A method of increasing the performance of an aircraft, missile, munition or ground vehicle
with plasma actuators, and more particularly of controlling fluid flow across their surfaces or …

A system in accordance with present embodiments includes a ground controller and an
unmanned aerial vehicle including communications circuitry configured to transmit signals to …

A projectile incorporates one or more spoiler-tabbed spin ning disks to effect flow around the
projectile and thus impart steering forces and/or moments. The spoiler tabs may be …

A flow control apparatus includes a plasma actuator, a storage device, and a control circuit.
The plasma actuator causes discharge in a discharge area by applying an alternating …

US9789954B2 - Method of controlling boundary layer flow - Google Patents US9789954B2 -
Method of controlling boundary layer flow - Google Patents Method of controlling boundary layer …

Related US Application Data Continuation of application No. 11/415,534, filed on May 2,
2006, now Pat. No. 8,191,833, which is a continuation of application No. 10/750,422, filed on …

A method and an instrumentation system for an aircraft are provided. The method of
presenting aircraft information includes activating a master indicator in response to a trigger …

The present invention relates to a missile or aircraft with a hierarchical, modular, closed-loop
flow control system and more particularly to aircraft or missile with a flow control system for …

An apparatus including a controllable fluid-contacting surface is provided. In another aspect,
the present apparatus includes a flexible membrane and multiple actuators each having an …

A discharge platform comprises an air propulsion mechanism that propels the discharge
platform through the air. The discharge platform also comprises a special effect storage …