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HELICOPTERS
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keywords:(HELICOPTERS)
Model tests on the economy and effectiveness of helicopter propellers
Elements of stability calculation for helicopter
New theories on problem of helicopter design
Aerodynamic analysis of gyroplane rotating-wing system
Wind-tunnel tests of 10-foot-diameter gyroplane rotor
Kay 331 gyroplane (British), all-metal single-seat light rotor plane
Gyroplane -- Its principles and its possibilities
Dynamic stability of helicopter with hinged rotor blades
Contribution to aerodynamics of rotating wing aircraft
Static-thrust tests of six rotor-blade designs on helicopter in Langley full-scale tunnel
Evaluation of induced-velocity field of idealized helicopter rotor
Charts for helicopter-performance estimation
Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades
Effect of rotor-tip speed on helicopter hovering performance and maximum forward speed
Effect of Rotor-Tip Speed on Helicopter Hovering Performance and Maximum Forward Speed
Charts showing relations among primary aerodynamic variables for helicopter-performance estimation
Effect of blade stalling on efficiency of helicopter rotor as measured in flight
Theory of ground vibrations of two-blade helicopter rotor on anisotropic flexible supports
Flight tests of helicopter in autorotation, including comparison with theory
Flight Tests of a Helicopter in Autorotation, Including a Comparison with Theory
Theoretical study of dynamic properties of helicopter-blade systems
Full-scale investigation of blade motion of PV-2 helicopter rotor
NACA-University Conference on Aerodynamics - A Compilation of the Papers Presented
Introduction to physical aspects of helicopter stability
Introduction to physical aspects of helicopter stability
Analytical study of steady vertical descent in autorotation of single-rotor helicopters
Analysis of transition of helicopter from hovering to steady autorotative vertical descent
Theory of helicopter damping in pitch or roll and comparison with flight measurements
Analysis of autorotative performance of helicopter powered by rotor-tip jet units