Publisher's Synopsis
A copy of the PHOENICS input files and FORTRAN code developed for the modeling of thrust chambers is given. These copies are contained in the Appendices. The listings are contained in Appendices A through E. Appendix A describes the input statements relevant to thrust chamber modeling as well as the FORTRAN code developed for the Satellite program. Appendix B describes the FORTRAN code developed for the Ground program. Appendices C through E contain copies of the Q1 (input) file, the Satellite program, and the Ground program respectively. Daley, P. L. and Owens, S. F. Marshall Space Flight Center APPLICATIONS PROGRAMS (COMPUTERS); COMBUSTIBLE FLOW; COMPUTATIONAL FLUID DYNAMICS; COMPUTERIZED SIMULATION; FLOW DISTRIBUTION; NAVIER-STOKES EQUATION; ROCKET ENGINE DESIGN; SPACE SHUTTLE MAIN ENGINE; THRUST CHAMBERS; CHEMICAL EQUILIBRIUM; FORTRAN; FUEL INJECTION; GRID GENERATION (MATHEMATICS); HEAT TRANSFER; SUBROUTINES; WALL TEMPERATURE...
