.8043 1.6657 3.7078 3.0851 1.5903 0.9726
0.8478 1.6090 3.0237 2.0533 1.2904 0.8000
0.8913 1.5523 2.2972 1.1907 0.9894 0.8000
0.9348 1.4956 1.5532 0.8000 0.8000 0.8000
0.9783 1.4388 0.8000 0.8000 0.8000 0.8000
Wing Weight 5983.7666 kg
iteration 3...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 11.9047 11.6256 2.5544 1.4419
0.0652 6.3300 10.8346 10.5733 2.5148 1.3510
0.1087 5.7563 10.9425 10.6724 2.5260 1.3307
0.1522 5.1826 10.8674 10.5929 2.5023 1.4359
0.1957 4.6090 10.7396 10.4621 2.6863 1.4480
0.2391 4.0353 11.2830 10.9880 2.8038 1.5170
0.2826 3.4616 12.2496 11.9267 2.9999 1.6385
0.3261 2.8879 13.8560 13.4866 3.3491 1.8606
0.3696 2.3143 17.6055 17.1314 4.5277 2.4931
0.4130 2.1762 16.8778 16.4219 4.4517 2.4402
0.4565 2.1195 15.1457 14.7361 4.1231 2.2721
0.5000 2.0628 13.4487 13.0847 3.8025 2.1089
0.5435 2.0060 11.7902 11.4707 3.4844 1.9498
0.5870 1.9493 10.0907 9.8170 3.1376 1.7994
0.6304 1.8926 8.5400 8.3082 2.8226 1.6397
0.6739 1.8359 7.0551 6.8634 2.5088 1.4774
0.7174 1.7792 5.6542 5.5004 2.1960 1.3119
0.7609 1.7224 4.3508 4.2323 1.8840 1.1427
0.8043 1.6657 3.7027 3.0766 1.5835 0.9690
0.8478 1.6090 3.0202 2.0487 1.2860 0.8000
0.8913 1.5523 2.2951 1.1886 0.9867 0.8000
0.9348 1.4956 1.5522 0.8000 0.8000 0.8000
0.9783 1.4388 0.8000 0.8000 0.8000 0.8000
Wing Weight 5947.171 kg
iteration 4...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 11.9154 11.6362 2.5572 1.4432
0.0652 6.3300 10.8442 10.5827 2.5175 1.3524
0.1087 5.7563 10.9520 10.6817 2.5287 1.3321
0.1522 5.1826 10.8765 10.6018 2.5052 1.4372
0.1957 4.6090 10.7484 10.4707 2.6893 1.4495
0.2391 4.0353 11.2919 10.9967 2.8070 1.5186
0.2826 3.4616 12.2590 11.9358 3.0033 1.6401
0.3261 2.8879 13.8662 13.4965 3.3528 1.8624
0.3696 2.3143 17.6182 17.1437 4.5325 2.4953
0.4130 2.1762 16.8894 16.4332 4.4563 2.4423
0.4565 2.1195 15.1554 14.7456 4.1271 2.2740
0.5000 2.0628 13.4568 13.0925 3.8059 2.1106
0.5435 2.0060 11.7968 11.4771 3.4874 1.9512
0.5870 1.9493 10.0958 9.8220 3.1400 1.8006
0.6304 1.8926 8.5440 8.3120 2.8245 1.6407
0.6739 1.8359 7.0580 6.8662 2.5104 1.4782
0.7174 1.7792 5.6563 5.5024 2.1972 1.3125
0.7609 1.7224 4.3522 4.2336 1.8849 1.1432
0.8043 1.6657 3.7032 3.0774 1.5842 0.9694
0.8478 1.6090 3.0206 2.0492 1.2864 0.8000
0.8913 1.5523 2.2953 1.1888 0.9870 0.8000
0.9348 1.4956 1.5523 0.8000 0.8000 0.8000
0.9783 1.4388 0.8000 0.8000 0.8000 0.8000
Wing Weight 5950.7781 kg
Solution is converged
*******************************************
EMWET Student Version 1.5
Copyright <C> 2010 Ali Elham, TU Delft
ATTENTION: Student vesion is a simplified version of EMWET.
*******************************************
Geometry Generation ...
