Распределение циркуляции по размаху плоского крыла.

Применяем следующие обозначения:

L – размах крыла;

L_ц – размах центроплана;

h – сужение крыла;

– относительная координата z.

Таблица 4.1.

Распределение циркуляции при L_ц/L=0.5.

h
0.0	0.1	0.2	0.3	0.4	0.5	0.6	0.7	0.8	0.9	1.0
1.2	1.172	1.172	1.170	1.159	1.137	1.094	1.029	0.946	0.941	0.693	0.0
1.4	1.179	1.179	1.177	1.166	1.142	1.097	1.029	0.941	0.832	0.676	0.0
1.6	1.186	1.186	1.184	1.173	1.147	1.100	1.029	0.936	0.823	0.659	0.0
1.8	1.193	1.193	1.191	1.180	1.152	1.103	1.029	0.931	0.814	0.642	0.0
2.0	1.200	1.200	1.196	1.186	1.158	1.107	1.029	0.927	0.804	0.634	0.0
2.2	1.207	1.207	1.205	1.192	1.164	1.111	1.029	0.923	0.794	0.626	0.0
2.4	1.214	1.214	1.211	1.199	1.169	1.114	1.028	0.922	0.784	0.608	0.0
2.6	1.220	1.220	1.218	1.205	1.174	1.117	1.028	0.913	0.775	0.596	0.0
2.8	1.227	1.227	1.224	1.211	1.180	1.120	1.028	0.908	0.765	0.583	0.0
3.0	1.233	1.233	1.231	1.218	1.185	1.124	1.028	0.904	0.755	0.571	0.0
3.2	1.237	1.237	1.235	1.222	1.188	1.126	1.028	0.901	0.749	0.563	0.0
3.4	1.242	1.242	1.239	1.225	1.191	1.127	1.028	0.899	0.743	0.555	0.0
3.6	1.256	1.256	1.243	1.229	1.194	1.128	1.028	0.896	0.738	0.547	0.0
3.8	1.250	1.250	1.247	1.232	1.197	1.130	1.028	0.893	0.732	0.538	0.0
4.0	1.254	1.254	1.251	1.236	1.200	1.132	1.028	0.891	0.726	0.530	0.0
4.2	1.257	1.257	1.253	1.238	1.202	1.133	1.028	0.890	0.723	0.525	0.0
4.4	1.259	1.259	1.255	1.241	1.204	1.135	1.029	0.888	0.719	0.520	0.0
4.6	1.262	1.262	1.257	1.243	1.206	1.136	1.029	0.887	0.716	0.515	0.0
4.8	1.265	1.265	1.259	1.145	1.208	1.137	1.029	0.885	0.713	0.510	0.0
5.0	1.267	1.267	1.262	1.248	1.210	1.139	1.029	0.884	0.709	0.505	0.0

Таблица 4.2. Распределение циркуляции при L_ц/L=0.25.

