EXPERIMENTAL AND DESIGN STUDIES FOR TURBO-RAMJET COMBINATION ENGINE VOLUME VI - COMBUSTION TESTS AT LES GATINES.
Abstract
The combustion chamber model of a turbo-ramjet combination engine was tested on the 15,000-horsepower bench at Les Gatines. Only the secondary flow was supplied; the primary flow was not simulated. The measurement methods and th data analysis procedures were developed from the first stage of the tests; also, the behavior of the test implements were verified and improved. The internal flame holder was studied in the second part of the tests. A combustion sytem incorporating a pilot burner was developed in the last stage. Equivalence ratios ranging from 0.12 to 0.46 were investigated. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1966
- Accession Number
- AD0484775
Entities
People
- A. Gozlan
- M. Ravel
- P. Chaulin