Name = naca-6416
Mach = 0; Re = 25000; T.U. = 1.0; T.L. = 1.0
Surface Finish = 0; Stall model = 1; Transition model = 1; Aspect Ratio = 0; ground effect = 0
?	Cl	Cd	Cm 0.25	T.U.	T.L.	S.U.	S.L.	L/D	A.C.	C.P.
[¡]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]
-15.0	-0.364	0.15958	-0.076	0.844	0.012	1.000	0.015	-2.282	0.338	0.042
-14.5	-0.331	0.16159	-0.079	0.836	0.013	1.000	0.016	-2.048	0.338	0.012
-14.0	-0.297	0.13919	-0.082	0.827	0.013	1.000	0.016	-2.132	0.336	-0.025
-13.5	-0.261	0.13101	-0.085	0.819	0.013	1.000	0.017	-1.991	0.332	-0.075
-13.0	-0.224	0.13538	-0.088	0.812	0.013	0.924	0.018	-1.654	0.332	-0.141
-12.5	-0.187	0.12446	-0.091	0.804	0.014	0.920	0.018	-1.499	0.331	-0.236
-12.0	-0.148	0.11934	-0.094	0.793	0.014	0.916	0.019	-1.238	0.329	-0.385
-11.5	-0.108	0.10935	-0.097	0.784	0.014	0.912	0.020	-0.989	0.329	-0.646
-11.0	-0.068	0.09943	-0.100	0.774	0.015	0.908	0.020	-0.687	0.328	-1.215
-10.5	-0.027	0.09588	-0.103	0.762	0.016	0.906	0.020	-0.287	0.236	-3.505
-10.0	-0.506	0.09110	-0.106	0.752	0.016	0.901	0.022	-5.554	0.234	0.040
-9.5	-0.434	0.08606	-0.110	0.741	0.017	0.898	0.023	-5.046	0.295	-0.002
-9.0	-0.363	0.07891	-0.113	0.728	0.018	0.896	0.024	-4.595	0.295	-0.061
-8.5	-0.291	0.07657	-0.116	0.715	0.019	0.893	0.026	-3.800	0.295	-0.149
-8.0	-0.220	0.07254	-0.119	0.703	0.020	0.891	0.027	-3.028	0.296	-0.293
-7.5	-0.149	0.06794	-0.123	0.689	0.021	0.888	0.029	-2.191	0.297	-0.574
-7.0	-0.079	0.06442	-0.126	0.675	0.023	0.884	0.031	-1.219	0.297	-1.354
-6.5	-0.009	0.06137	-0.129	0.658	0.025	0.881	0.034	-0.146	0.298	-14.228
-6.0	0.060	0.05851	-0.133	0.644	0.026	0.875	0.038	1.024	0.299	2.464
-5.5	0.128	0.05527	-0.136	0.626	0.029	0.873	0.041	2.314	0.300	1.313
-5.0	0.195	0.05338	-0.139	0.608	0.032	0.871	0.046	3.653	0.301	0.965
-4.5	0.261	0.05058	-0.143	0.589	0.035	0.867	0.052	5.163	0.302	0.797
-4.0	0.326	0.04867	-0.146	0.568	0.040	0.866	0.060	6.702	0.303	0.698
-3.5	0.390	0.04670	-0.150	0.545	0.046	0.865	0.072	8.354	0.304	0.634
-3.0	0.453	0.04457	-0.153	0.520	0.053	0.864	0.087	10.163	0.306	0.588
-2.5	0.515	0.04280	-0.157	0.488	0.062	0.868	0.111	12.024	0.307	0.554
-2.0	0.575	0.04087	-0.160	0.456	0.074	0.870	0.148	14.068	0.310	0.528
-1.5	0.634	0.03823	-0.164	0.431	0.088	0.866	0.222	16.575	0.359	0.508
-1.0	0.684	0.03213	-0.172	0.421	0.106	0.851	0.966	21.292	0.337	0.501
-0.5	0.747	0.03286	-0.174	0.412	0.131	0.836	0.966	22.717	0.070	0.482
