Numerical and Experimental Aeroelastic Analysis of High Aspect Ratio Wings .

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Title
Numerical and Experimental Aeroelastic Analysis of High Aspect Ratio Wings .
CoPED ID
57c03e82-fda5-4b70-a207-df7149669448
Status
Active
Funders
EPSRC
EPSRC
Value
No funds listed.
Start Date
Sept. 30, 2021
End Date
Sept. 29, 2024
Description

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This exciting research project is focused on the accurate nonlinear numerical and experimental aeroelastic analysis of flexible wings and explore the use of reduced-order models to ensure the practicability in the use of developed methods for domains with large degrees of freedom. It will also explore the use of high-fidelity numerical modelling, including turbulence modelling. This research is applicable to the aeroelasticity of flexible and large wind turbine blades. The unified scaling law in solid continuum recently developed by the research team here at Brunel will be further developed for experimental investigations during this research project.

Thomas Goonan STUDENT_PER

Subjects by relevance
  1. Research methods
  2. Numerical methods
  3. Experimental methods
  4. Development projects
  5. Numerical analysis
  6. Research

Extracted key phrases
  1. Fidelity numerical modelling
  2. Accurate nonlinear numerical
  3. High Aspect Ratio Wings
  4. Exciting research project
  5. Experimental Aeroelastic Analysis
  6. Large wind turbine blade
  7. Research team
  8. Flexible wing
  9. Turbulence modelling
  10. Use
  11. Large degree
  12. Experimental investigation
  13. Unified scaling law

Related Pages

UKRI project entry

UK Project Locations