avance_lab2_aerodinamica

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Coeficiente de presión y sustentación a -5°
	C_p
	0.051465446
Coeficiente de presión y sustentación a 0°
	C_p
	0.084679315
Coeficiente de presión y sustentación a 5°
	C_p
	0.273301697
Arriba	0	9.4899999999999998E-2	0.17699999999999999	0.26229999999999998	0.35170000000000001	0.44979999999999998	0.54559999999999997	0.64039999999999997	0.72419999999999995	0.80289999999999995	0.84370000000000001	1	0.33952832149264367	5.0584818441496052E-2	-0.13942606982229702	-0.31521987688804487	-0.29049355787397163	-0.22718299023190167	-0.16202451294225803	-0.12517854854148949	-9.3208212339539992E-2	-7.5030850031970325E-2	-0.70029053321419887	0	abajo	0	0.10249999999999999	0.18440000000000001	0.28160000000000002	0.38250000000000001	0.46710000000000002	0.55620000000000003	0.64770000000000005	0.73299999999999998	0.79469999999999996	0.8387	0.93810000000000004	1	0.33952832149264367	-0.49598012151459248	-0.46146301188473132	-0.46740282627648899	-0.35729942198315162	-0.27056687033087629	-0.16008286434220423	-5.7433149138500859E-2	-3.1659009332135751E-2	-1.8482216137973705E-2	1.6668341321823727E-2	0.86953751877067409	0	
arriba	0	9.4899999999999998E-2	0.17699999999999999	0.26229999999999998	0.35170000000000001	0.44979999999999998	0.54559999999999997	0.64039999999999997	0.72419999999999995	0.80289999999999995	0.84370000000000001	1	0.81935190796186497	-0.27539110401622746	-0.36878455940758909	-0.41087732252082265	-0.52914327947155881	-0.40641224969160938	-0.32898988933733558	-0.27385474864215598	-0.19860962279291905	-0.17070987550389555	-0.14232705337958843	0	abajo	0	0.10249999999999999	0.18440000000000001	0.28160000000000002	0.38250000000000001	0.46710000000000002	0.55620000000000003	0.64770000000000005	0.73299999999999998	0.79469999999999996	0.8387	0.93810000000000004	1	0.81935190796186497	-0.32756098156384911	-0.33033733186548914	-0.36600292603450901	-0.37403785100719555	-0.30105554529511103	-0.23791894487768023	-0.18856295082494198	-7.6476321087455251E-2	-8.1193624541800197E-3	2.1673543109792321E-2	5.9261561617243261E-2	0	x% C
Cp
arriba	0	9.4899999999999998E-2	0.17699999999999999	0.26229999999999998	0.35170000000000001	0.44979999999999998	0.54559999999999997	0.64039999999999997	0.72419999999999995	0.80289999999999995	0.84370000000000001	1	0.99970243043118701	-0.67074668127391412	-0.61562855867341515	-0.61044558960017825	-0.63913763018104774	-0.52864882178151584	-0.44902327352233018	-0.35707935070328839	-0.23272327786079408	-0.14658655898538253	-0.10278062620924339	0	abajo	0	0.10249999999999999	0.18440000000000001	0.28160000000000002	0.38250000000000001	0.46710000000000002	0.55620000000000003	0.64770000000000005	0.73299999999999998	0.79469999999999996	0.8387	0.93810000000000004	1	0.99970243043118701	-4.5656172322748087E-2	-0.16243430351353416	-0.23519765665387246	-0.32456388710431178	-0.24911574529494027	-0.17872168487849993	-0.12643263240395092	-5.95341674379282E-2	2.6317377945445329E-3	2.6109886545325728E-2	6.3418965581313408E-2	0