0.0	0.667	0.03591	-0.175	0.407	0.159	0.816	0.967	18.565	0.140	0.513
0.5	0.709	0.03697	-0.178	0.403	0.194	0.791	0.967	19.176	0.316	0.501
1.0	0.748	0.03824	-0.180	0.399	0.249	0.763	0.969	19.560	0.326	0.491
1.5	0.786	0.03996	-0.184	0.396	0.925	0.734	0.962	19.679	0.337	0.483
2.0	0.822	0.04183	-0.187	0.393	0.934	0.701	0.962	19.651	0.349	0.477
2.5	0.857	0.04458	-0.191	0.389	0.942	0.668	0.962	19.228	0.364	0.472
3.0	0.889	0.04677	-0.194	0.386	0.950	0.629	0.963	18.998	0.356	0.469
3.5	0.930	0.04901	-0.198	0.380	0.959	0.607	0.963	18.972	0.351	0.463
4.0	0.966	0.05154	-0.202	0.374	0.962	0.577	0.962	18.745	0.355	0.459
4.5	1.007	0.05443	-0.206	0.368	0.961	0.555	0.962	18.494	0.352	0.455
5.0	1.046	0.05722	-0.210	0.363	0.961	0.531	0.962	18.276	0.348	0.451
5.5	1.089	0.05915	-0.214	0.355	0.962	0.516	0.963	18.411	0.341	0.447
6.0	1.133	0.06175	-0.218	0.347	0.962	0.503	0.963	18.353	0.341	0.443
6.5	1.176	0.06453	-0.222	0.340	0.962	0.490	0.963	18.232	0.343	0.439
7.0	1.220	0.06733	-0.226	0.332	0.962	0.478	0.963	18.118	0.341	0.436
7.5	1.265	0.07007	-0.230	0.323	0.962	0.470	0.963	18.049	0.341	0.432
8.0	1.308	0.07333	-0.234	0.315	0.961	0.460	0.962	17.833	0.339	0.429
8.5	1.353	0.07616	-0.238	0.304	0.961	0.456	0.962	17.769	0.340	0.426
9.0	1.395	0.07914	-0.242	0.294	0.961	0.447	0.962	17.630	0.343	0.424
9.5	1.439	0.08249	-0.246	0.283	0.961	0.444	0.962	17.446	0.339	0.421
10.0	1.483	0.08558	-0.250	0.270	0.961	0.441	0.962	17.325	0.341	0.419
10.5	1.525	0.08927	-0.254	0.257	0.961	0.437	0.962	17.082	0.342	0.417
11.0	1.567	0.09242	-0.258	0.242	0.961	0.436	0.963	16.954	0.341	0.415
11.5	1.609	0.09618	-0.262	0.225	0.963	0.436	0.964	16.729	0.337	0.413
12.0	1.653	0.09975	-0.265	0.203	0.963	0.439	0.964	16.567	0.325	0.411
12.5	1.701	0.10326	-0.269	0.173	0.963	0.452	0.964	16.475	0.261	0.408
13.0	1.814	0.10102	-0.267	0.030	0.963	0.546	0.965	17.959	0.277	0.397
13.5	1.833	0.10631	-0.272	0.021	0.963	0.523	0.965	17.241	0.595	0.399
14.0	1.845	0.11304	-0.278	0.018	0.964	0.494	0.965	16.320	1.506	0.401
14.5	1.842	0.12220	-0.284	0.015	0.964	0.447	0.965	15.075	-0.262	0.404
15.0	1.819	0.13359	-0.291	0.013	0.964	0.370	0.965	13.617	-0.050	0.410

Name = naca-6416
Mach = 0; Re = 50000; T.U. = 1.0; T.L. = 1.0
Surface Finish = 0; Stall model = 1; Transition model = 1; Aspect Ratio = 0; ground effect = 0
?	Cl	Cd	Cm 0.25	T.U.	T.L.	S.U.	S.L.	L/D	A.C.	C.P.
