UNIQUENESS THEOREMS FOR THE COMPRESSIBLE FLOW EQUATION.

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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 languageEnglish (US)
Pages (from-to)207-215
Number of pages9
JournalAppl Anal
Volume5
Issue number3
DOIs
StatePublished - Jan 1 1976

All Science Journal Classification (ASJC) codes

  • Analysis
  • Applied Mathematics

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