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PNEUMATIC VORTEX CONTROL .AJAA-98-4449
Forebody pneumatic vortex control has previously been demonstrated through full-scale flight test to be effective for directional control of aircraft at low Mach number and high angle-ofattack flightExpand
A 98-37266 HIGH SPEED , LOW ANGLE-OF-ATTACK PNEUMATIC VORTEX CONTROL . AJAA-98-4449
Forebody pneumatic vortex control has previously been demonstrated through full-scale flight test to be effective for directional control of aircraft at low Mach number and high angle-ofattack flightExpand
Flying qualities of the X-29 forward swept wing aircraft
An overview of the X-29 Forward Swept Wing Technology Demonstrator traces its development and test path during past years. Brief descriptions of the aircraft and its flight control system provideExpand
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