Input File with Rotor #Case title: This is a sample input file Mach alpha beta ReUe,mil Tinf,dR itwall Tw/Tinf ipwall 0.84 3.06 0.0 11.7 460.0 0 -1.0 0 sref cref bref xmc ymc zmc 0.5255 0.667 1.0 0.0 0.0 0.0 ioverset impl cfl1 iramp cfl2 cflmin GS_tol crelax 0 1 -20.0 50 150.0 5.0 0.0 1.0 itimeacc delta_t ntstep res_step imvgrd isolavg nbgnavg 0 0.3 500 -3.0 0 0 1500 irest mstage iresmth dqmax p_break pmin limiter 0 3 1 0.5 0.05 0.001 0. nupdate nwrest nwflo nwflobgn ipltqn idiagnos nodeypl 50 75 100 1500 2 0 0 iorder lapl-avg high-bc ifds ivisc itrip EV_lim 2 1 1 1 2 0 0.0 ncyc nengines nsinkbc nrotor compF&M p_bc1002 cldes 1000 0 0 1 0 0. 0. rotid inner_R outer_R cen_X cen_Y cen_Z 502 0.0 24.0 0.0 0.0 0.0 Advratio thrst_c torq_c irotat rotsim 0.20 0.00861 0.0 1 0 RED denotes the primary parameters that will require attention from the user. GREEN denotes the parameters that will require attention from the user for this option. The remaining parameters can generally remain unchanged. NASA Official Responsible For Content: Dr. Neal T. Frink Site Curator: Dr. Neal T. Frink Last Updated: August 8, 2003 Feedback on Langley Products and Services
RED denotes the primary parameters that will require attention from the user. GREEN denotes the parameters that will require attention from the user for this option. The remaining parameters can generally remain unchanged.
