Summaries - Office of Research & Innovation
Research Summaries
Back Flapping Wing Aerodynamics and Control for Maneuverable Hovering Micro Air Vehicles
Fiscal Year | 2007 |
Division | Graduate School of Engineering & Applied Science |
Department | Mechanical & Aerospace Engineering |
Investigator(s) | Jones, Kevin D. |
Sponsor | Pacific Soft (Other) |
Summary | Wind tunnel test results will provide data for validation of numerical simulations performed by Pacific Soft. Results from the numerical simulations will be used to guide the design of a radio controlled flying model. |
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Publications | Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal |
Data | Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal |