ANNEXES
ANNEXE A
ANNEXE B
ANNEXE A
1. L'histoire de convergence des
résidus
Les figures ci-dessous montrent l'histoire de convergence
exprimée en termes de résidus pour chaque angle d'incidence
á=-3.0170, -2.8730, 00,
3.0170.
On peut dire que les solutions a été
convergées ; d'une part, parce que le résidu des variables
conservatives a une allure presque constante en dépassant 600
itérations.
Pour á=-3.0170
Pour á=-2.8730
Figure (2) : Historique des résidus Pour
á=-2.8730
Pour á=00
Pour á=3.0170
Figure (4) : Historique des résidus Pour
á=3.0170 2. L'histoire de convergence des coefficients Cd, Cl
et Cm
Les figures ci-dessous montrent l'histoire de
convergence des coefficients de portance, de trainée et de moment en
fonction d'itérations pour chaque angle d'incidence.
2.1. Historique de convergence des Coefficient de
Portance Cl
2.2. Historique des Coefficient de
trainée
Figure (6) : Historique des Coefficient de trainée
(ORIGIN) 2.2. Historique des Coefficient de moment
ANNEXE B
Données Expérimentales
Dans cette annexe, se regroupent tous les données
expérimentales du coefficient de pression qui ont été
utilisées pour la validation.
Coefficient de pression CP expérimentale pour:
ETA=0.019
|
X/C
|
Cp
|
|
0.0000000000E+00
|
0.7454000115
|
|
0.9999999776E-02
|
0.1265999973
|
|
0.2500000037E-01
|
-0.1181999967
|
|
0.5000000075E-01
|
-0.5508000255
|
|
0.7500000298E-01
|
-0.6563000083
|
|
0.1000000015
|
-0.6841999888
|
|
0.1500000060
|
-0.8065999746
|
|
0.2000000030
|
-0.8626000285
|
|
0.2500000000
|
-0.9520999789
|
|
0.3000000119
|
-0.9183999896
|
|
0.3499999940
|
-0.9179000258
|
|
0.4000000060
|
-0.8177999854
|
|
0.4499999881
|
-0.7979999781
|
|
0.5000000000
|
-0.7206000090
|
|
0.5500000119
|
-0.5311999917
|
|
0.6000000238
|
-0.4031000137
|
|
0.6499999762
|
-0.3244999945
|
|
0.6999999881
|
-0.2547000051
|
|
0.7500000000
|
-0.2011999935
|
|
0.8000000119
|
-0.1508000046
|
|
0.8500000238
|
-0.1105000004
|
|
0.8999999762
|
-0.7360000163E-01
|
|
0.9499999881
|
-0.1869999990E-01
|
|
0.9900000095
|
0.3810000047E-01
|
|
1.000000000
|
0.6530000269E-01
|
|
0.9999999776E-02
|
0.4345000088
|
|
0.2500000037E-01
|
0.2973000109
|
|
0.5000000075E-01
|
0.1785999984
|
|
0.7500000298E-01
|
0.1322000027
|
|
0.1000000015
|
0.1005999967
|
|
0.1599999964
|
0.3159999847E-01
|
|
0.2199999988
|
-0.2999999933E-01
|
|
0.2800000012
|
-0.7440000027E-01
|
|
0.3400000036
|
-0.9929999709E-01
|
|
0.4000000060
|
-0.1032000035
|
|
0.4600000083
|
-0.9920000285E-01
|
|
0.5199999809
|
-0.8649999648E-01
|
|
0.5799999833
|
-0.5480000004E-01
|
|
0.6399999857
|
-0.1040000003E-01
|
|
0.6999999881
|
0.3720000014E-01
|
|
0.7599999905
|
0.8810000122E-01
|
|
0.8199999928
|
0.1278000027
|
|
0.8799999952
|
0.1773999929
|
|
0.9399999976
|
0.2043000013
|
|
0.9900000095
|
0.1500999928
|
Coefficient de pression CP expérimentale pour:
ETA=0.325
|
X/C
|
Cp
|
|
0.0000000000E+00
|
0.6146000028
|
|
0.9999999776E-02
|
0.6384000182
|
|
0.2500000037E-01
|
0.7091000080
|
|
0.5000000075E-01
|
-1.183599949
|
|
0.7500000298E-01
|
-1.254600048
|
|
0.1000000015
|
-1.334900022
|
|
0.1500000060
|
-1.404199958
|
|
0.2000000030
|
-1.448199987
|
|
0.2500000000
|
-1.437500000
|
|
0.3000000119
|
-1.411499977
|
|
0.3499999940
|
-1.362900019
|
|
0.4000000060
|
-1.333799958
|
|
0.4499999881
|
-1.064299941
|
|
0.5000000000
|
-0.7462999821
|
|
0.5500000119
|
-0.5303999782
|
|
0.6000000238
|
-0.3533000052
|
|
0.6499999762
|
-0.2824000120
|
|
0.6999999881
|
-0.2409999967
|
|
0.7500000000
|
-0.2198999971
|
|
0.8000000119
|
-0.1908999979
|
|
0.8500000238
|
-0.1469999999
|
|
0.8999999762
|
-0.8309999853E-01
|
|
0.9499999881
|
0.1030000020E-01
|
|
0.9900000095
|
0.9009999782E-01
|
|
0.9999999776E-02
|
0.4859000146
|
|
0.2500000037E-01
|
0.4178000093
