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.
Keywords
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