NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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)
Date Acquired
August 12, 2013
Publication Date
June 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 84-1245
Accession Number
84A35145
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available