51	=ix mesh system <102
1.8	=omega relaxation factor
0.086	=dm camber ratio (<0 means flying wing profile)
0.12	=em thickness ratio                                           
3	=ithick (1/2/3/4/5/6) ellip/semi-cubic/q-j/naca00xx/selig/super-selig 
0.0	=alphd angle of incidence (deg.)                              
1.0e5	=Re reynolds number                                           thinabl
21	=ivx end of viscous interaction region                        thinabl
0.5	=xinv location of inverse coupling                            thinvair
1.	=wxm wake length (m)                                          invair