Abstract
Based on the performance characteristics of the turbo-components a calculation method for theoretical investigations of multi-flow, multi-spool engines with variable geometry is described. Furthermore, this paper outlines as an example for a wide range of flight conditions the effects of variable nozzles and turbines on the off-design performance of a typical low-bypass engine.
| Translated title of the contribution | On the Off-Design Operation of Bypass-Engines with Variable Nozzles and Turbines. |
|---|---|
| Original language | German |
| Pages (from-to) | 268-275 |
| Number of pages | 8 |
| Journal | Zeitschrift fur Flugwissenschaften und Weltraumforschung |
| Volume | 24 |
| Issue number | 5 |
| State | Published - 1976 |