High-Speed Helicopter Impulsive Noise

Maximum likelihood identification and optimal input design for identifying aircraft stability and control derivatives

D. E. Stepner, R.К. Mehra · NASA Technical Reports Server (NASA) · 1973 · 45 citations

Engineering, Aerospace Engineering, Systems Engineering +17

Hingeless rotor frequency response with unsteady inflow

David A. Peters · NASA Technical Reports Server (NASA) · 1974 · 37 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +17

Hingeless Helicopter Rotor Response with Nonuniform Inflow and Elastic Blade Bending

Robert A. Ormiston, David A. Peters · Journal of Aircraft · 1972 · 34 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

An Unsteady Wake Model for a Hingeless Rotor

Stephen T. Crews, Kurt Hohenemser, Robert A. Ormiston · Journal of Aircraft · 1973 · 22 citations

Engineering, Mechanical Engineering, Aerodynamics +16

Technical Notes: Application of Simplified Inflow Models to Rotorcraft Dynamic Analysis

Robert A. Ormiston · Journal of the American Helicopter Society · 1976 · 22 citations

Engineering, Aerospace Engineering, Aerodynamics +15