Abstract
Techniques developed for compressible flow past a profile are utilized and generalized to deal with linear and nonlinear boundary conditions for the mass flux for interior regions. Partial uniqueness is demonstrated for a subsonic flow in a class of mixed flows.
Original language | English (US) |
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Pages (from-to) | 207-215 |
Number of pages | 9 |
Journal | Appl Anal |
Volume | 5 |
Issue number | 3 |
DOIs | |
State | Published - 1976 |
All Science Journal Classification (ASJC) codes
- Analysis
- Applied Mathematics