Abstract
In connection with the energy supply of ramjet engines with supersonic combustion, the partial task of fuel supply by secondary injection is treated. This leads to the concept of a combined multi-jet injection. An injection with minimal loss for the main flow is obtained by several gaseous individual jets injected laterally into the primary flow. This injection method is approximately described by a calculation model and is experimentally tested in a short time test installation.
Translated title of the contribution | Fuel Supply in Supersonic Combustion. |
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Original language | German |
Pages (from-to) | 379-393 |
Number of pages | 15 |
Journal | Zeitschrift fur Flugwissenschaften und Weltraumforschung |
Volume | 22 |
Issue number | 11 |
State | Published - 1974 |