h
0.0	0.1	0.2	0.3	0.4	0.5	0.6	0.7	0.8	0.9	1.0
1.2	1.209	1.208	1.191	1.174	1.124	1.073	1.028	0.923	0.839	0.688	0.0
1.4	1.222	1.220	1.202	1.178	1.130	10.72	1.019	0.916	0.826	0.675	0.0
1.6	1.235	1.231	1.213	1.182	1.136	10.74	1.010	0.909	0.813	0.622	0.0
1.8	1.248	1.242	1.224	1.191	1.141	1.075	1.001	0.902	0.800	0.649	0.0
2.0	1.260	1.254	1.234	1.199	1.146	1.076	0.991	0.895	0.787	0.635	0.0
2.2	1.272	1.266	1.144	1.207	1.151	1.077	0.987	0.888	0.774	0.621	0.0
2.4	1.284	1.277	1.255	1.215	1.156	1.078	0.984	0.882	0.762	0.607	0.0
2.6	1.297	1.289	1.265	1.224	1.161	1.079	0.980	0.875	0.749	0.594	0.0
2.8	1.309	1.300	1.276	1.232	1.166	1.080	0.977	0.867	0.737	0.580	0.0
3.0	1.321	1.312	1.286	1.240	1.171	1.081	0.973	0.862	0.724	0.566	0.0
3.2	1.328	1.319	1.292	1.245	1.174	1.082	0.971	0.855	0.717	0.558	0.0
3.4	1.335	1.325	1.195	1.149	1.177	1.083	0.969	0.849	0.710	0.549	0.0
3.6	1.341	1.332	1.303	1.254	1.180	1.093	0.967	0.842	0.702	0.541	0.0
3.8	1.348	1.338	1.309	1.258	1.183	1.084	0.965	0.836	0.695	0.532	0.0
4.0	1.355	1.345	1.315	1.263	1.186	1.085	0.963	0.829	0.688	0.524	0.0
4.2	1.360	1.349	1.320	1.266	1.188	1.085	0.962	0.826	0.683	0.513	0.0
4.4	1.365	1.354	1.325	1.269	1.191	1.085	0.961	0.823	0.678	0.501	0.0
4.6	1.369	1.358	1.331	1.273	1.193	1.085	0.960	0.82	0.672	0.490	0.0
4.8	1.374	1.363	1.336	1.276	1.196	1.085	0.959	0.817	0.667	0.478	0.0
5.0	1.379	1.367	1.341	1.278	1.198	1.085	0.958	0.814	0.66	0.467	0.0

Таблица 4.3. Распределение циркуляции при Lц/L=0.0.

h
0.0	0.1	0.2	0.3	0.4	0.5	0.6	0.7	0.8	0.9	1.0
1.0	1.129	1.126	1.120	1.110	1.096	1.077	1.046	0.995	0.914	0.760	0.0
1.2	1.158	1.153	1.143	1.126	1.103	1.073	1.033	0.976	0.892	0.738	0.0
1.4	1.186	1.180	1.166	1.142	1.110	1.070	1.020	0.957	0.870	0.716	0.0
1.6	1.215	1.208	1.190	1.157	1.116	1.066	1.007	0.937	0.847	0.695	0.0
1.8	1.243	1.235	1.213	1.173	1.123	1.063	0.994	0.918	0.825	0.673	0.0
2.0	1.272	1.262	1.236	1.189	1.130	1.059	0.981	0.899	0.803	0.651	0.0
2.2	1.286	1.276	1.247	1.196	1.134	1.059	0.976	0.390	0.791	0.643	0.0
2.4	1.301	1.289	1.258	1.203	1.137	1.058	0.971	0.881	0.779	0.634	0.0
2.6	1.315	1.303	1.269	1.109	1.141	1.058	0.967	0.872	0.767	0.626	0.0
2.8	1.330	1.316	1.280	1.216	1.144	1.057	0.962	0.863	0.755	0.617	0.0
3.0	1.344	1.330	1.291	1.113	1.148	1.057	0.957	0.854	0.743	0.609	0.0
3.2	1.352	1.338	1.298	1.229	1.150	1.056	0.954	0.849	0.735	0.596	0.0
3.4	1.361	1.346	1.305	1.235	1.153	1.056	0.951	0.843	0.728	0.583	0.0
3.6	1.369	1.354	1.311	1.240	1.155	1.055	0.948	0.838	0.720	0.560	0.0
3.8	1.378	1.362	1.318	1.246	1.158	1.055	0.945	0.832	0.713	0.556	0.0
4.0	1.386	1.30	1.325	1.252	1.160	1.054	0.942	0.827	0.705	0.543	0.0
4.2	1.92	1.376	1.330	1.256	1.162	1.054	0.940	0.824	0.700	0.539	0.0
4.4	1.398	1.382	1.335	1.260	1.164	1.055	0.939	0.820	0.694	0.531	0.0
4.6	1.404	1.387	1.339	1.263	1.167	1.055	0.937	0.817	0.689	0.524	0.0
4.8	1.410	1.393	1.334	1.267	1.169	1.056	0.936	0.813	0.683	0.518	0.0
5.0	1.416	1.399	1.349	1.271	1.171	1.056	0.934	0.810	0.678	0.512	0.0