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Project Wing Design (draft)-2.xlsx

Comparison

	Wing1	Wing2	Wing3	Wing4	Wing5	Wing6	Wing7
Cost [$]	$141.07	$102.69	$83.19	$82.61
S.F.	4.66	3.18	1.23	1.20

Cost vs Saftety Factor

[CELLRANGE] [CELLRANGE] [CELLRANGE] [CELLRANGE] 141.06713807337371 102.69055917264349 83.190315755592621 82.607554471019782 4.6566705397179655 3.1758046329607406 1.2302870947509152 1.2041075880449656 Wing1 Wing2 Wing3 Wing4 Wing5 Wing6 Wing7 Cost [$] Safety Factor

Wing1

Total Cost	$141.07		Min S.F.	4.66						Density Aluminum [kg/m3]:				Yeald Stress:
										2650				276000000
	Individual Stringers			Diameters [m]
Section	X1 (m)	X2 (m)	#	String1	String2	String3	String4	String5	String6	String7	String8				Variables
1	0.00	0.20	5	0.03	0.03	0.03	0.03	0.03
2	0.20	0.40	4	0.025	0.025	0.025	0.025								Constants
3	0.40	0.60	3	0.015	0.015	0.015
4	0.60	1.00	2	0.01	0.01										Change Manually if variables are changed
5
6															Delete this cell
7
8
													Total # Ribs:		5
	Stringer Weight [N]										Rib Dimensions
Section	String1	String2	String3	String4	String5	String6	String7	String8		Rib	Length [m]	Volume [m3]	Mass [kg]	Weight [N]	X [m]
1	1.322389962	1.322389962	1.322389962	1.322389962	1.322389962					1	0.2	0.0006	1.59	15.5979	0
2	1.077502932	1.077502932	1.077502932	1.077502932						2	0.18	0.00054	1.431	14.03811	0.2
3	0.587728872	0.587728872	0.587728872							3	0.16	0.00048	1.272	12.47832	0.4
4	0.685683684	0.685683684								4	0.14	0.00042	1.113	10.91853	0.6
5										5	0.1	0.0003	0.795	7.79895	1
6										6		0	0	0
7										7		0	0	0
8										8		0	0	0
Load Fuselage [N]		Load Fuel [N]		Total Ribs [N]		Total Stringers [N]		Total Load [N]		Lift [N]
147		98		60.83181		14.056515522		246.388325522		739.164976566
Shear Foce								Bending Moment [CW+]
Other	Load [N]	Ribs	Load [N]	Lift [N]	Stringer	Load [N]		Other	BM [N]	Ribs	BM [Nm]	Lift [Nm]	Stringer	BM [Nm]
ReactionA	-492.776651044	1	-15.5979	189.5294811708	1	-6.61194981		M0	233.2499595607	1	0	0	1	-0.661194981
Fuselage Mateo: Fuselage is divided between both wings.	-73.5	2	-14.03811	170.5765330537	2	-4.310011728		Fuel	-9.8	2	-2.807622	34.1153066107	2	-1.2930035184
Fuel	-98	3	-12.47832	151.6235849366	3	-1.763186616		Fuselage	0	3	-4.991328	60.6494339746	3	-0.881593308
		4	-10.91853	132.6706368195	4	-1.371367368				4	-6.551118	79.6023820917	4	-1.0970938944
		5	-7.79895	94.7647405854	5	0				5	-7.79895	94.7647405854	5	0
		6	0		6	0				6	0	0	6	0
		7	0		7	0				7	0	0	7	0
		8	0		8	0				8	0	0	8	0
Shear Force Diagram Data
	[start]	Ra	Fuselage+Rib1+Lift1	[stop]	Fuel (start)	[stop]	Stringer1	Fuel (end)	[stop]	Rib2	[stop]	Stringer2	[stop]	Rib3	[stop]	Stringer3	[stop]	Rib4	[stop]	Stringer4	[stop]	Rib5
X [m]	0	0	0	0.025	0.025	0.1	0.1	0.175	0.2	0.2	0.3	0.3	0.4	0.4	0.5	0.5	0.6	0.6	0.8	0.8	1	1
