Abstract
One of the important issues in the assessment of intake/engine compatibility in civil turbofan engines is the prediction of the coupling effects between the intake and the engine. An actuator-disk model has been applied to the calculations of the flow through a high-bypass-ratio turbofan geometry, including the presence of the core-support pylon and a nonaxisymmetric inlet, and the effects of the core engine. The results of a series of calculations are presented, and the nature of the interactions between the flow through a fan and the system components is addressed.
| Original language | English |
|---|---|
| Pages (from-to) | 697-704 |
| Number of pages | 8 |
| Journal | Journal of Propulsion and Power |
| Volume | 16 |
| Issue number | 4 |
| DOIs | |
| Publication status | Published - 2000 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Fuel Technology
- Mechanical Engineering
- Space and Planetary Science