Gupta, Abhineet2014-11-102014-11-102013-08-10https://hdl.handle.net/11299/167676Included is a report describing the moment of inertia testing done on the Body Freedom Flutter (BFF) aircraft. Pitch inertia was found treating the aircraft as a compound pendulum; roll and yaw inertias were found using the bifilar pendulum technique. Included with the report is a summary of the experimentally determined inertia values.enMoment of InertiaBody Freedom FlutterBFFReport