Calculation of quasi-one-dimensional flows with shocksThe two-point subsonic method of Wornom (1983) is modified to permit calculation of transonic flows with shocks using artificial density and/or artificial pressure. This method, which requires no numerical boundary conditions, is then used to calculate transonic flow for large and small CFL (Courant-Friedrichs-Lewy) numbers. Convergence acceleration is achieved for small CFL numbers by using multi-grid.
Document ID
19840052358
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wornom, S. F. (NASA Langley Research Center Hampton, VA, United States)
Hafez, M. M. (NASA Langley Research Center Hampton, VA, United States)