Aerodynamic characteristics obtained in a rotational flow environment utilizing a rotary balance located in a spin tunnel are presented in plotted form for a 1/6.5 scale, single engine, high wing, general aviation airplane model. The configurations tested included the basic airplane, various wing leading-edge devices, tail designs, and rudder control settings as well as airplane components. Data are presented without analysis for an angle of attack range of 8 deg to 90 deg and clockwise and counter-clockwise rotations covering an omega b/2V range from 0 to 0.85.
Rotary Balance Data for a Typical Single-Engine General Aviation Design for an Angle-of-Attack Range of 8 Deg to 90 Deg. 1: High-Wing Model B
1979
497 pages
Report
Keine Angabe
Englisch