[¡]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]
-15.0	-0.364	0.12928	-0.076	0.844	0.012	1.000	0.016	-2.813	0.341	0.042
-14.5	-0.331	0.11968	-0.079	0.836	0.013	1.000	0.016	-2.765	0.337	0.012
-14.0	-0.296	0.12257	-0.082	0.827	0.013	1.000	0.018	-2.413	0.333	-0.026
-13.5	-0.260	0.11287	-0.085	0.819	0.013	1.000	0.019	-2.302	0.334	-0.075
-13.0	-0.223	0.10550	-0.088	0.812	0.013	1.000	0.019	-2.118	0.333	-0.142
-12.5	-0.186	0.10024	-0.091	0.804	0.014	1.000	0.019	-1.856	0.331	-0.238
-12.0	-0.147	0.09659	-0.094	0.793	0.014	1.000	0.020	-1.524	0.328	-0.387
-11.5	-0.107	0.09197	-0.097	0.784	0.014	1.000	0.021	-1.168	0.328	-0.652
-11.0	-0.068	0.08556	-0.100	0.774	0.015	1.000	0.021	-0.790	0.328	-1.231
-10.5	-0.027	0.08049	-0.103	0.762	0.016	1.000	0.022	-0.331	0.236	-3.618
-10.0	-0.506	0.07568	-0.106	0.752	0.016	1.000	0.024	-6.684	0.234	0.040
-9.5	-0.434	0.07092	-0.110	0.741	0.017	1.000	0.025	-6.122	0.295	-0.002
-9.0	-0.362	0.06694	-0.113	0.728	0.018	1.000	0.026	-5.414	0.295	-0.061
-8.5	-0.291	0.06233	-0.116	0.715	0.019	1.000	0.027	-4.668	0.295	-0.149
-8.0	-0.220	0.06159	-0.119	0.703	0.020	1.000	0.030	-3.565	0.296	-0.293
-7.5	-0.149	0.05695	-0.123	0.689	0.021	1.000	0.032	-2.612	0.297	-0.574
-7.0	-0.079	0.05349	-0.126	0.675	0.023	1.000	0.035	-1.468	0.297	-1.353
-6.5	-0.009	0.05098	-0.129	0.658	0.025	1.000	0.039	-0.175	0.298	-14.222
-6.0	0.060	0.04865	-0.133	0.644	0.026	1.000	0.044	1.231	0.299	2.463
-5.5	0.128	0.04600	-0.136	0.626	0.029	1.000	0.048	2.779	0.300	1.313
-5.0	0.195	0.04400	-0.139	0.608	0.032	1.000	0.054	4.430	0.300	0.965
-4.5	0.261	0.04132	-0.143	0.589	0.035	1.000	0.067	6.312	0.301	0.797
-4.0	0.326	0.03929	-0.146	0.568	0.040	1.000	0.080	8.290	0.302	0.698
-3.5	0.389	0.03711	-0.149	0.545	0.046	1.000	0.110	10.490	0.303	0.633
-3.0	0.451	0.03489	-0.153	0.520	0.053	1.000	0.165	12.934	0.419	0.588
-2.5	0.496	0.02421	-0.167	0.488	0.062	1.000	0.965	20.498	0.401	0.587
-2.0	0.559	0.02478	-0.169	0.456	0.074	1.000	0.967	22.558	0.275	0.552
-1.5	0.622	0.02469	-0.170	0.431	0.088	1.000	0.968	25.178	0.275	0.524
-1.0	0.684	0.02468	-0.172	0.421	0.106	0.921	0.968	27.716	0.275	0.501
-0.5	0.746	0.02581	-0.174	0.412	0.131	0.913	0.968	28.921	0.319	0.482
0.0	0.729	0.02661	-0.175	0.407	0.159	0.903	0.968	27.414	0.352	0.490
0.5	0.782	0.02720	-0.177	0.403	0.194	0.893	0.969	28.741	0.291	0.477
1.0	0.831	0.02750	-0.179	0.399	0.249	0.879	0.970	30.221	0.297	0.466
1.5	0.879	0.02777	-0.182	0.396	0.925	0.864	0.963	31.651	0.302	0.457
2.0	0.926	0.02885	-0.184	0.393	0.934	0.848	0.963	32.080	0.309	0.449
2.5	0.969	0.03020	-0.187	0.389	0.942	0.829	0.962	32.102	0.321	0.443
3.0	1.009	0.03137	-0.190	0.386	0.950	0.806	0.963	32.162	0.325	0.438