Weight Estimation ...
iteration 1...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 13.4341 13.1192 2.7935 1.5710
0.0652 6.3300 12.2618 11.9661 2.7682 1.4860
0.1087 5.7563 12.4197 12.1132 2.8005 1.4716
0.1522 5.1826 12.3625 12.0503 2.8028 1.5825
0.1957 4.6090 12.2502 11.9336 3.0235 1.6141
0.2391 4.0353 12.9032 12.5660 3.1736 1.6979
0.2826 3.4616 14.0512 13.6807 3.4209 1.8430
0.3261 2.8879 15.9513 15.5261 3.8601 2.1063
0.3696 2.3143 20.4119 19.8623 5.2653 2.8207
0.4130 2.1762 19.6315 19.1012 5.2089 2.7739
0.4565 2.1195 17.6446 17.1674 4.8324 2.5905
0.5000 2.0628 15.6901 15.2654 4.4634 2.4109
0.5435 2.0060 13.7728 13.3996 4.0959 2.2341
0.5870 1.9493 11.9010 11.5782 3.7301 2.0558
0.6304 1.8926 9.9984 9.7269 3.3287 1.8855
0.6739 1.8359 8.2648 8.0402 2.9619 1.7011
0.7174 1.7792 6.6269 6.4466 2.5957 1.5112
0.7609 1.7224 5.1004 4.9615 2.2295 1.3157
0.8043 1.6657 4.0104 3.6069 1.8709 1.1133
0.8478 1.6090 3.2737 2.4042 1.5200 0.9013
0.8913 1.5523 2.4910 1.3965 1.1645 0.8000
0.9348 1.4956 1.6840 0.8000 0.8036 0.8000
0.9783 1.4388 0.8650 0.8000 0.8000 0.8000
Wing Weight 6692.3846 kg
iteration 2...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 14.2249 13.8915 2.9959 1.6638
0.0652 6.3300 12.9693 12.6565 2.9693 1.5848
0.1087 5.7563 13.1194 12.7956 3.0055 1.5708
0.1522 5.1826 13.0354 12.7062 3.0146 1.6759
0.1957 4.6090 12.8979 12.5646 3.2479 1.7215
0.2391 4.0353 13.5621 13.2076 3.4060 1.8091
0.2826 3.4616 14.7431 14.3543 3.6698 1.9619
0.3261 2.8879 16.7083 16.2629 4.1421 2.2402
0.3696 2.3143 21.3686 20.7931 5.6391 2.9867
0.4130 2.1762 20.5058 19.9519 5.5648 2.9318
0.4565 2.1195 18.3783 17.8814 5.1408 2.7302
0.5000 2.0628 16.2956 15.8545 4.7277 2.5330
0.5435 2.0060 14.2626 13.8761 4.3195 2.3394
0.5870 1.9493 12.2879 11.9546 3.9164 2.1450
0.6304 1.8926 10.2936 10.0141 3.4793 1.9594
0.6739 1.8359 8.4831 8.2525 3.0820 1.7610
0.7174 1.7792 6.7809 6.5964 2.6886 1.5585
0.7609 1.7224 5.2032 5.0615 2.2991 1.3514
0.8043 1.6657 4.0447 3.6684 1.9200 1.1389
0.8478 1.6090 3.2969 2.4382 1.5525 0.9184
0.8913 1.5523 2.5049 1.4118 1.1838 0.8000
0.9348 1.4956 1.6906 0.8000 0.8137 0.8000
0.9783 1.4388 0.8670 0.8000 0.8000 0.8000
Wing Weight 6953.3758 kg
iteration 3...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 14.1474 13.8158 2.9760 1.6547
0.0652 6.3300 12.9000 12.5889 2.9496 1.5751
0.1087 5.7563 13.0509 12.7288 2.9854 1.5611
0.1522 5.1826 12.9695 12.6419 2.9938 1.6668
0.1957 4.6090 12.8344 12.5027 3.2259 1.7110
0.2391 4.0353 13.4976 13.1448 3.3832 1.7982
0.2826 3.4616 14.6753 14.2884 3.6453 1.9503
0.3261 2.8879 16.6340 16.1906 4.1144 2.2270
0.3696 2.3143 21.2745 20.7017 5.6021 2.9704
0.4130 2.1762 20.4199 19.8683 5.5296 2.9163
0.4565 2.1195 18.3063 17.8113 5.1104 2.7165
0.5000 2.0628 16.2362 15.7967 4.7017 2.5211
0.5435 2.0060 14.2146 13.8294 4.2975 2.3291
0.5870 1.9493 12.2500 11.9177 3.8981 2.1363
0.6304 1.8926 10.2647 9.9860 3.4645 1.9522
0.6739 1.8359 8.4618 8.2318 3.0702 1.7551
0.7174 1.7792 6.7658 6.5817 2.6795 1.5539
0.7609 1.7224 5.1931 5.0517 2.2923 1.3479
0.8043 1.6657 4.0414 3.6624 1.9152 1.1364
0.8478 1.6090 3.2946 2.4349 1.5493 0.9167
0.8913 1.5523 2.5036 1.4103 1.1819 0.8000
0.9348 1.4956 1.6900 0.8000 0.8127 0.8000
0.9783 1.4388 0.8668 0.8000 0.8000 0.8000
Wing Weight 6927.8693 kg
Solution is converged
*******************************************
EMWET Student Version 1.5
Copyright <C> 2010 Ali Elham, TU Delft
ATTENTION: Student vesion is a simplified version of EMWET.
