Application of Artificial Neural Networks to a Model of a Helicopter Rotor Blade for Damage Identification in Realistic Load Conditions. [PDF]
Ballarin P +5 more
europepmc +1 more source
Coupled rotor-body equations of motion hover flight [PDF]
A set of linearized equations of motion to predict the linearized dynamic response of a single rotor helicopter in a hover trim condition to cyclic pitch control inputs is described.
Curtiss, H. C., Jr. +1 more
core +1 more source
Helicopter noise regulations: An industry perspective [PDF]
A review of helicopter noise measurement programs and noise reduction/economic studies of FAA is given along with a critique of a study which addresses the economic impact of noise reduction on helicopter noise.
Wagner, R. A.
core +1 more source
Rotor performance characteristics from an aeroacoustic helicopter wind-tunnel test program [PDF]
An investigation of helicopter rotor noise at model scale was conducted in the Langley 4 by 7 meter tunnel. The program described was the first of a planned three-phase project whose purpose was to examine the characteristic noise mechanism involved in ...
Elliott, J. W., Hoad, D. R., Orie, N. M.
core +1 more source
Nonlinear controller design for unmanned helicopter flight platform. [PDF]
Ruchun W.
europepmc +1 more source
CFD-enabled sustainable design and manufacturing of cooling fan for unmanned helicopter. [PDF]
Si L +10 more
europepmc +1 more source
Integration of dynamic, aerodynamic, and structural optimization of helicopter rotor blades [PDF]
Summarized here is the first six years of research into the integration of structural, dynamic, and aerodynamic considerations in the design-optimization process for rotor blades.
Peters, David A.
core +1 more source
Micro-Doppler radar deception and camouflage of airborne targets. [PDF]
Kozlov V +6 more
europepmc +1 more source
Rotor aeroelastic stability coupled with helicopter body motion [PDF]
A 5.5-foot-diameter, soft-in-plane, hingeless-rotor system was tested on a gimbal which allowed the helicopter rigid-body pitch and roll motions. Coupled rotor/airframe aeroelastic stability boundaries were explored and the modal damping ratios were ...
Huber, H. B., Miao, W. L.
core +1 more source
Fixed-wing air transport of patients with spinal pathologies: a scoping review of current evidence and future research priorities. [PDF]
Thamilmaran A +9 more
europepmc +1 more source

