# R C^*     Phi^*          0.5 a^T a
50	2.88	2.877335359045955	2.6799096463597007
100	3.01	3.0073935749219656	2.6994029476335304
150	3.03	3.0282949972370052	2.724569689629631
200	3.06	3.054172131134294	2.749957755749046
