Extension of a three-dimensional viscous wing flow analysis: user's manual: VISTA 3-D code

Original publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] OCLC Number: (OCoLC)65176774 Excerpt: ... IMODEL Model problem parameter used in testing the code or flag to signify type of problem under consideration IMUSKER-Skin turbulence model parameter INCOMPR-Incompressible flow parameter 0-Compressible flow ( default ) 1-Incompressible flow INCORE-Logical variable indication whether variables are kept incore or are written onto disk. INTPRNT-Intermediate print flag ( Default-0 do not print )-Interface print flag ( Default-O ) INTRFC-Orders of accuracy of finite difference scheme in each of the IORDER three directions IORTHOG Indicates orthogonal or nonorthogonal problem lOUT Flag which controls variables that are printed out IPEROD Not used ( set to 0 ) IPLOT Plot flag IPRINTF Print flag for initial flow field 0-Do not print i-Do print IPRINTG-Print flag for geometry print 0-Do not print 1-Do print IPRINTL-Print flag for final flow field 0-Do not print 1-Do print IPRINTX-Print flag for final flow field 0 Do not print 1 Do print IPRNTZI Print flag ( unused ) IPRNTZ2 Print flag ( unused ) IPRNTZ3 Print flag ( unused ) IPRINTI Print flag for first time step ( Default-I ) PRNT24 Print flag for unsteady flow ( cf I )-Calculation run parameter IRUN 0-No do not run code 1-Yes run code; used when checking out initialization-13-