Method of Calculating a Two-Phase Ejector,
Abstract
A method of designing a two phase two component injector is presented on the basis of an experimental study. The operation of the injector is compared under subsonic and supersonic conditions. It is shown that for fixed conditions (nozzle geometry and initial parameters) there is a certain optimum area of the throat of the exit cone where the highest back pressure is reached. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 11, 1972
- Accession Number
- AD0754051
Entities
People
- G. V. Tsiklauri
- M. E. Deich
- N. A. Dikii
- Yu. F. Kalinin
Organizations
- National Air and Space Intelligence Center