| EPSRC Reference: |
GR/R07738/01 |
| Title: |
An Integrated Aerodynamics/Propulsion Solution In Micro Air Vehicles |
| Principal Investigator: |
Gursul, Professor I |
| Other Investigators: |
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| Researcher Co-Investigators: |
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| Project Partners: |
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| Department: |
Mechanical Engineering |
| Organisation: |
University of Bath |
| Scheme: |
Standard Research (Pre-FEC) |
| Starts: |
01 March 2001 |
Ends: |
30 September 2004 |
Value (£): |
107,361
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| EPSRC Research Topic Classifications: |
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| EPSRC Industrial Sector Classifications: |
| Aerospace, Defence and Marine |
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| Related Grants: |
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| Panel History: |
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Summary on Grant Application Form |
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An integrated aerodynamics/propulsion solution is proposed for Micro Air Vehicle (MAV) applications. The concept involves a synthetic jet integrated into the trailing edge of a thin, wedge shaped aerofoil. This proposed shape is based on the fact that sharp leading edges produce more life than rounded noses and a sharp trailing edge is no longer necessary for developing lift at low Reynolds numbers. The proposed configuration is simple and promises good aerodynamic performance. The integration of a synthetic jet takes advantage of the low Reynolds number regime, while propellers and flapping-wing propulsion systems suffer from either reduced effectiveness or increased cost can complexity.
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Key Findings |
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This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
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Potential use in non-academic contexts |
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This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
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Impacts |
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| Description |
This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk |
| Summary |
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| Date Materialised |
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Sectors submitted by the Researcher |
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This information can now be found on Gateway to Research (GtR) http://gtr.rcuk.ac.uk
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| Project URL: |
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| Further Information: |
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| Organisation Website: |
http://www.bath.ac.uk |