Transition Duct Geometry Polynomial Coefficients

 The superellipse of the transition duct boundary is given
by

   (y/a)**(eta) + (z/b)**(eta) = 1

where a,b and eta are functions of streamwise position x.
The quantities (a/R), (b/R) and eta are given by polynomials
of the form c0 + c1*(x/R) + c2*(x/R)**2 + .. + c5*(x/R)**5
The tables below give the coefficients c0..c5 for a,b and eta
at the various x intervals.

The radius R of the inlet circular duct is 102.15 mm.

            a/R                 b/R                 eta
 x/R .le. 1.0
c0       1.000000000         1.000000000         2.000000000
c1       0.000000000         0.000000000         0.000000000
c2       0.000000000         0.000000000         0.000000000
c3       0.000000000         0.000000000         0.000000000
c4       0.000000000         0.000000000         0.000000000
c5       0.000000000         0.000000000         0.000000000

 1.0 .le. x/R .le. 1.96
c0       0.875682170         1.110219900         8.483346500
c1       0.386998680        -0.343102010       -21.329880000
c2      -0.387831440         0.343807210        26.148548000
c3       0.096543991        -0.085532496       -15.173079000
c4       0.041969148        -0.037245857         4.361414300
c5      -0.013362557         0.011853259        -0.490349400

 1.96 .le. x/R .le. 2.92
c0      -0.373365600         2.216277900         1.097110900
c1       3.351019300        -2.968311200         2.362357900
c2      -3.279659000         2.905634800        -2.878524200
c3       1.552321700        -1.375475300         2.062091200
c4      -0.336649300         0.298313020        -0.641363010
c5       0.027262234        -0.024157751         0.080685615

 2.92 .le. x/R .le. 4.125
c0      14.292266000       -10.787227000     -1858.441200000
c1     -19.643522000        17.419488000      2828.735300000
c2      11.204615000        -9.936079200     -1704.806300000
c3      -3.038098800         2.694140300       508.598460000
c4       0.396892830        -0.351957700       -74.960370000
c5      -0.020128978         0.017849940         4.365165200

 x/R .ge. 4.125
c0       1.546359100         0.515449880        10.000000000
c1       0.000000000         0.000000000         0.000000000
c2       0.000000000         0.000000000         0.000000000
c3       0.000000000         0.000000000         0.000000000
c4       0.000000000         0.000000000         0.000000000
c5       0.000000000         0.000000000         0.000000000