V [N]	0	-492.776651044	-392.3450698732	-392.3450698732	-392.3450698732	-441.3450698732	-447.9570196832	-496.9570196832	-496.9570196832	-340.4185966295	-340.4185966295	-344.7286083575	-344.7286083575	-205.5833434209	-205.5833434209	-207.3465300369	-207.3465300369	-85.5944232174	-85.5944232174	-86.9657905854	-86.9657905854	0
Bending Moment Diagram Data
	[start]	Fuselage+Rib1+Lift1	M0	Fuel	Stringer1	Rib2	Stringer2	Rib3	Stringer3	Rib4	Stringer4	Rib5
X [m]	0	0	0	0.025	0.1	0.175	0.2	0.3	0.4	0.5	0.6	0.8	1
BM [Nm]	0	0	233.2499595607	223.4413328139	192.1779525734	156.7436760971	144.319750605	110.2778909421	75.8050301063	55.2466957642	34.5120427606	17.3931581171	0
																	Stringers Dimension Properties
																Section	Area [m2] Mateo: per springer	Weighted Area	Max. Shear [N] Mateo: along whole stringer	Max. BM [Nm]	Inertia [m4]
																1	0.00025434	0.3970588235	-496.9570196832	233.2499595607	0.0000000235
																2	0.00020724	0.3235294118	-344.7286083575	144.319750605	0.0000000128
																3	0.00011304	0.1764705882	-207.3465300369	75.8050301063	0.0000000022
																4	0.00006594	0.1029411765	-86.9657905854	34.5120427606	0.0000000005
																5		0
																6		0
																7		0
																8		0
	Max. Shear Force [N]										Max. Bending Moment [Nm]
Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8		Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8
1	-197.3211695801	-197.3211695801	-197.3211695801	-197.3211695801	-197.3211695801					1	92.6139545315	92.6139545315	92.6139545315	92.6139545315	92.6139545315
2	-111.5298438804	-111.5298438804	-111.5298438804	-111.5298438804						2	46.6916840193	46.6916840193	46.6916840193	46.6916840193
3	-36.5905641242	-36.5905641242	-36.5905641242							3	13.3773582541	13.3773582541	13.3773582541
4	-8.9523607956	-8.9523607956								4	3.5527102842	3.5527102842
5										5
6										6
7										7
8										8
	Shear Stress [Pa]										Normal Stress [Pa]
Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8		Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8
1	-1551633.00762842	-1551633.00762842	-1551633.00762842	-1551633.00762842	-1551633.00762842	0	0	0		1	59208853	59208852.7113705	59208852.7113705	59208852.7113705	59208852.7113705	0	0	0
2	-1076335.1078979	-1076335.1078979	-1076335.1078979	-1076335.1078979	0	0	0	0		2	45700298.308024	45700298.308024	45700298.308024	45700298.308024	0	0	0	0
3	-647391.438856385	-647391.438856385	-647391.438856385	0	0	0	0	0		3	46408553.1203937	46408553.1203937	46408553.1203937	0	0	0	0	0
4	-271530.506386239	-271530.506386239	0	0	0	0	0	0		4	37157188.7104752	37157188.7104752	0	0	0	0	0	0
5										5
6										6
7										7
8										8
		Principal Stresses [Pa]
Section	Stringer #	Sigma_1	Sigma_2	Signma_3	Sigma_VM	S.F.
1	5	59249487.0714192	0	-40634.3600487188	59269814.698275	4.6566705397
2	4	45725634.1461404	0	-25335.8381163403	45738307.3280578	6.0343291242
3	3	46417582.3643516	0	-9029.2439579219	46422097.6449117	5.9454443897
4	2	37159172.8454882	0	-1984.1350130402	37160164.9527227	7.4273082574
5	0
6	0
7	0
8	0

