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Analysis of proprotor whirl flutter: Review and update

Author
KUNZ, Donald L1
[1] U.S. Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433-7765, United States
Source

Journal of aircraft. 2005, Vol 42, Num 1, pp 172-178, 7 p ; ref : 21 ref

CODEN
JAIRAM
ISSN
0021-8669
Scientific domain
Aeronautics astronautics; Mechanical engineering; Mechanics acoustics; Transportation
Publisher
American Institute of Aeronautics and Astronautics, Reston, VA
Publication country
United States
Document type
Article
Language
English
Keyword (fr)
Ajustement modèle Angle inclinaison Aéronef Aéroélasticité Basculement Ecrasement Etude expérimentale Flottement aéroélastique Hélice avion Hélicoptère Propulseur Précession Rotor hélicoptère Vibration
Keyword (en)
Model matching Tilt angle Aircraft Aeroelasticity Tilting Crush Experimental study Aeroelastic flutter Airscrew Helicopter Propeller Precession Helicopter rotor Vibration
Keyword (es)
Ajustamiento modelo Angulo inclinación Aeronave Aeroelasticidad Balanceo Aplastamiento Estudio experimental Flameo aeroelástico Hélice avión Helicóptero Propulsor Precesión Rotor helicóptero Vibración
Classification
Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40F Solid mechanics / 001B40F30 Structural and continuum mechanics / 001B40F30M Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)

Discipline
Physics : solid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
16471876

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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