Airfoil Data from the University of Illinois Low-Speed Wind Tunnel		
Winter 98 Test Phase		
Airfoil: SG6050		
Test conditions: clean surface		
Data for 6 Reynolds numbers		

Re		
"100,000"		
alpha	Cl	Cd
-7.94	-0.259	0.0347
-6.94	-0.235	0.0302
-6	-0.234	0.0283
-4.96	-0.226	0.0263
-3.94	-0.174	0.0268
-2.91	-0.069	0.0283
-1.87	0.014	0.0295
-0.83	0.086	0.0315
0.19	0.213	0.0329
1.15	0.276	0.0368
2.19	0.344	0.0369
3.19	0.42	0.0344
4.24	0.584	0.0324
5.29	0.752	0.0315
6.34	0.868	0.0293
7.33	0.963	0.028
8.36	1.063	0.0285
9.38	1.153	0.0279
10.39	1.224	0.0297
11.39	1.288	0.031
12.42	1.347	0.0322
13.45	1.347	0.0358
14.43	1.33	0.0448

Re	 	
"150,000"	 	
alpha	Cl	Cd
-7.94	-0.431	0.0261
-6.98	-0.318	0.0232
-5.97	-0.227	0.0203
-4.9	-0.134	0.0201
-3.86	-0.037	0.0199
-2.88	0.049	0.0193
-1.82	0.145	0.0191
-0.78	0.236	0.0187
0.18	0.326	0.0185
1.2	0.463	0.0186
2.25	0.565	0.019
3.25	0.654	0.0188
4.33	0.756	0.0187
5.31	0.851	0.019
6.35	0.948	0.0198
7.33	1.036	0.0206
8.41	1.135	0.0215
9.4	1.212	0.0225
10.42	1.284	0.0239
11.42	1.349	0.0252
12.44	1.375	0.0276

Re		
"200,000"		
alpha	Cl	Cd
-8.99	-0.509	0.0254
-7.97	-0.396	0.022
-6.97	-0.312	0.0195
-5.98	-0.232	0.017
-4.9	-0.144	0.0164
-3.83	-0.04	0.0163
-2.83	0.054	0.016
-1.8	0.153	0.0157
-0.79	0.249	0.0149
0.19	0.347	0.0143
1.23	0.466	0.0139
2.29	0.602	0.0145
3.26	0.69	0.0146
4.32	0.789	0.0149
5.34	0.883	0.0153
6.35	0.977	0.016
7.36	1.067	0.0167
8.4	1.162	0.0177
9.43	1.244	0.0191
10.42	1.32	0.0207
11.42	1.374	0.0227
12.45	1.374	0.026

Re		
"300,000"		
alpha	Cl	Cd
-9.04	-0.509	0.0204
-7.98	-0.418	0.0177
-6.97	-0.336	0.016
-6	-0.251	0.0146
-4.93	-0.159	0.0129
-3.88	-0.056	0.0128
-2.86	0.048	0.0126
-1.85	0.153	0.0126
-0.83	0.254	0.0124
0.19	0.361	0.0119
1.24	0.459	0.0112
2.24	0.577	0.0108
3.27	0.703	0.0111
4.33	0.803	0.0116
5.34	0.898	0.0119
6.36	0.995	0.0125
7.36	1.083	0.0135
8.4	1.178	0.0145
9.46	1.267	0.0161
10.45	1.333	0.0178
11.4	1.365	0.0204
12.48	1.374	0.0258

Re		
"400,000"		
alpha	Cl	Cd
-9.03	-0.512	0.0179
-8.01	-0.428	0.0159
-7.01	-0.34	0.0145
-6	-0.248	0.0132
-4.9	-0.149	0.0115
-3.9	-0.049	0.011
-2.84	0.055	0.0112
-1.82	0.157	0.0111
-0.8	0.256	0.011
0.21	0.364	0.0109
1.25	0.468	0.0103
2.25	0.567	0.0094
3.27	0.695	0.0092
4.35	0.815	0.0102
5.37	0.911	0.0106
6.39	1.008	0.0112
7.41	1.099	0.0122
8.41	1.19	0.0134
9.47	1.273	0.0151
10.5	1.333	0.017
11.47	1.355	0.0205
12.49	1.363	0.0267

Re		
"500,000"		
alpha	Cl	Cd
-9.05	-0.553	0.0165
-8.06	-0.469	0.0146
-7.05	-0.38	0.0134
-6.05	-0.278	0.0123
-4.98	-0.179	0.011
-3.94	-0.075	0.0102
-2.91	0.025	0.0101
-1.78	0.139	0.0103
-0.77	0.234	0.0103
0.21	0.342	0.01
1.23	0.446	0.0097
2.29	0.555	0.0093
3.29	0.673	0.0086
4.28	0.79	0.0091
5.34	0.897	0.0101
6.34	0.988	0.0108
7.42	1.092	0.0116
8.47	1.178	0.0129
9.43	1.247	0.0143
10.43	1.299	0.0165
11.6	1.323	0.0214
12.5	1.329	0.0283