3.5	1.053	0.03271	-0.193	0.380	0.959	0.788	0.963	32.198	0.329	0.434
4.0	1.093	0.03428	-0.197	0.374	0.962	0.766	0.962	31.866	0.339	0.430
4.5	1.133	0.03617	-0.200	0.368	0.961	0.745	0.962	31.318	0.347	0.427
5.0	1.170	0.03827	-0.204	0.363	0.961	0.720	0.962	30.569	0.348	0.425
5.5	1.211	0.03985	-0.208	0.355	0.962	0.702	0.963	30.386	0.343	0.422
6.0	1.252	0.04197	-0.212	0.347	0.962	0.685	0.963	29.834	0.351	0.419
6.5	1.290	0.04405	-0.216	0.340	0.962	0.664	0.963	29.287	0.358	0.417
7.0	1.329	0.04655	-0.220	0.332	0.962	0.644	0.963	28.547	0.352	0.416
7.5	1.370	0.04873	-0.224	0.323	0.962	0.629	0.963	28.115	0.354	0.414
8.0	1.408	0.05155	-0.228	0.315	0.961	0.612	0.962	27.313	0.347	0.412
8.5	1.453	0.05390	-0.232	0.304	0.961	0.604	0.962	26.953	0.348	0.410
9.0	1.490	0.05657	-0.236	0.294	0.961	0.588	0.962	26.344	0.352	0.409
9.5	1.533	0.05913	-0.240	0.283	0.961	0.580	0.962	25.920	0.339	0.407
10.0	1.576	0.06163	-0.244	0.270	0.961	0.575	0.962	25.575	0.341	0.405
10.5	1.618	0.06423	-0.248	0.257	0.961	0.568	0.962	25.184	0.340	0.403
11.0	1.661	0.06717	-0.252	0.242	0.961	0.565	0.963	24.730	0.336	0.402
11.5	1.703	0.06972	-0.255	0.225	0.963	0.563	0.964	24.428	0.329	0.400
12.0	1.749	0.07277	-0.259	0.203	0.963	0.566	0.964	24.042	0.314	0.398
12.5	1.800	0.07570	-0.262	0.173	0.963	0.576	0.964	23.774	0.276	0.395
13.0	1.876	0.08130	-0.262	0.030	0.963	0.615	0.965	23.074	0.305	0.390
13.5	1.898	0.08625	-0.267	0.021	0.963	0.596	0.965	22.006	0.485	0.391
14.0	1.918	0.09131	-0.272	0.018	0.964	0.578	0.965	21.004	0.539	0.392
14.5	1.933	0.09669	-0.277	0.015	0.964	0.556	0.965	19.992	0.631	0.393
15.0	1.946	0.10186	-0.282	0.013	0.964	0.533	0.965	19.101	0.674	0.395

Name = naca-6416
Mach = 0; Re = 75000; T.U. = 1.0; T.L. = 1.0
Surface Finish = 0; Stall model = 1; Transition model = 1; Aspect Ratio = 0; ground effect = 0
?	Cl	Cd	Cm 0.25	T.U.	T.L.	S.U.	S.L.	L/D	A.C.	C.P.
[¡]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]
-15.0	-0.363	0.12480	-0.076	0.844	0.012	1.000	0.018	-2.907	0.344	0.042
-14.5	-0.330	0.10840	-0.079	0.836	0.013	1.000	0.017	-3.049	0.338	0.012
-14.0	-0.295	0.10785	-0.082	0.827	0.013	1.000	0.019	-2.738	0.333	-0.026
-13.5	-0.259	0.09836	-0.085	0.819	0.013	1.000	0.020	-2.637	0.333	-0.076
-13.0	-0.223	0.09784	-0.088	0.812	0.013	1.000	0.020	-2.275	0.333	-0.143
-12.5	-0.186	0.08947	-0.091	0.804	0.014	1.000	0.020	-2.073	0.332	-0.239
-12.0	-0.147	0.08590	-0.094	0.793	0.014	1.000	0.020	-1.710	0.327	-0.388
-11.5	-0.107	0.08338	-0.097	0.784	0.014	1.000	0.023	-1.279	0.327	-0.657
-11.0	-0.067	0.07893	-0.100	0.774	0.015	1.000	0.023	-0.846	0.329	-1.247
-10.5	-0.026	0.07149	-0.103	0.762	0.016	1.000	0.023	-0.367	0.236	-3.677
-10.0	-0.506	0.06886	-0.106	0.752	0.016	1.000	0.026	-7.345	0.234	0.040
