MRes Gas Turbine Aerodynamics + PhD

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Title
MRes Gas Turbine Aerodynamics + PhD
CoPED ID
e8620b86-380b-4b4d-a52d-bec6642d0be1
Status
Closed
Funders
EPSRC
EPSRC
Value
No funds listed.
Start Date
Sept. 30, 2017
End Date
Sept. 29, 2021
Description

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MRes-The programme is designed to develop the following broad themes:

Component (compressor, combustor, turbine) aerodynamics
System-level design and component integration
Methods (experimental and computational) for aerodynamic research and design
Researcher skills
Experience of university research groups and industry facilities

University of Cambridge LEAD_ORG
Rolls-Royce plc STUDENT_PP_ORG

Paul G. Tucker SUPER_PER
Kwun Ma STUDENT_PER

Subjects by relevance
  1. Planning and design
  2. Research programmes
  3. Research
  4. Industrial design
  5. Compressors
  6. Research methods
  7. Design (artistic creation)
  8. Experimental methods
  9. Designer (computer programmes)

Extracted key phrases
  1. MRes Gas Turbine Aerodynamics
  2. Level design
  3. Aerodynamic research
  4. Component integration
  5. Broad theme
  6. Mres
  7. Programme
  8. Phd
  9. University research group

Related Pages

UKRI project entry

UK Project Locations