Experimental transition data files from a wind tunnel test on a 1/4.622 Froude scale hingeless rotor, tilt rotor model are reported. Diverse data are presented; variables include parametric force, moment and blade fatigue loads, hovering to low speed flight, aircraft attitude, rotor control inputs, wing flap deflection, thrust load, and rotor RPM.
Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 2
1976
679 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Rigid rotors , Tilt rotor research aircraft program , Scale models , Wind tunnel tests , Aerodynamic characteristics , Dynamic models , Froude number , Hovering , Low speed , Nasa programs , Tables (Data) , Aerodynamic forces , Airspeed , Attitude (Inclination) , Rotor speed , Stability derivatives , Stress concentration , Thrust loads , Wing flaps , Rotor blades(Rotary wings)