-9.5	-0.434	0.06449	-0.110	0.741	0.017	1.000	0.026	-6.731	0.295	-0.002
-9.0	-0.362	0.06169	-0.113	0.728	0.018	1.000	0.029	-5.873	0.295	-0.061
-8.5	-0.291	0.05763	-0.116	0.715	0.019	1.000	0.030	-5.046	0.296	-0.149
-8.0	-0.220	0.05590	-0.119	0.703	0.020	1.000	0.033	-3.927	0.296	-0.293
-7.5	-0.149	0.05269	-0.122	0.689	0.021	1.000	0.037	-2.822	0.296	-0.573
-7.0	-0.078	0.04901	-0.126	0.675	0.023	1.000	0.040	-1.601	0.297	-1.353
-6.5	-0.009	0.04690	-0.129	0.658	0.025	1.000	0.045	-0.190	0.298	-14.216
-6.0	0.060	0.04405	-0.132	0.644	0.026	1.000	0.052	1.358	0.298	2.462
-5.5	0.128	0.04201	-0.136	0.626	0.029	1.000	0.059	3.040	0.299	1.312
-5.0	0.195	0.04010	-0.139	0.608	0.032	1.000	0.070	4.853	0.299	0.964
-4.5	0.260	0.03737	-0.142	0.589	0.035	1.000	0.099	6.963	0.299	0.796
-4.0	0.324	0.03447	-0.145	0.568	0.040	1.000	0.140	9.412	0.303	0.698
-3.5	0.385	0.02805	-0.149	0.545	0.046	1.000	0.297	13.727	0.438	0.636
-3.0	0.433	0.02053	-0.166	0.520	0.053	1.000	0.967	21.097	0.418	0.633
-2.5	0.496	0.02101	-0.167	0.488	0.062	1.000	0.968	23.613	0.274	0.587
-2.0	0.559	0.02163	-0.169	0.456	0.074	1.000	0.968	25.839	0.274	0.552
-1.5	0.622	0.02198	-0.170	0.431	0.088	1.000	0.969	28.276	0.275	0.524
-1.0	0.684	0.02096	-0.172	0.421	0.106	1.000	0.969	32.633	0.275	0.501
-0.5	0.746	0.02103	-0.174	0.412	0.131	1.000	0.969	35.494	0.275	0.482
0.0	0.809	0.02135	-0.175	0.407	0.159	1.000	0.969	37.877	0.274	0.466
0.5	0.871	0.02209	-0.176	0.403	0.194	1.000	0.970	39.438	0.323	0.453
1.0	0.861	0.02327	-0.179	0.399	0.249	0.916	0.971	36.988	0.357	0.458
1.5	0.913	0.02299	-0.181	0.396	0.925	0.907	0.963	39.727	0.291	0.448
2.0	0.966	0.02385	-0.183	0.393	0.934	0.897	0.963	40.483	0.294	0.440
2.5	1.016	0.02474	-0.186	0.389	0.942	0.886	0.962	41.064	0.301	0.433
3.0	1.063	0.02541	-0.188	0.386	0.950	0.871	0.963	41.836	0.305	0.427
3.5	1.112	0.02639	-0.191	0.380	0.959	0.860	0.963	42.141	0.307	0.422
4.0	1.159	0.02753	-0.194	0.374	0.962	0.846	0.962	42.079	0.314	0.417
4.5	1.204	0.02888	-0.197	0.368	0.961	0.832	0.962	41.692	0.321	0.413
5.0	1.247	0.03020	-0.200	0.363	0.961	0.815	0.962	41.300	0.324	0.410
5.5	1.292	0.03136	-0.203	0.355	0.962	0.801	0.963	41.217	0.325	0.407
6.0	1.337	0.03297	-0.207	0.347	0.962	0.787	0.963	40.549	0.332	0.405
6.5	1.378	0.03446	-0.210	0.340	0.962	0.771	0.963	40.000	0.340	0.403
7.0	1.419	0.03636	-0.214	0.332	0.962	0.754	0.963	39.037	0.341	0.401
7.5	1.462	0.03813	-0.218	0.323	0.962	0.740	0.963	38.336	0.347	0.399
8.0	1.500	0.04018	-0.222	0.315	0.961	0.723	0.962	37.325	0.345	0.398
8.5	1.543	0.04222	-0.226	0.304	0.961	0.713	0.962	36.552	0.347	0.396
9.0	1.581	0.04458	-0.230	0.294	0.961	0.697	0.962	35.461	0.353	0.395
