Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Yair Guy"'
Publikováno v:
Flow, Turbulence and Combustion. 78:429-443
An active flow control experiment was conducted on a cropped NACA 0018 airfoil to study 3D effects and maneuverability aspects made possible by a segmented actuation system installed in the airfoil. The 14 piezo-fluidic actuators were installed at th
Publikováno v:
2nd AIAA Flow Control Conference.
An active flow control experiment was conducted on a cropped NACA 0018 airfoil to study 3D effects and maneuverability aspects made possible by a segmented actuation system installed in the airfoil. The 14 piezo-fluidic actuators were installed at th
Publikováno v:
39th Aerospace Sciences Meeting and Exhibit.
Publikováno v:
39th Aerospace Sciences Meeting and Exhibit.
Detailed measurements of the velocity field in a synthetic jet emanating from a piezoelectric actuator are conducted. A two-dimensional, steady, turbulent jet is synthesized from the ambient air by periodically deflecting a piezoelectric-driven disk,
Publikováno v:
18th Applied Aerodynamics Conference.
An experimental investigation is conducted to study the effects of deflectable flaps on the aerodynamic characteristics of a TCP-sweep delta wing. Leading edge upper-surface flaps and lower-surface flaps are investigated. The flaps are deflected down
Publikováno v:
Fluids 2000 Conference and Exhibit.
Publikováno v:
38th Aerospace Sciences Meeting and Exhibit.
The efficacy of active flow control in delaying vortex breakdown and enhancing the lift characteristics of a 70°-sweep delta wing is experimentally investigated in a low-speed wind tunnel at the USAF Academy. Periodic blowing and suction with zero n
Publikováno v:
38th Aerospace Sciences Meeting and Exhibit.
Publikováno v:
38th Aerospace Sciences Meeting and Exhibit.
An experimental investigation is conducted to study the effects of canard shape on the center of pressure location of a generic canard-wing-body configuration. The aspect ratio, sweep angle and taper ratio of canards having constant planform area are
Publikováno v:
38th Aerospace Sciences Meeting and Exhibit.
The mechanism by which periodic blowing and suction at the leading edge improves lift and stall angle of a 70° sweep delta wing is investigated in water tunnel experiments using PIV measurements. Periodic sinusoidal blowing and suction with zero net