|
|
0.5000000075E-01
|
0.2558000088
|
|
0.7500000298E-01
|
0.1969999969
|
|
0.1000000015
|
0.1228000000
|
|
0.1599999964
|
0.5499999970E-01
|
|
0.2800000012
|
-0.8420000225E-01
|
|
0.3400000036
|
-0.1185000017
|
|
0.4000000060
|
-0.1344999969
|
|
0.4600000083
|
-0.1316999942
|
|
0.5199999809
|
-0.8820000291E-01
|
|
0.5799999833
|
-0.4569999874E-01
|
|
0.6399999857
|
0.5100000184E-02
|
|
0.6999999881
|
0.5730000138E-01
|
|
0.7599999905
|
0.1111999974
|
|
0.8199999928
|
0.1636999995
|
|
0.8799999952
|
0.2257999927
|
|
0.9399999976
|
0.2617000043
|
|
0.9900000095
|
0.2287999988
|
Coefficient de pression CP expérimentale pour:
ETA=0.635
|
X/C
|
Cp
|
|
0.0000000000E+00
|
0.6557999849
|
|
0.9999999776E-02
|
-0.5781999826
|
|
0.2500000037E-01
|
-0.6524000168
|
|
0.5000000075E-01
|
-1.165300012
|
|
0.7500000298E-01
|
-1.241299987
|
|
0.1000000015
|
-1.284999967
|
|
0.1500000060
|
-1.271700025
|
|
0.2000000030
|
-1.259099960
|
|
0.2500000000
|
-1.224099994
|
|
0.3000000119
|
-1.209900022
|
|
0.3499999940
|
-1.184900045
|
|
0.4000000060
|
-1.145200014
|
|
0.4499999881
|
-0.9991000295
|
|
0.5000000000
|
-0.6259999871
|
|
0.5500000119
|
-0.4677999914
|
|
0.6000000238
|
-0.3826999962
|
|
0.6499999762
|
-0.3716999888
|
|
0.6999999881
|
-0.3467000127
|
|
0.7500000000
|
-0.3321000040
|
|
0.8000000119
|
-0.2806000113
|
|
0.8500000238
|
-0.2196000069
|
|
0.8999999762
|
-0.1206000000
|
|
0.9499999881
|
-0.1219999976E-01
|
|
0.9900000095
|
0.6069999933E-01
|
|
1.000000000
|
0.7680000365E-01
|
|
0.9999999776E-02
|
0.4309999943
|
|
0.2500000037E-01
|
0.3892999887
|
|
0.5000000075E-01
|
0.2185000032
|
|
0.7500000298E-01
|
0.1770000011
|
|
0.1000000015
|
0.1327999979
|
|
0.1599999964
|
0.5420000106E-01
|
|
0.2199999988
|
-0.2050000057E-01
|
|
0.3400000036
|
-0.1001000032
|
|
0.4000000060
|
-0.1106999964
|
|
0.4600000083
|
-0.8160000294E-01
|
|
0.5199999809
|
-0.2740000002E-01
|
|
0.5799999833
|
0.4690000042E-01
|
|
0.6399999857
|
0.1199000031
|
|
0.6999999881
|
0.1871999949
|
|
0.7599999905
|
0.2467000037
|
|
0.8199999928
|
0.2845999897
|
|
0.8799999952
|
0.3093000054
|
|
0.9399999976
|
0.2881999910
|
|
0.9900000095
|
0.1333999932
|
Coefficient de pression CP expérimentale pour:
ETA=0.936
|
X/C
|
Cp
|
|
0.0000000000E+00
|
0.5993999839
|
|
0.9999999776E-02
|
-0.9096999764
|
|
0.2500000037E-01
|
-0.5863000154
|
|
0.5000000075E-01
|
-1.156200051
|
|
0.7500000298E-01
|
-1.208600044
|
|
0.1000000015
|
-1.206599951
|
|
0.1500000060
|
-1.184000015
|
|
0.2000000030
|
-1.159899950
|
|
0.2500000000
|
-1.086300015
|
|
0.3000000119
|
-1.036399961
|
|
0.3499999940
|
-0.5430999994
|
|
0.4000000060
|
-0.3443000019
|
|
0.4499999881
|
-0.3231999874
|
|
0.5000000000
|
-0.3438999951
|
|
0.5500000119
|
-0.3429000080
|
|
0.6000000238
|
-0.3490999937
|
|
0.6499999762
|
-0.3188999891
|
|
0.6999999881
|
-0.2741999924
|
|
0.7500000000
|
-0.2263000011
|
|
0.8000000119
|
-0.1633999944
|
|
0.8500000238
|
-0.9099999815E-01
|
|
0.8999999762
|
-0.1840000041E-01
|
|
0.9499999881
|
0.5959999934E-01
|
|
0.9900000095
|
0.8760000020E-01
|
|
1.000000000
|
0.9950000048E-01
|
|
0.9999999776E-02
|
0.4347000122
|
|
0.2500000037E-01
|
0.4052999914
|
|
0.7500000298E-01
|
0.1415999979
|
|
0.1000000015
|
0.5640000105E-01
|
|
0.1599999964
|
-0.1549999975E-01
|
|
0.2199999988
|
-0.9420000017E-01
|
|
0.2800000012
|
-0.1631000042
|
|
0.3400000036
|
-0.1787000000
|
|
0.4000000060
|
-0.1993000060
|
|
0.4600000083
|
-0.1852999926
|
|
0.5199999809
|
-0.1202000007
|
|
0.5799999833
|
-0.4610000178E-01
|
|
0.6399999857
|
0.3500000015E-01
|
|
0.6999999881
|
0.9730000049E-01
|
|
0.7599999905
|
0.1512999982
|
|
0.8199999928
|
0.1934999973
|
|
0.8799999952
|
0.2138999999
|
|
0.9399999976
|
0.1895000041
|
|
0.9900000095
|
0.6949999928E-01
|
| 