Shear Force Diagram

0 0 0 2.5000000000000001E-2 2.5000000000000001E-2 0.1 0.1 0.17499999999999999 0.2 0.2 0.30000000000000004 0.30000000000000004 0.4 0.4 0.5 0.5 0.6 0.6 0.8 0.8 1 1 0 -492.776651044 -392.34506987323073 -392.34506987323073 -392.34506987323073 -441.34506987323073 -447.95701968323073 -496.95701968323073 -496.95701968323073 -340.41859662953846 -340.41859662953846 -344.72860835753846 -344.72860835753846 -205.58334342092309 -205.58334342092309 -207.3465300369231 -207.3465300369231 -85.594423217384644 -85.594423217384644 -86.965790585384639 -86.965790585384639 0

Lenght [m]

Shear Force [N]

Bending Moment Diagram

0 0 0 2.5000000000000001E-2 0.1 0.17499999999999999 0.2 0.3 0.4 0.5 0.6 0.8 1 0 0 233.24995956069233 223.44133281386155 192.17795257336923 156.74367609712692 144.31975060504615 110.27789094209231 75.80503010633845 55.246695764246141 34.51204276055384 17.393158117076904 0

Lenght [m]

Bending Moment [Nm]

Wing2

Total Cost	$102.69		Min S.F.	3.18						Density Aluminum [kg/m3]:				Yeald Stress:
										2650				276000000
	Individual Stringers			Diameters [m]
Section	X1 (m)	X2 (m)	#	String1	String2	String3	String4	String5	String6	String7	String8				Variables
1	0.00	0.20	4	0.03	0.03	0.03	0.03
2	0.20	0.40	3	0.025	0.025	0.025									Constants
3	0.40	0.60	2	0.01	0.01
4	0.60	1.00	1	0.01											Change Manually if variables are changed
5
6															Delete this cell
7
8
													Total # Ribs:		5
	Stringer Weight [N]										Rib Dimensions
Section	String1	String2	String3	String4	String5	String6	String7	String8		Rib	Length [m]	Volume [m3]	Mass [kg]	Weight [N]	X [m]
1	1.322389962	1.322389962	1.322389962	1.322389962						1	0.2	0.0006	1.59	15.5979	0
2	1.077502932	1.077502932	1.077502932							2	0.18	0.00054	1.431	14.03811	0.2
3	0.342841842	0.342841842								3	0.16	0.00048	1.272	12.47832	0.4
4	0.685683684									4	0.14	0.00042	1.113	10.91853	0.6
5										5	0.1	0.0003	0.795	7.79895	1
6										6		0	0	0
7										7		0	0	0
8										8		0	0	0
Load Fuselage [N]		Load Fuel [N]		Total Ribs [N]		Total Stringers [N]		Total Load [N]		Lift [N]
147		98		60.83181		9.893436012		242.225246012		726.675738036
Shear Foce								Bending Moment [CW+]
Other	Load [N]	Ribs	Load [N]	Lift [N]	Stringer	Load [N]		Other	BM [N]	Ribs	BM [Nm]	Lift [Nm]	Stringer	BM [Nm]
ReactionA	-484.450492024	1	-15.5979	186.3271123169	1	-5.289559848		M0	230.2453840772	1	0	0	1	-0.5289559848
Fuselage Mateo: Fuselage is divided between both wings.	-73.5	2	-14.03811	167.6944010852	2	-3.232508796		Fuel	-9.8	2	-2.807622	33.538880217	2	-0.9697526388
Fuel	-98	3	-12.47832	149.0616898535	3	-0.685683684		Fuselage	0	3	-4.991328	59.6246759414	3	-0.342841842
		4	-10.91853	130.4289786218	4	-0.685683684				4	-6.551118	78.2573871731	4	-0.5485469472
		5	-7.79895	93.1635561585	5	0				5	-7.79895	93.1635561585	5	0
		6	0		6	0				6	0	0	6	0
		7	0		7	0				7	0	0	7	0
		8	0		8	0				8	0	0	8	0
Shear Force Diagram Data
	[start]	Ra	Fuselage+Rib1+Lift1	[stop]	Fuel (start)	[stop]	Stringer1	Fuel (end)	[stop]	Rib2	[stop]	Stringer2	[stop]	Rib3	[stop]	Stringer3	[stop]	Rib4	[stop]	Stringer4	[stop]	Rib5