9.5	1.621	0.04671	-0.234	0.283	0.961	0.686	0.962	34.713	0.344	0.394
10.0	1.663	0.04908	-0.237	0.270	0.961	0.677	0.962	33.884	0.346	0.393
10.5	1.702	0.05154	-0.241	0.257	0.961	0.666	0.963	33.021	0.349	0.392
11.0	1.742	0.05398	-0.245	0.242	0.961	0.658	0.963	32.273	0.346	0.391
11.5	1.781	0.05666	-0.249	0.225	0.963	0.651	0.964	31.442	0.343	0.390
12.0	1.822	0.05931	-0.253	0.203	0.963	0.647	0.964	30.718	0.332	0.389
12.5	1.865	0.06283	-0.256	0.173	0.963	0.647	0.964	29.687	0.329	0.387
13.0	1.906	0.07258	-0.259	0.030	0.963	0.646	0.965	26.263	0.382	0.386
13.5	1.928	0.07723	-0.264	0.021	0.963	0.628	0.965	24.964	0.482	0.387
14.0	1.949	0.08128	-0.269	0.018	0.964	0.610	0.965	23.975	0.513	0.388
14.5	1.966	0.08610	-0.274	0.015	0.964	0.591	0.965	22.833	0.553	0.389
15.0	1.982	0.09127	-0.279	0.013	0.964	0.572	0.965	21.716	0.563	0.391

Name = naca-6416
Mach = 0; Re = 100000; T.U. = 1.0; T.L. = 1.0
Surface Finish = 0; Stall model = 1; Transition model = 1; Aspect Ratio = 0; ground effect = 0
?	Cl	Cd	Cm 0.25	T.U.	T.L.	S.U.	S.L.	L/D	A.C.	C.P.
[¡]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]	[-]
-15.0	-0.362	0.11386	-0.076	0.844	0.012	1.000	0.019	-3.182	0.341	0.042
-14.5	-0.330	0.10773	-0.079	0.836	0.013	1.000	0.019	-3.059	0.338	0.012
-14.0	-0.295	0.09865	-0.081	0.827	0.013	1.000	0.020	-2.988	0.334	-0.026
-13.5	-0.259	0.09296	-0.084	0.819	0.013	1.000	0.021	-2.784	0.332	-0.076
-13.0	-0.222	0.09171	-0.087	0.812	0.013	1.000	0.022	-2.420	0.333	-0.144
-12.5	-0.185	0.08499	-0.091	0.804	0.014	1.000	0.021	-2.175	0.332	-0.240
-12.0	-0.146	0.08186	-0.094	0.793	0.014	1.000	0.022	-1.786	0.327	-0.391
-11.5	-0.106	0.07793	-0.097	0.784	0.014	1.000	0.025	-1.359	0.327	-0.663
-11.0	-0.066	0.07440	-0.100	0.774	0.015	1.000	0.025	-0.887	0.329	-1.263
-10.5	-0.025	0.06786	-0.103	0.762	0.016	1.000	0.025	-0.375	0.236	-3.801
-10.0	-0.506	0.06668	-0.106	0.752	0.016	1.000	0.029	-7.581	0.235	0.040
-9.5	-0.434	0.06185	-0.109	0.741	0.017	1.000	0.029	-7.015	0.295	-0.002
-9.0	-0.362	0.05847	-0.113	0.728	0.018	1.000	0.032	-6.193	0.295	-0.061
-8.5	-0.291	0.05519	-0.116	0.715	0.019	1.000	0.034	-5.267	0.295	-0.148
-8.0	-0.219	0.05341	-0.119	0.703	0.020	1.000	0.039	-4.107	0.295	-0.293
-7.5	-0.149	0.05008	-0.122	0.689	0.021	1.000	0.043	-2.967	0.297	-0.573
-7.0	-0.078	0.04648	-0.126	0.675	0.023	1.000	0.047	-1.687	0.297	-1.352
-6.5	-0.009	0.04458	-0.129	0.658	0.025	1.000	0.054	-0.200	0.297	-14.206
-6.0	0.060	0.04178	-0.132	0.644	0.026	1.000	0.067	1.430	0.297	2.460
-5.5	0.127	0.03929	-0.135	0.626	0.029	1.000	0.080	3.245	0.298	1.311
-5.0	0.194	0.03686	-0.139	0.608	0.032	1.000	0.103	5.267	0.297	0.964
-4.5	0.259	0.03269	-0.141	0.589	0.035	1.000	0.181	7.912	0.465	0.797