*******************************************
Geometry Generation ...
Weight Estimation ...
iteration 1...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 13.4341 13.1192 2.7935 1.5710
0.0652 6.3300 12.2618 11.9661 2.7682 1.4860
0.1087 5.7563 12.4197 12.1132 2.8005 1.4716
0.1522 5.1826 12.3625 12.0503 2.8028 1.5825
0.1957 4.6090 12.2502 11.9336 3.0235 1.6141
0.2391 4.0353 12.9032 12.5660 3.1736 1.6979
0.2826 3.4616 14.0512 13.6807 3.4209 1.8430
0.3261 2.8879 15.9513 15.5261 3.8601 2.1063
0.3696 2.3143 20.4119 19.8623 5.2653 2.8207
0.4130 2.1762 19.6315 19.1012 5.2089 2.7739
0.4565 2.1195 17.6446 17.1674 4.8324 2.5905
0.5000 2.0628 15.6901 15.2654 4.4634 2.4109
0.5435 2.0060 13.7728 13.3996 4.0959 2.2341
0.5870 1.9493 11.9010 11.5782 3.7301 2.0558
0.6304 1.8926 9.9984 9.7269 3.3287 1.8855
0.6739 1.8359 8.2648 8.0402 2.9619 1.7011
0.7174 1.7792 6.6269 6.4466 2.5957 1.5112
0.7609 1.7224 5.1004 4.9615 2.2295 1.3157
0.8043 1.6657 4.0104 3.6069 1.8709 1.1133
0.8478 1.6090 3.2737 2.4042 1.5200 0.9013
0.8913 1.5523 2.4910 1.3965 1.1645 0.8000
0.9348 1.4956 1.6840 0.8000 0.8036 0.8000
0.9783 1.4388 0.8650 0.8000 0.8000 0.8000
Wing Weight 6692.3846 kg
iteration 2...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 14.2249 13.8915 2.9959 1.6638
0.0652 6.3300 12.9693 12.6565 2.9693 1.5848
0.1087 5.7563 13.1194 12.7956 3.0055 1.5708
0.1522 5.1826 13.0354 12.7062 3.0146 1.6759
0.1957 4.6090 12.8979 12.5646 3.2479 1.7215
0.2391 4.0353 13.5621 13.2076 3.4060 1.8091
0.2826 3.4616 14.7431 14.3543 3.6698 1.9619
0.3261 2.8879 16.7083 16.2629 4.1421 2.2402
0.3696 2.3143 21.3686 20.7931 5.6391 2.9867
0.4130 2.1762 20.5058 19.9519 5.5648 2.9318
0.4565 2.1195 18.3783 17.8814 5.1408 2.7302
0.5000 2.0628 16.2956 15.8545 4.7277 2.5330
0.5435 2.0060 14.2626 13.8761 4.3195 2.3394
0.5870 1.9493 12.2879 11.9546 3.9164 2.1450
0.6304 1.8926 10.2936 10.0141 3.4793 1.9594
0.6739 1.8359 8.4831 8.2525 3.0820 1.7610
0.7174 1.7792 6.7809 6.5964 2.6886 1.5585
0.7609 1.7224 5.2032 5.0615 2.2991 1.3514
0.8043 1.6657 4.0447 3.6684 1.9200 1.1389
0.8478 1.6090 3.2969 2.4382 1.5525 0.9184
0.8913 1.5523 2.5049 1.4118 1.1838 0.8000
0.9348 1.4956 1.6906 0.8000 0.8137 0.8000
0.9783 1.4388 0.8670 0.8000 0.8000 0.8000
Wing Weight 6953.3758 kg
iteration 3...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 14.1474 13.8158 2.9760 1.6547
0.0652 6.3300 12.9000 12.5889 2.9496 1.5751
