Experimental cruise flight 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, cruising flight speed, aircraft attitude, rotor control input, wing flap deflection, thrust load, and rotor RPM.
Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 4
1976
568 pages
Report
No indication
English
Aerodynamics , Aircraft , Rigid rotors , Tilt rotor research aircraft program , Scale models , Wind tunnel tests , Aerodynamic characteristics , Cruising flight , Dynamic models , Froude number , Nasa programs , Tables (Data) , Aerodynamic forces , Airspeed , Attitude (Inclination) , Rotor speed , Stability derivatives , Stress concentration , Thrust loads , Wing flaps , Rotor blades(Rotary wings)