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The documentation for the current release is also available on this site.
NAG Library Manual, Mark 27.3
Interfaces:  FL   CL   CPP   AD 

NAG FL Interface Introduction
Example description
 D02GAF Example Program Results

 Problem with BETA =    0.00

 Solution on final mesh of 26 points
       X(I)        Y1(I)        Y2(I)        Y3(I)
       0.000       0.0000       0.0000       0.4695
       0.400       0.0375       0.1876       0.4673
       0.800       0.1497       0.3719       0.4511
       1.200       0.3336       0.5450       0.4104
       1.600       0.5828       0.6963       0.3424
       2.000       0.8864       0.8163       0.2558
       2.400       1.2309       0.9009       0.1678
       2.800       1.6026       0.9529       0.0953
       3.200       1.9900       0.9805       0.0464
       3.600       2.3851       0.9930       0.0193
       4.000       2.7834       0.9978       0.0069
       4.400       3.1829       0.9994       0.0021
       4.800       3.5828       0.9999       0.0006
       5.200       3.9828       1.0000       0.0001
       5.600       4.3828       1.0000       0.0000
       6.000       4.7828       1.0000       0.0000
       6.400       5.1828       1.0000       0.0000
       6.800       5.5828       1.0000       0.0000
       7.200       5.9828       1.0000      -0.0000
       7.600       6.3828       1.0000       0.0000
       8.000       6.7828       1.0000      -0.0000
       8.400       7.1828       1.0000       0.0000
       8.800       7.5828       1.0000      -0.0000
       9.200       7.9828       1.0000       0.0000
       9.600       8.3828       1.0000      -0.0000
      10.000       8.7828       1.0000      -0.0000

 Problem with BETA =    0.20

 Solution on final mesh of 26 points
       X(I)        Y1(I)        Y2(I)        Y3(I)
       0.000       0.0000       0.0000       0.6865
       0.400       0.0528       0.2584       0.6040
       0.800       0.2020       0.4814       0.5091
       1.200       0.4324       0.6636       0.4001
       1.600       0.7268       0.8007       0.2860
       2.000       1.0670       0.8939       0.1821
       2.400       1.4368       0.9498       0.1017
       2.800       1.8233       0.9791       0.0492
       3.200       2.2180       0.9924       0.0206
       3.600       2.6162       0.9976       0.0074
       4.000       3.0157       0.9993       0.0023
       4.400       3.4156       0.9998       0.0006
       4.800       3.8155       1.0000       0.0001
       5.200       4.2155       1.0000       0.0000
       5.600       4.6155       1.0000       0.0000
       6.000       5.0155       1.0000       0.0000
       6.400       5.4155       1.0000      -0.0000
       6.800       5.8155       1.0000      -0.0000
       7.200       6.2155       1.0000      -0.0000
       7.600       6.6155       1.0000      -0.0000
       8.000       7.0155       1.0000      -0.0000
       8.400       7.4155       1.0000      -0.0000
       8.800       7.8155       1.0000      -0.0000
       9.200       8.2155       1.0000      -0.0000
       9.600       8.6155       1.0000      -0.0000
      10.000       9.0155       1.0000      -0.0000