0.1087 5.7563 13.0509 12.7288 2.9854 1.5611
0.1522 5.1826 12.9695 12.6419 2.9938 1.6668
0.1957 4.6090 12.8344 12.5027 3.2259 1.7110
0.2391 4.0353 13.4976 13.1448 3.3832 1.7982
0.2826 3.4616 14.6753 14.2884 3.6453 1.9503
0.3261 2.8879 16.6340 16.1906 4.1144 2.2270
0.3696 2.3143 21.2745 20.7017 5.6021 2.9704
0.4130 2.1762 20.4199 19.8683 5.5296 2.9163
0.4565 2.1195 18.3063 17.8113 5.1104 2.7165
0.5000 2.0628 16.2362 15.7967 4.7017 2.5211
0.5435 2.0060 14.2146 13.8294 4.2975 2.3291
0.5870 1.9493 12.2500 11.9177 3.8981 2.1363
0.6304 1.8926 10.2647 9.9860 3.4645 1.9522
0.6739 1.8359 8.4618 8.2318 3.0702 1.7551
0.7174 1.7792 6.7658 6.5817 2.6795 1.5539
0.7609 1.7224 5.1931 5.0517 2.2923 1.3479
0.8043 1.6657 4.0414 3.6624 1.9152 1.1364
0.8478 1.6090 3.2946 2.4349 1.5493 0.9167
0.8913 1.5523 2.5036 1.4103 1.1819 0.8000
0.9348 1.4956 1.6900 0.8000 0.8127 0.8000
0.9783 1.4388 0.8668 0.8000 0.8000 0.8000
Wing Weight 6927.8693 kg
Solution is converged
*******************************************
EMWET Student Version 1.5
Copyright <C> 2010 Ali Elham, TU Delft
ATTENTION: Student vesion is a simplified version of EMWET.
*******************************************
Geometry Generation ...
Weight Estimation ...
iteration 1...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 13.4341 13.1192 2.7935 1.5710
0.0652 6.3300 12.2618 11.9661 2.7682 1.4860
0.1087 5.7563 12.4197 12.1132 2.8005 1.4716
0.1522 5.1826 12.3625 12.0503 2.8028 1.5825
0.1957 4.6090 12.2502 11.9336 3.0235 1.6141
0.2391 4.0353 12.9032 12.5660 3.1736 1.6979
0.2826 3.4616 14.0512 13.6807 3.4209 1.8430
0.3261 2.8879 15.9513 15.5261 3.8601 2.1063
0.3696 2.3143 20.4119 19.8623 5.2653 2.8207
0.4130 2.1762 19.6315 19.1012 5.2089 2.7739
0.4565 2.1195 17.6446 17.1674 4.8324 2.5905
0.5000 2.0628 15.6901 15.2654 4.4634 2.4109
0.5435 2.0060 13.7728 13.3996 4.0959 2.2341
0.5870 1.9493 11.9010 11.5782 3.7301 2.0558
0.6304 1.8926 9.9984 9.7269 3.3287 1.8855
0.6739 1.8359 8.2648 8.0402 2.9619 1.7011
0.7174 1.7792 6.6269 6.4466 2.5957 1.5112
0.7609 1.7224 5.1004 4.9615 2.2295 1.3157
0.8043 1.6657 4.0104 3.6069 1.8709 1.1133
0.8478 1.6090 3.2737 2.4042 1.5200 0.9013
0.8913 1.5523 2.4910 1.3965 1.1645 0.8000
0.9348 1.4956 1.6840 0.8000 0.8036 0.8000
0.9783 1.4388 0.8650 0.8000 0.8000 0.8000
Wing Weight 6692.3846 kg
iteration 2...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 14.2249 13.8915 2.9959 1.6638