X [m]	0	0	0	0.025	0.025	0.1	0.1	0.175	0.2	0.2	0.3	0.3	0.4	0.4	0.5	0.5	0.6	0.6	0.8	0.8	1	1
V [N]	0	-484.450492024	-387.2212797071	-387.2212797071	-387.2212797071	-436.2212797071	-441.5108395551	-490.5108395551	-490.5108395551	-336.8545484698	-336.8545484698	-340.0870572658	-340.0870572658	-203.5036874123	-203.5036874123	-204.1893710963	-204.1893710963	-84.6789224745	-84.6789224745	-85.3646061585	-85.3646061585	0
Bending Moment Diagram Data
	[start]	Fuselage+Rib1+Lift1	M0	Fuel	Stringer1	Rib2	Stringer2	Rib3	Stringer3	Rib4	Stringer4	Rib5
X [m]	0	0	0	0.025	0.1	0.175	0.2	0.3	0.4	0.5	0.6	0.8	1
BM [Nm]	0	0	230.2453840772	220.5648520846	189.6857561065	154.7349431399	142.472172151	108.786717304	74.7780115774	54.4276428362	34.0087057266	17.0729212317	0
																	Stringers Dimension Properties
																Section	Area [m2] Mateo: per springer	Weighted Area	Max. Shear [N] Mateo: along whole stringer	Max. BM [Nm]	Inertia [m4]
																1	0.00025434	0.4285714286	-490.5108395551	230.2453840772	0.0000000235
																2	0.00020724	0.3492063492	-340.0870572658	142.472172151	0.0000000128
																3	0.00006594	0.1111111111	-204.1893710963	74.7780115774	0.0000000005
																4	0.00006594	0.1111111111	-85.3646061585	34.0087057266	0.0000000005
																5		0
																6		0
																7		0
																8		0
	Max. Shear Force [N]										Max. Bending Moment [Nm]
Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8		Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8
1	-210.2189312379	-210.2189312379	-210.2189312379	-210.2189312379						1	98.676593176	98.676593176	98.676593176	98.676593176
2	-118.7605596801	-118.7605596801	-118.7605596801							2	49.7521871004	49.7521871004	49.7521871004
3	-22.6877078996	-22.6877078996								3	8.308667953	8.308667953
4	-9.4849562398									4	3.7787450807
5										5
6										6
7										7
8										8
	Shear Stress [Pa]										Normal Stress [Pa]
Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8		Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8
1	-1653054.42508367	-1653054.42508367	-1653054.42508367	-1653054.42508367	0	0	0	0		1	63084747	63084746.7962391	63084746.7962391	63084746.7962391	0	0	0	0
2	-1146116.1906981	-1146116.1906981	-1146116.1906981	0	0	0	0	0		2	48695818.960481	48695818.960481	48695818.960481	0	0	0	0	0
3	-688131.874418857	-688131.874418857	0	0	0	0	0	0		3	86898935.8460625	86898935.8460625	0	0	0	0	0	0
4	-287684.447674524	0	0	0	0	0	0	0		4	39521247.9551068	0	0	0	0	0	0	0
5										5
6										6
7										7
8										8
		Principal Stresses [Pa]
Section	Stringer #	Sigma_1	Sigma_2	Signma_3	Sigma_VM	S.F.
1	4	63128033.2537991	0	-43286.4575600289	63149687.6092231	4.3705679386
2	3	48722779.2928276	0	-26960.3323465101	48736265.0518039	5.6631340072
3	2	86904384.6560215	0	-5448.8099589646	86907109.1891098	3.175804633
4	1	39523341.9668304	0	-2094.0117235854	39524389.0142952	6.9830301463
5	0
6	0
7	0
8	0

Shear Force Diagram

Lenght [m]

Shear Force [N]

Bending Moment Diagram

Lenght [m]

