7 Matching Results

Search Results

Advanced search parameters have been applied.

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22: lateral-directional characteristics of a triangular wing and canard

Description: Report presenting the results of an investigation of the static lateral-directional stability characteristics of a canard airplane configuration without analysis for a range of Mach numbers. Data are presented for various combinations of the canard, body, wing, and vertical tail. Data were obtained at a variety of angles of attack, sideslip angles, and canard angles.
Date: March 4, 1958
Creator: Peterson, Victor L. & Menees, Gene P.
Partner: UNT Libraries Government Documents Department

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22: triangular wing and canard on an extended body

Description: Report presenting an investigation of the static stability and control characteristics of a canard airplane configuration without analysis for a range of Mach numbers from 0.70 to 2.22. This configuration consisted of a triangular wing and triangular canard, a low aspect ratio vertical tail, and a modified Sears-Haack body. Data are presented for various combinations of the body, canard, wing, and vertical tail at severla angles of sideslip, angles of attack, and canard deflection angles.
Date: February 10, 1958
Creator: Boyd, John W. & Peterson, Victor L.
Partner: UNT Libraries Government Documents Department

Static stability and control characteristics of a triangular wing and canard configuration at Mach numbers form 2.58 to 3.53

Description: Report presenting the results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration without analysis over a range of Mach numbers. Data are presented for various combinations of the body, canard, wings, and vertical tail at 0 and 5 degrees of sideslip over a range of angles of attack and canard deflection angles.
Date: May 13, 1958
Creator: Hedstrom, C. Ernest; Blackaby, James R. & Peterson, Victor L.
Partner: UNT Libraries Government Documents Department

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22: longitudinal characteristics of an unswept wing and canard

Description: Report presenting the results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration without analysis for a range of Mach numbers. The configuration had an unswept wing, an unswept canard, a low aspect ratio vertical tail, and a Sears-Haack body. Data are presented for various combinations of the canard, wing, and vertical tail for a range of angles of attack and canard deflection angles.
Date: February 17, 1958
Creator: Peterson, Victor L. & Boyd, John W.
Partner: UNT Libraries Government Documents Department

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22 : longitudinal characteristics of a triangular wing and canard

Description: Report presenting the results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration without analysis for a range of Mach numbers. Data are presented for a variety of angles of attack and canard angles.
Date: January 22, 1958
Creator: Boyd, John W. & Peterson, Victor L.
Partner: UNT Libraries Government Documents Department

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22longitudinal characteristics of a triangular wing and unswept canard

Description: Report presenting the results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration without analysis for a range of Mach numbers from 0.70 to 2.22. The configuration consisted of a triangular wing, an unswept canard, a low aspect ratio vertical tail, and a Sears-Haack body. Data are presented for various combinations of the canard, wing, and vertical tail for a range of angles of attack and canard deflection angles.
Date: February 17, 1958
Creator: Peterson, Victor L. & Menees, Gene P.
Partner: UNT Libraries Government Documents Department

Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0

Description: Report presenting the results of an investigation to determine the effects of conical camber on the lift, drag, and pitching-moment characteristics of a wing-body combination with a triangular wing of aspect ratio 3.0. At subsonic speeds, the use of camber was found to result in substantial reductions in drag coefficients at lift coefficients above 0.15.
Date: February 19, 1957
Creator: Peterson, Victor L. & Boyd, John W.
Partner: UNT Libraries Government Documents Department