Add to ORKGThe effect of boundary layer control blowing on the download of a wing in the wake of a hovering rotor was measured in a small scale experiment. The objective was to evaluate the potential of boundary layer control blowing for reducing tilt rotor download. Variations were made in rotor thrust coefficient, blowing pressure ratio, and blowing slot height. The effect of these parameter variations on the wing download and wing surface pressures is presented. The boundary layer control blowing caused reductions in the wing download of 25 to 55 percent
West Virginia University has developed a circulation controlled model of the V-22 wing to reduce the...
Application of circulation to rotary wing systems is a new development. Efforts to determine the nea...
Results are reported on the modification of the wing download due to a rotor wake interaction, using...
The aerodynamic characteristics of airfoils with several flap configurations were studied theoretica...
Wind tunnel measurements of boundary layer and wake velocity profiles and surface static pressure di...
A full-scale wind-tunnel test was conducted of two boundary-layer-control applications to a 44-foot ...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
The wing employed in this investigation had a 67-percent-chord slotted flap in combination with a 33...
Circulation control is a high-lift methodology that can be used on the wing of an aircraft. This tec...
An experimental and theoretical investigation of rotor/wing aerodynamic interactions in hover is des...
Pressure distributions and photographs of oil flow patterns are presented for a circulation control ...
Lower surface blowing (LSB) is investigated as an alternative to the variable blade pitch requiremen...
The hovering performance and the lifting capability of tiltrotor aircraft are strongly affected by t...
Interactions between the rotors and wing of a rotary wing aircraft in hover have a significant detri...
The reduction of the aerodynamic load that acts on a generic rotorcraft fuselage by the application ...
West Virginia University has developed a circulation controlled model of the V-22 wing to reduce the...
Application of circulation to rotary wing systems is a new development. Efforts to determine the nea...
Results are reported on the modification of the wing download due to a rotor wake interaction, using...
The aerodynamic characteristics of airfoils with several flap configurations were studied theoretica...
Wind tunnel measurements of boundary layer and wake velocity profiles and surface static pressure di...
A full-scale wind-tunnel test was conducted of two boundary-layer-control applications to a 44-foot ...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
The wing employed in this investigation had a 67-percent-chord slotted flap in combination with a 33...
Circulation control is a high-lift methodology that can be used on the wing of an aircraft. This tec...
An experimental and theoretical investigation of rotor/wing aerodynamic interactions in hover is des...
Pressure distributions and photographs of oil flow patterns are presented for a circulation control ...
Lower surface blowing (LSB) is investigated as an alternative to the variable blade pitch requiremen...
The hovering performance and the lifting capability of tiltrotor aircraft are strongly affected by t...
Interactions between the rotors and wing of a rotary wing aircraft in hover have a significant detri...
The reduction of the aerodynamic load that acts on a generic rotorcraft fuselage by the application ...
West Virginia University has developed a circulation controlled model of the V-22 wing to reduce the...
Application of circulation to rotary wing systems is a new development. Efforts to determine the nea...
Results are reported on the modification of the wing download due to a rotor wake interaction, using...