The wind-tunnel/flight dynamics simulator has been applied to a limited study of the dynamic response at low speeds of the Handley-Page HP 115 aircraft. Motions with six degrees of freedom were simulated. The technique ...
A new closed loop system is described which enables the incidence, roll and motivator (i.e. control surface) angles of a wind tunnel model to be controlled remotely, either by hand or by analogue voltages derived from, ...