MRes Gas Turbine Aerodynamics + PhD in Installation Effects on Variable Pitch Fans

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Title
MRes Gas Turbine Aerodynamics + PhD in Installation Effects on Variable Pitch Fans
CoPED ID
a3285f83-39e5-491f-9898-dc8cf3380a70
Status
Closed
Funders
EPSRC
EPSRC
Value
No funds listed.
Start Date
Sept. 30, 2017
End Date
Dec. 31, 2021
Description

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The forward thrust flow field is also important since the low speed
operating points at take-off and landing are prone to instabilities and any installation effects
may have a big impact on the engine performance.
The review of the existing literature on variable.
The plan includes the investigation of the ADP model using both unsteady
RANS simulations and experiments. Turbomachinery installation effects will be the main
subject of interest for the PhD project.

University of Cambridge LEAD_ORG
Rolls-Royce plc STUDENT_PP_ORG

Cesare Hall SUPER_PER
Kwun Ma STUDENT_PER

Subjects by relevance
  1. Simulation

Extracted key phrases
  1. MRes Gas Turbine Aerodynamics
  2. Variable Pitch Fans
  3. Installation Effects
  4. Forward thrust flow field
  5. Phd project
  6. Turbomachinery installation effect
  7. Low speed
  8. Engine performance
  9. Big impact
  10. ADP model
  11. Ran simulation

Related Pages

UKRI project entry

UK Project Locations