On Parameters of a Supersonic Combustion Chamber with Organization of Combustion at the Flame Front,
Abstract
In some engineering problems, it is necessary to burn fuel in the combustion chamber with supersonic flow. As a rule, the scheme of organization of the process in such a chamber presupposes a separate accompanying feed of fuel and oxidant in which combustion of fuel takes place in a diffusion flame front. In this article we give theoretical results of investigation of a supersonic combustion chamber in which combustion of the fuel mixture takes place in a oblique flame front stabilized by an external source (analogous to the subsonic combustion chambers of ramjets). The possibility of the existence of such an oblique flame front in a supersonic flow of fuel mixture was previously proved experimentally.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 25, 1985
- Accession Number
- ADA161176
Entities
People
- E. L. Solokhin
- V. A. Mironenko
- Vladimir I. Ivanov
Organizations
- National Air and Space Intelligence Center