Bending Moment [Nm]

Shear Force Diagram

Lenght [m]

Shear Force [N]

Bending Moment Diagram

Lenght [m]

Bending Moment [Nm]

Wing3

Total Cost	$83.19		Min S.F.	1.23						Density Aluminum [kg/m3]:				Yeald Stress:
										2650				276000000
	Individual Stringers			Diameters [m]
Section	X1 (m)	X2 (m)	#	String1	String2	String3	String4	String5	String6	String7	String8				Variables
1	0.00	0.20	2	0.0163	0.0163
2	0.20	0.40	2	0.012	0.012										Constants
3	0.40	0.60	2	0.011	0.011
4	0.60	1.00	2	0.01	0.01										Change Manually if variables are changed
5
6															Delete this cell
7
8
													Total # Ribs:		5
	Stringer Weight [N]										Rib Dimensions
Section	String1	String2	String3	String4	String5	String6	String7	String8		Rib	Length [m]	Volume [m3]	Mass [kg]	Weight [N]	X [m]
1	0.6513994998	0.6513994998								1	0.2	0.0006	1.59	15.5979	0
2	0.440796654	0.440796654								2	0.18	0.00054	1.431	14.03811	0.2
3	0.391819248	0.391819248								3	0.16	0.00048	1.272	12.47832	0.4
4	0.685683684	0.685683684								4	0.14	0.00042	1.113	10.91853	0.6
5										5	0.1	0.0003	0.795	7.79895	1
6										6		0	0	0
7										7		0	0	0
8										8		0	0	0
Load Fuselage [N]		Load Fuel [N]		Total Ribs [N]		Total Stringers [N]		Total Load [N]		Lift [N]
147		98		60.83181		4.3393981716		236.6712081716		710.0136245148
Shear Foce								Bending Moment [CW+]
Other	Load [N]	Ribs	Load [N]	Lift [N]	Stringer	Load [N]		Other	BM [N]	Ribs	BM [Nm]	Lift [Nm]	Stringer	BM [Nm]
ReactionA	-473.3424163432	1	-15.5979	182.0547755166	1	-1.3027989996		M0	224.6850921988	1	0	0	1	-0.1302799
Fuselage Mateo: Fuselage is divided between both wings.	-73.5	2	-14.03811	163.849297965	2	-0.881593308		Fuel	-9.8	2	-2.807622	32.769859593	2	-0.2644779924
Fuel	-98	3	-12.47832	145.6438204133	3	-0.783638496		Fuselage	0	3	-4.991328	58.2575281653	3	-0.391819248
		4	-10.91853	127.4383428616	4	-1.371367368				4	-6.551118	76.463005717	4	-1.0970938944
		5	-7.79895	91.0273877583	5	0				5	-7.79895	91.0273877583	5	0
		6	0		6	0				6	0	0	6	0
		7	0		7	0				7	0	0	7	0
		8	0		8	0				8	0	0	8	0
Shear Force Diagram Data
	[start]	Ra	Fuselage+Rib1+Lift1	[stop]	Fuel (start)	[stop]	Stringer1	Fuel (end)	[stop]	Rib2	[stop]	Stringer2	[stop]	Rib3	[stop]	Stringer3	[stop]	Rib4	[stop]	Stringer4	[stop]	Rib5
X [m]	0	0	0	0.025	0.025	0.1	0.1	0.175	0.2	0.2	0.3	0.3	0.4	0.4	0.5	0.5	0.6	0.6	0.8	0.8	1	1
V [N]	0	-473.3424163432	-380.3855408266	-380.3855408266	-380.3855408266	-429.3855408266	-430.6883398262	-479.6883398262	-479.6883398262	-329.8771518612	-329.8771518612	-330.7587451692	-330.7587451692	-197.5932447559	-197.5932447559	-198.3768832519	-198.3768832519	-81.8570703903	-81.8570703903	-83.2284377583	-83.2284377583	0