0.0652 6.3300 12.9693 12.6565 2.9693 1.5848
0.1087 5.7563 13.1194 12.7956 3.0055 1.5708
0.1522 5.1826 13.0354 12.7062 3.0146 1.6759
0.1957 4.6090 12.8979 12.5646 3.2479 1.7215
0.2391 4.0353 13.5621 13.2076 3.4060 1.8091
0.2826 3.4616 14.7431 14.3543 3.6698 1.9619
0.3261 2.8879 16.7083 16.2629 4.1421 2.2402
0.3696 2.3143 21.3686 20.7931 5.6391 2.9867
0.4130 2.1762 20.5058 19.9519 5.5648 2.9318
0.4565 2.1195 18.3783 17.8814 5.1408 2.7302
0.5000 2.0628 16.2956 15.8545 4.7277 2.5330
0.5435 2.0060 14.2626 13.8761 4.3195 2.3394
0.5870 1.9493 12.2879 11.9546 3.9164 2.1450
0.6304 1.8926 10.2936 10.0141 3.4793 1.9594
0.6739 1.8359 8.4831 8.2525 3.0820 1.7610
0.7174 1.7792 6.7809 6.5964 2.6886 1.5585
0.7609 1.7224 5.2032 5.0615 2.2991 1.3514
0.8043 1.6657 4.0447 3.6684 1.9200 1.1389
0.8478 1.6090 3.2969 2.4382 1.5525 0.9184
0.8913 1.5523 2.5049 1.4118 1.1838 0.8000
0.9348 1.4956 1.6906 0.8000 0.8137 0.8000
0.9783 1.4388 0.8670 0.8000 0.8000 0.8000
Wing Weight 6953.3758 kg
iteration 3...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 14.1474 13.8158 2.9760 1.6547
0.0652 6.3300 12.9000 12.5889 2.9496 1.5751
0.1087 5.7563 13.0509 12.7288 2.9854 1.5611
0.1522 5.1826 12.9695 12.6419 2.9938 1.6668
0.1957 4.6090 12.8344 12.5027 3.2259 1.7110
0.2391 4.0353 13.4976 13.1448 3.3832 1.7982
0.2826 3.4616 14.6753 14.2884 3.6453 1.9503
0.3261 2.8879 16.6340 16.1906 4.1144 2.2270
0.3696 2.3143 21.2745 20.7017 5.6021 2.9704
0.4130 2.1762 20.4199 19.8683 5.5296 2.9163
0.4565 2.1195 18.3063 17.8113 5.1104 2.7165
0.5000 2.0628 16.2362 15.7967 4.7017 2.5211
0.5435 2.0060 14.2146 13.8294 4.2975 2.3291
0.5870 1.9493 12.2500 11.9177 3.8981 2.1363
0.6304 1.8926 10.2647 9.9860 3.4645 1.9522
0.6739 1.8359 8.4618 8.2318 3.0702 1.7551
0.7174 1.7792 6.7658 6.5817 2.6795 1.5539
0.7609 1.7224 5.1931 5.0517 2.2923 1.3479
0.8043 1.6657 4.0414 3.6624 1.9152 1.1364
0.8478 1.6090 3.2946 2.4349 1.5493 0.9167
0.8913 1.5523 2.5036 1.4103 1.1819 0.8000
0.9348 1.4956 1.6900 0.8000 0.8127 0.8000
0.9783 1.4388 0.8668 0.8000 0.8000 0.8000
Wing Weight 6927.8693 kg
Solution is converged
*******************************************
EMWET Student Version 1.5
Copyright <C> 2010 Ali Elham, TU Delft
ATTENTION: Student vesion is a simplified version of EMWET.
*******************************************
Geometry Generation ...
Weight Estimation ...