-4.0	0.307	0.01817	-0.163	0.568	0.040	1.000	0.964	16.887	0.456	0.780
-3.5	0.370	0.01813	-0.164	0.545	0.046	1.000	0.967	20.408	0.275	0.694
-3.0	0.433	0.01891	-0.166	0.520	0.053	1.000	0.968	22.904	0.274	0.633
-2.5	0.496	0.01912	-0.167	0.488	0.062	1.000	0.968	25.951	0.274	0.587
-2.0	0.559	0.01913	-0.169	0.456	0.074	1.000	0.969	29.219	0.274	0.552
-1.5	0.622	0.01916	-0.170	0.431	0.088	1.000	0.969	32.439	0.275	0.524
-1.0	0.684	0.01841	-0.172	0.421	0.106	1.000	0.970	37.157	0.275	0.501
-0.5	0.746	0.01888	-0.174	0.412	0.131	1.000	0.970	39.548	0.275	0.482
0.0	0.809	0.01969	-0.175	0.407	0.159	1.000	0.970	41.067	0.274	0.466
0.5	0.871	0.01991	-0.176	0.403	0.194	1.000	0.971	43.746	0.272	0.453
1.0	0.933	0.01959	-0.178	0.399	0.249	1.000	0.971	47.656	0.272	0.441
1.5	0.996	0.01954	-0.179	0.396	0.925	1.000	0.963	50.966	0.343	0.430
2.0	0.985	0.02111	-0.183	0.393	0.934	0.920	0.963	46.646	0.382	0.435
2.5	1.038	0.02199	-0.185	0.389	0.942	0.911	0.962	47.190	0.293	0.428
3.0	1.089	0.02247	-0.187	0.386	0.950	0.901	0.963	48.451	0.296	0.422
3.5	1.141	0.02308	-0.190	0.380	0.959	0.893	0.963	49.431	0.298	0.416
4.0	1.192	0.02391	-0.192	0.374	0.962	0.884	0.962	49.836	0.302	0.411
4.5	1.241	0.02510	-0.195	0.368	0.961	0.873	0.962	49.425	0.308	0.407
5.0	1.288	0.02630	-0.198	0.363	0.961	0.861	0.962	48.986	0.311	0.403
5.5	1.336	0.02701	-0.201	0.355	0.962	0.850	0.963	49.458	0.313	0.400
6.0	1.383	0.02837	-0.204	0.347	0.962	0.839	0.963	48.754	0.320	0.397
6.5	1.428	0.02941	-0.207	0.340	0.962	0.825	0.963	48.536	0.326	0.395
7.0	1.472	0.03089	-0.210	0.332	0.962	0.812	0.963	47.639	0.327	0.393
7.5	1.516	0.03254	-0.214	0.323	0.962	0.800	0.963	46.595	0.333	0.391
8.0	1.558	0.03438	-0.218	0.315	0.961	0.786	0.962	45.313	0.336	0.390
8.5	1.601	0.03596	-0.221	0.304	0.961	0.774	0.962	44.518	0.343	0.388
9.0	1.639	0.03781	-0.225	0.294	0.961	0.760	0.962	43.354	0.347	0.387
9.5	1.680	0.03990	-0.229	0.283	0.961	0.748	0.962	42.117	0.343	0.386
10.0	1.721	0.04198	-0.233	0.270	0.961	0.738	0.962	40.992	0.349	0.385
10.5	1.759	0.04416	-0.237	0.257	0.961	0.726	0.963	39.824	0.355	0.385
11.0	1.796	0.04643	-0.241	0.242	0.961	0.715	0.963	38.688	0.354	0.384
11.5	1.834	0.04916	-0.244	0.225	0.963	0.706	0.964	37.299	0.355	0.383
12.0	1.871	0.05198	-0.248	0.203	0.963	0.697	0.964	35.988	0.353	0.383
12.5	1.908	0.05562	-0.252	0.173	0.963	0.690	0.964	34.298	0.400	0.382
13.0	1.930	0.06688	-0.257	0.030	0.963	0.670	0.965	28.852	0.501	0.383
13.5	1.949	0.07142	-0.262	0.021	0.963	0.649	0.965	27.283	0.505	0.385
14.0	1.969	0.07577	-0.267	0.018	0.964	0.631	0.965	25.990	0.508	0.386
14.5	1.987	0.08042	-0.272	0.015	0.964	0.613	0.965	24.711	0.539	0.387
15.0	2.004	0.08505	-0.277	0.013	0.964	0.595	0.965	23.562	0.546	0.388