230.548 People
Tamer, Aykut
Imperial College London
in Cooperation with on an Cooperation-Score of 37%
Topics
- assessment
- helicopter
- weight
- simulation
- vibration
- acceleration
- rotor
- machinery
- flight
- human being
- chemical element
- picture
- flight test
- helicopter pilot
- eye
- psychology
- seat
- aviation safety
- vehicle design
- instrument panel
- retrofitting
- instrument display
- vision disorder
- biodynamics
- emergency
- optimization
- layout
- medical service
- emergency medical service
- hazard mitigation
- performance evaluation
- cockpit
- vehicle occupant
- comfort
- modeling
- head
- health
- regulation
- interface
- gender
- neck
- spinal column
- numerical analysis
- resident
- ride quality
- positioning
- safety
- position fixing
- hospital
- patient
- airframe
- medical equipment
- fuselage
- axis
- screw
- female
- shock absorber
- stability analysis
- aerodynamic
- propeller blade
- momentum
- aerodynamic force
- transfer function
- aeroelasticity
- boundary element method
- harmonic
- show 36 more
Publications
- 2021A numerical study of vibration-induced instrument reading capability degradation in helicopter pilotscitations
- 2020Cabin layout optimization for vibration hazard reduction in helicopter emergency medical servicecitations
- 2019Visual performance evaluation of helicopter pilots in vibrating cockpitcitations
- 2019Biodynamic Modeling Techniques for Rotorcraft Comfort Evaluationcitations
- 2019Evaluation of vibration reduction devices for helicopter ride quality improvementcitations
- 2018Vibration Rating of Medical Helicopters
- 2018Helicopter Kit
- 2015Helicopter ground resonance investigation with dissimilar nonlinear lead-lag dampers
- 2014Helicopter rotor aeroelastic stability evaluation using Lyapunov Exponents
- 2013Rotorcraft aeroelastic stability using robust analysiscitations
- 2013Helicopter vibratory loads and vibrations reduction using higher-harmonic control
- 2013The effect of higher harmonic control on the vibratory loads reduction and aeroelastic stability of a light helicopter
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