Bending Moment Diagram Data
	[start]	Fuselage+Rib1+Lift1	M0	Fuel	Stringer1	Rib2	Stringer2	Rib3	Stringer3	Rib4	Stringer4	Rib5
X [m]	0	0	0	0.025	0.1	0.175	0.2	0.3	0.4	0.5	0.6	0.8	1
BM [Nm]	0	0	224.6850921988	215.1754536782	184.8090381162	150.6699126292	138.6777041336	105.6899889474	72.6141144305	52.8547899549	33.0171016297	16.6456875517	0
																	Stringers Dimension Properties
																Section	Area [m2] Mateo: per springer	Weighted Area	Max. Shear [N] Mateo: along whole stringer	Max. BM [Nm]	Inertia [m4]
																1	0.000125286	0.3565683646	-479.6883398262	224.6850921988	0.0000000029
																2	0.00008478	0.2412868633	-330.7587451692	138.6777041336	0.000000001
																3	0.00007536	0.2144772118	-198.3768832519	72.6141144305	0.0000000007
																4	0.00006594	0.1876675603	-83.2284377583	33.0171016297	0.0000000005
																5		0
																6		0
																7		0
																8		0
	Max. Shear Force [N]										Max. Bending Moment [Nm]
Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8		Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8
1	-171.0416868549	-171.0416868549								1	80.1155958779	80.1155958779
2	-79.8077401213	-79.8077401213								2	33.461108236	33.461108236
3	-42.5473208047	-42.5473208047								3	15.5740728001	15.5740728001
4	-15.6192778635	-15.6192778635								4	6.1962389117	6.1962389117
5										5
6										6
7										7
8										8
	Shear Stress [Pa]										Normal Stress [Pa]
Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8		Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8
1	-2730419.78920092	-2730419.78920092	0	0	0	0	0	0		1	224288028	224288027.604365	0	0	0	0	0	0
2	-1882702.05523147	-1882702.05523147	0	0	0	0	0	0		2	210496867.097453	210496867.097453	0	0	0	0	0	0
3	-1129175.18059197	-1129175.18059197	0	0	0	0	0	0		3	124563593.055583	124563593.055583	0	0	0	0	0	0
4	-473742.125067922	-473742.125067922	0	0	0	0	0	0		4	64805402.1079171	64805402.1079171	0	0	0	0	0	0
5										5
6										6
7										7
8										8
		Principal Stresses [Pa]
Section	Stringer #	Sigma_1	Sigma_2	Signma_3	Sigma_VM	S.F.
1	2	224321262.04749	0	-33234.4431250542	224337881.115366	1.2302870948
2	2	210513704.799455	0	-16837.7020020932	210522124.155465	1.3110261029
3	2	124573828.243877	0	-10235.1882930696	124578946.153362	2.2154626325
4	2	64808865.0847918	0	-3462.9768746942	64810596.6426172	4.2585628631
5	0
6	0
7	0
8	0

