The model was a full-scale mockup of a light single-engine high-wing monoplane. Tests were made over an angle-of-attack range of -4 deg to 24 deg and over a sideslip range of plus or minus 8 deg at thrust coefficients of 0, 0.14, and 0.30. Control effectiveness and hinge moments were taken on the aileron, elevator, and rudder for a full range of deflections. Downwash measurements at the tail were obtained for the range of thrust coefficient and flap deflection. (Author)
Wind Tunnel Investigation of Static Longitudinal and Lateral Characteristics of a Full Scale Mockup of a Light Single Engine High Wing Airplane
1973
158 pages
Report
Keine Angabe
Englisch