467.600 PEOPLE
| People | Locations | Statistics |
|---|---|---|
| Serhiienko, Serhii |
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| Schmalz, Ulrike |
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| Oliveira, Marisa |
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| Ribeiro Pereira, Maria Teresa |
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| Bellér, Gábor |
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| Araujo, M. |
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| Frey, Michael | Karlsruhe |
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| Coutinho-Rodrigues, João | Coimbra |
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| Wouters, Christian Guillaume Louise | Aachen |
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| Kessel, Paul J. Van Van |
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| Árpád, István |
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| Fontul, Simona |
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| Kocsis, Dénes |
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| Cigada, Alfredo | Milan |
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| Oort, Neils Van | Delft |
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| Agárdi, Anita | Miskolc |
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| Andrews, Gordon E. |
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| Sousa, Nuno |
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| Witlox, Frank Jacomina Albert | Ghent |
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| Dobruszkes, Frederic |
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| Kiss, Judit T. |
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| Hadachi, Amnir | Saint-Étienne-du-Rouvray |
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| Hamilton, Carl J. | Kunovice |
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| Misiura, Serhii |
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| Schimpf, Marina |
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Bernardini, Giovanni
in Cooperation with on an Cooperation-Score of 37%
Topics
- assessment
- data
- helicopter
- noise
- forecasting
- chemical element
- validation
- database
- rotor
- experiment
- tunnel
- wind tunnel
- wind
- fuselage
- equation
- scattering
- noise source
- boundary element method
- acoustic scattering
- algorithm
- weight
- simulation
- flight
- monitoring
- health
- stiffness
- propeller blade
- structural health monitoring
- strain gage
- strain measurement
- design
- contaminant
- behavior
- vibration
- reconstruction
- deflection
- flight control system
- rotor blade
- acoustic emission
- aerodynamic
- aerospace engineering
- aeroelasticity
- hemisphere
- theory
- photogrammetry
- particle beam
- control device
- variable
- region
- constraint
- bottleneck
- law
- hub
- estimate
- picture
- modeling
- noise control
- vortex
- attention
- estimating
- optimisation
- pressure
- effective sound pressure
- steady state
- feeding stuff
- machinery
- human being
- interface
- avionics
- system of measurement
- perturbation
- city
- density
- trajectory
- environmental impact
- airport
- fuel
- hospital
- information system
- rotary wing aircraft
- population density
- software package
- harmonic
- airplane
- vibration control
- pylon
- aircraft
- aircraft cabin
- skin
- actuating system
- actuator
- turboprop aircraft
- show 62 more
Publications
- 2021EVALUATION OF ACOUSTIC SHIELDING EFFECTS FROM A GENERIC GARTEUR HELICOPTER CONFIGURATION
- 2019In-flight health monitoring of helicopter blades via differential analysiscitations
- 2019Conceptual All-Electric Retrofit of Helicopters: Review, Technological Outlook, and a Sample Designcitations
- 2018Rotor blade shape reconstruction from strain measurementscitations
- 2016Numerical characterization of helicopter noise hemispherescitations
- 2016Structural Characterization of Rotor Blades Through Photogrammetrycitations
- 2015Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devicescitations
- 2015Photogrammetric Detection Technique for Rotor Blades Structural Characterizationcitations
- 2014Parallel blade-vortex interaction modelling for helicopter rotor noise control synthesiscitations
- 2014Simulation of Helicopter Noise in Maneuvering Flight
- 2014MANOEUVRES - An Effort Towards Quieter, Reliable Rotorcraft Terminal Procedures
- 2012Optimal design and acoustic assessment of swept-tip helicopter rotor blades
- 2012Optimization of Rotorcraft Noise Abatement Trajectories
- 2012Tiltrotor Wing-Root Vibratory Loads Reduction Through Higher Harmonic Control Actuationcitations
- 2011Aircraft cabin tonal noise alleviation through fuselage skin embedded piezoelectric actuatorscitations
- 2010Optimal design of tonal noise control inside smart-stiffened fuselages of turboprop aircraft
- 2008Combined action of variable-stiffness devices and trailing-edge flap for helicopter hub loads reduction
- 2007Novel boundary integral formulation for blade-vortex interaction aerodynamics of helicopter rotorscitations
- 2007Sound scattered by a helicopter fuselage in descent flight condition
- 2006Aeroelastic response of helicopter rotors using a 3D unsteady aerodynamic solvercitations
- 2006Multi-disciplinary optimization for the conceptual design of innovative aircraft configurations
- 2005A novel potential-flow boundary integral formulation for helicopter rotors in BVI conditionscitations
- 2003A boundary element method for the aerodynamic analysis of aircraft in arbitrary motionscitations
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