Shear Force Diagram

0 0 0 2.5000000000000001E-2 2.5000000000000001E-2 0.1 0.1 0.17499999999999999 0.2 0.2 0.30000000000000004 0.30000000000000004 0.4 0.4 0.5 0.5 0.6 0.6 0.8 0.8 1 1 0 -473.3424163432 -380.38554082658459 -380.38554082658459 -380.38554082658459 -429.38554082658459 -430.68833982618457 -479.68833982618457 -479.68833982618457 -329.87715186123074 -329.87715186123074 -330.75874516923074 -330.75874516923074 -197.59324475593843 -197.59324 475593843 -198.37688325193844 -198.37688325193844 -81.857070390307669 -81.857070390307669 -83.228437758307663 -83.228437758307663 0

Lenght [m]

Shear Force [N]

Bending Moment Diagram

0 0 0 2.5000000000000001E-2 0.1 0.17499999999999999 0.2 0.3 0.4 0.5 0.6 0.8 1 0 0 224.68509219883387 215.17545367816925 184.8090381161754 150.66991262921155 138.67770413355692 105.68998894743385 72.614114430510767 52.854789954916924 33.017101629723086 16.645687551661545 0

Lenght [m]

Bending Moment [Nm]

Wing4

Total Cost	$82.61		Min S.F.	1.20						Density Aluminum [kg/m3]:				Yeald Stress:
										2650				276000000
	Individual Stringers			Diameters [m]
Section	X1 (m)	X2 (m)	#	String1	String2	String3	String4	String5	String6	String7	String8				Variables
1	0.00	0.20	2	0.0164	0.0164
2	0.20	0.40	2	0.0118	0.0118										Constants
3	0.40	0.60	2	0.01	0.01
4	0.60	1.00	2	0.01	0.01										Change Manually if variables are changed
5
6															Delete this cell
7
8
													Total # Ribs:		5
	Stringer Weight [N]										Rib Dimensions
Section	String1	String2	String3	String4	String5	String6	String7	String8		Rib	Length [m]	Volume [m3]	Mass [kg]	Weight [N]	X [m]
1	0.6562972404	0.6562972404								1	0.2	0.0006	1.59	15.5979	0
2	0.4310011728	0.4310011728								2	0.18	0.00054	1.431	14.03811	0.2
3	0.342841842	0.342841842								3	0.16	0.00048	1.272	12.47832	0.4
4	0.685683684	0.685683684								4	0.14	0.00042	1.113	10.91853	0.6
5										5	0.1	0.0003	0.795	7.79895	1
6										6		0	0	0
7										7		0	0	0
8										8		0	0	0
Load Fuselage [N]		Load Fuel [N]		Total Ribs [N]		Total Stringers [N]		Total Load [N]		Lift [N]
147		98		60.83181		4.2316478784		236.5634578784		709.6903736352
Shear Foce								Bending Moment [CW+]
Other	Load [N]	Ribs	Load [N]	Lift [N]	Stringer	Load [N]		Other	BM [N]	Ribs	BM [Nm]	Lift [Nm]	Stringer	BM [Nm]
ReactionA	-473.1269157568	1	-15.5979	181.9718906757	1	-1.3125944808		M0	224.6212708713	1	0	0	1	-0.1312594481
Fuselage Mateo: Fuselage is divided between both wings.	-73.5	2	-14.03811	163.7747016081	2	-0.8620023456		Fuel	-9.8	2	-2.807622	32.7549403216	2	-0.2586007037
Fuel	-98	3	-12.47832	145.5775125406	3	-0.685683684		Fuselage	0	3	-4.991328	58.2310050162	3	-0.342841842
		4	-10.91853	127.380323473	4	-1.371367368				4	-6.551118	76.4281940838	4	-1.0970938944
		5	-7.79895	90.9859453378	5	0				5	-7.79895	90.9859453378	5	0
		6	0		6	0				6	0	0	6	0
		7	0		7	0				7	0	0	7	0
		8	0		8	0				8	0	0	8	0
Shear Force Diagram Data
	[start]	Ra	Fuselage+Rib1+Lift1	[stop]	Fuel (start)	[stop]	Stringer1	Fuel (end)	[stop]	Rib2	[stop]	Stringer2	[stop]	Rib3	[stop]	Stringer3	[stop]	Rib4	[stop]	Stringer4	[stop]	Rib5
X [m]	0	0	0	0.025	0.025	0.1	0.1	0.175	0.2	0.2	0.3	0.3	0.4	0.4	0.5	0.5	0.6	0.6	0.8	0.8	1	1
V [N]	0	-473.1269157568	-380.2529250811	-380.2529250811	-380.2529250811	-429.2529250811	-430.5655195619	-479.5655195619	-479.5655195619	-329.8289279538	-329.8289279538	-330.6909302994	-330.6909302994	-197.5917377588	-197.5917377588	-198.2774214428	-198.2774214428	-81.8156279698	-81.8156279698	-83.1869953378	-83.1869953378	0