iteration 1...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 13.4403 13.1253 2.7948 1.5703
0.0652 6.3300 12.2676 11.9717 2.7697 1.4869
0.1087 5.7563 12.4252 12.1186 2.8023 1.4726
0.1522 5.1826 12.3671 12.0548 2.8048 1.5814
0.1957 4.6090 12.2545 11.9378 3.0260 1.6154
0.2391 4.0353 12.9070 12.5696 3.1764 1.6994
0.2826 3.4616 14.0540 13.6834 3.4243 1.8448
0.3261 2.8879 15.9525 15.5273 3.8644 2.1085
0.3696 2.3143 20.4119 19.8623 5.2653 2.8207
0.4130 2.1762 19.6315 19.1012 5.2089 2.7739
0.4565 2.1195 17.6446 17.1674 4.8324 2.5905
0.5000 2.0628 15.6901 15.2654 4.4634 2.4109
0.5435 2.0060 13.7728 13.3996 4.0959 2.2341
0.5870 1.9493 11.9010 11.5782 3.7301 2.0558
0.6304 1.8926 9.9984 9.7269 3.3287 1.8855
0.6739 1.8359 8.2648 8.0402 2.9619 1.7011
0.7174 1.7792 6.6269 6.4466 2.5957 1.5112
0.7609 1.7224 5.1004 4.9615 2.2295 1.3157
0.8043 1.6657 4.0104 3.6069 1.8709 1.1133
0.8478 1.6090 3.2737 2.4042 1.5200 0.9013
0.8913 1.5523 2.4910 1.3965 1.1645 0.8000
0.9348 1.4956 1.6840 0.8000 0.8036 0.8000
0.9783 1.4388 0.8650 0.8000 0.8000 0.8000
Wing Weight 6693.4415 kg
iteration 2...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 14.2308 13.8972 2.9971 1.6630
0.0652 6.3300 12.9747 12.6618 2.9708 1.5856
0.1087 5.7563 13.1247 12.8008 3.0072 1.5717
0.1522 5.1826 13.0398 12.7104 3.0165 1.6749
0.1957 4.6090 12.9020 12.5686 3.2503 1.7228
0.2391 4.0353 13.5656 13.2110 3.4088 1.8106
0.2826 3.4616 14.7456 14.3568 3.6731 1.9636
0.3261 2.8879 16.7092 16.2638 4.1463 2.2423
0.3696 2.3143 21.3682 20.7928 5.6390 2.9866
0.4130 2.1762 20.5054 19.9516 5.5647 2.9318
0.4565 2.1195 18.3780 17.8811 5.1407 2.7302
0.5000 2.0628 16.2953 15.8543 4.7276 2.5330
0.5435 2.0060 14.2624 13.8760 4.3195 2.3394
0.5870 1.9493 12.2877 11.9544 3.9164 2.1450
0.6304 1.8926 10.2934 10.0140 3.4792 1.9594
0.6739 1.8359 8.4830 8.2524 3.0819 1.7610
0.7174 1.7792 6.7808 6.5963 2.6886 1.5585
0.7609 1.7224 5.2032 5.0615 2.2990 1.3514
0.8043 1.6657 4.0447 3.6684 1.9200 1.1389
0.8478 1.6090 3.2969 2.4382 1.5525 0.9184
0.8913 1.5523 2.5049 1.4118 1.1838 0.8000
0.9348 1.4956 1.6906 0.8000 0.8137 0.8000
0.9783 1.4388 0.8670 0.8000 0.8000 0.8000
Wing Weight 6954.326 kg
iteration 3...
y/(b/2) Chord[m] tu[mm] tl[mm] tfs[mm] trs[mm]
0.0217 6.9037 14.1533 13.8216 2.9773 1.6539
0.0652 6.3300 12.9055 12.5942 2.9511 1.5760
0.1087 5.7563 13.0562 12.7339 2.9871 1.5620
0.1522 5.1826 12.9739 12.6462 2.9957 1.6657
0.1957 4.6090 12.8386 12.5068 3.2283 1.7123
0.2391 4.0353 13.5011 13.1482 3.3860 1.7997
0.2826 3.4616 14.6779 14.2909 3.6487 1.9520
0.3261 2.8879 16.6350 16.1916 4.1185 2.2292
0.3696 2.3143 21.2742 20.7013 5.6020 2.9703
0.4130 2.1762 20.4196 19.8680 5.5295 2.9163
0.4565 2.1195 18.3060 17.8110 5.1102 2.7165
0.5000 2.0628 16.2359 15.7965 4.7016 2.5210
0.5435 2.0060 14.2144 13.8292 4.2975 2.3291
0.5870 1.9493 12.2498 11.9176 3.8981 2.1362
0.6304 1.8926 10.2646 9.9859 3.4645 1.9522
0.6739 1.8359 8.4617 8.2317 3.0702 1.7551
0.7174 1.7792 6.7657 6.5817 2.6795 1.5538
0.7609 1.7224 5.1931 5.0517 2.2922 1.3479
0.8043 1.6657 4.0413 3.6624 1.9152 1.1364
0.8478 1.6090 3.2946 2.4348 1.5493 0.9167
0.8913 1.5523 2.5036 1.4103 1.1819 0.8000
0.9348 1.4956 1.6900 0.8000 0.8127 0.8000
0.9783 1.4388 0.8668 0.8000 0.8000 0.8000
Wing Weight 6928.8302 kg
Solution is converged