Bending Moment Diagram Data
	[start]	Fuselage+Rib1+Lift1	M0	Fuel	Stringer1	Rib2	Stringer2	Rib3	Stringer3	Rib4	Stringer4	Rib5
X [m]	0	0	0	0.025	0.1	0.175	0.2	0.3	0.4	0.5	0.6	0.8	1
BM [Nm]	0	0	224.6212708713	215.1149477443	184.7584783632	150.6285643961	138.639426407	105.6565336116	72.5874405817	52.8282668058	33.0005246615	16.6373990676	0
																	Stringers Dimension Properties
																Section	Area [m2] Mateo: per springer	Weighted Area	Max. Shear [N] Mateo: along whole stringer	Max. BM [Nm]	Inertia [m4]
																1	0.000126228	0.3701657459	-479.5655195619	224.6212708713	0.000000003
																2	0.000082896	0.2430939227	-330.6909302994	138.639426407	0.0000000009
																3	0.00006594	0.1933701657	-198.2774214428	72.5874405817	0.0000000005
																4	0.00006594	0.1933701657	-83.1869953378	33.0005246615	0.0000000005
																5		0
																6		0
																7		0
																8		0
	Max. Shear Force [N]										Max. Bending Moment [Nm]
Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8		Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8
1	-177.5187282356	-177.5187282356								1	83.1471002673	83.1471002673
2	-80.3889554319	-80.3889554319								2	33.7024019995	33.7024019995
3	-38.3409378481	-38.3409378481								3	14.0362454164	14.0362454164
4	-16.0858830764	-16.0858830764								4	6.3813169235	6.3813169235
5										5
6										6
7										7
8										8
	Shear Stress [Pa]										Normal Stress [Pa]
Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8		Section	Stringer1	Stringer2	Stringer3	Stringer4	Stringer5	Stringer6	Stringer7	Stringer8
1	-2812668.00132496	-2812668.00132496	0	0	0	0	0	0		1	229163621	229163621.383441	0	0	0	0	0	0
2	-1939513.49719877	-1939513.49719877	0	0	0	0	0	0		2	222000790.045686	222000790.045686	0	0	0	0	0	0
3	-1162903.78671705	-1162903.78671705	0	0	0	0	0	0		3	146802688.090027	146802688.090027	0	0	0	0	0	0
4	-487894.54280798	-487894.54280798	0	0	0	0	0	0		4	66741101.3513007	66741101.3513007	0	0	0	0	0	0
5										5
6										6
7										7
8										8
		Principal Stresses [Pa]
Section	Stringer #	Sigma_1	Sigma_2	Signma_3	Sigma_VM	S.F.
1	2	229198137.812593	0	-34516.4291524291	229215397.976292	1.204107588
2	2	222017733.343634	0	-16943.2979481667	222026205.477476	1.2430965048
3	2	146811899.504236	0	-9211.4142091125	146816505.428065	1.8798976259
4	2	66744667.794775	0	-3566.4434743114	66746451.087974	4.1350513099
5	0
6	0
7	0
8	0

Shear Force Diagram

0 0 0 2.5000000000000001E-2 2.5000000000000001E-2 0.1 0.1 0.17499999999999999 0.2 0.2 0.30000000000000004 0.30000000000000004 0.4 0.4 0.5 0.5 0.6 0.6 0.8 0.8 1 1 0 -473.12691575679997 -380.25292508110766 -380.25292508110766 -380.25292508110766 -429.25292508110766 -430.56551956190765 -479.56551956190765 -479.56551956190765 -329.82892795378461 -329.82892795378461 -330.6909302993846 -330.6909302993846 -197.59173775883076 -197.59173775883076 -198.27742144283076 -198.27742144283076 -81.815627969846147 -81.815627969846147 -83.186995337846142 -83.186995337846142 0

Lenght [m]

Shear Force [N}

Bending Moment Diagram

0 0 0 2.5000000000000001E-2 0.1 0.17499999999999999 0.2 0.3 0.4 0.5 0.6 0.8 1 0 0 224.62127087132308 215.11494774429539 184.7584783632123 150.62856439606924 138.63942640702155 105.65653361164308 72.587440581704612 52.828266805821542 33.000524661538471 16.637399067569234 0

Lenght [m]

Bending Moment [Nm]