Treffer: Numerical investigation on the aeroelastic instability of a complete aircraft model

Title:
Numerical investigation on the aeroelastic instability of a complete aircraft model
Authors:
KIM, Jong-Yun, KWON, Hyuk-Jun, KIM, Kyung-Seok, LEE, In, HAN, Jae-Hung
Source:
Advanced fluid informationJSME international journal. Series B, fluids and thermal engineering. 48(2):212-217
Publisher Information:
Tokyo: Japan Society of Mechanical Engineers, 2005.
Publication Year:
2005
Physical Description:
print, 8 ref
Original Material:
INIST-CNRS
Subject Terms:
Energy, Énergie, Mechanical engineering, Génie mécanique, Sciences exactes et technologie, Exact sciences and technology, Physique, Physics, Domaines classiques de la physique (y compris les applications), Fundamental areas of phenomenology (including applications), Mécanique des solides, Solid mechanics, Mécanique des structures et des milieux continus, Structural and continuum mechanics, Vibration, onde mécanique, stabilité dynamique (aéroélasticité, contrôle vibration...), Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...), Mécanique des fluides, Fluid dynamics, Méthodes de calcul en mécanique des fluides, Computational methods in fluid dynamics, Sciences appliquees, Applied sciences, Transports terrestres, transports aeriens, transports maritimes, constructions navales, Ground, air and sea transportation, marine construction, Transports et trafic aériens, Air transportation and traffic, Vibrations and mechanical waves, Analyse structurale, Structural analysis, Análisis estructural, Avion combat, Fight aircraft, Avión combate, Aérodynamique, Aerodynamics, Aerodinámica, Aéronef, Aircraft, Aeronave, Aéroélasticité, Aeroelasticity, Aeroelasticidad, Distribution pression, Pressure distribution, Distribución presión, Ecoulement transsonique, Transonic flow, Flujo transónico, Flottement, Flutter, Flotamiento, Génération maille, Mesh generation, Mécanique fluide numérique, Computational fluid dynamics, Mecánica fluido numérica, Simulation numérique, Numerical simulation, Simulación numérica, Computational Fluid Dynamics, Transonic Flow
Document Type:
Konferenz Conference Paper
File Description:
text
Language:
English
Author Affiliations:
Division of Aerospace Eng., KAIST, 373-1 Guseong- Dong, Yuseong-gu, Daejeon 305-701, Korea, Republic of
ISSN:
1340-8054
Access URL:
http://pascal-francis.inist.fr/vibad/index.php?action=search&terms=16954536
Rights:
Copyright 2005 INIST-CNRS
CC BY 4.0
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
Notes:
Building. Public works. Transport. Civil engineering

Physics: fluid mechanics

Physics: solid mechanics
Accession Number:
edscal.16954536
Database:
PASCAL Archive

Weitere Informationen

A nonlinear aeroelastic analysis system has been developed using the coupled numerical techniques of computational fluid dynamics (CFD) and computational structural dynamics (CSD) in the present study and the analysis system has been applied to an actual aircraft design procedure to examine aeroelastic stabilities. An aerodynamic analysis is performed using the transonic small disturbance (TSD) theory for computational efficiency and the results are compared with experimental data. An aeroelastic analysis in the time domain is performed to obtain the flutter boundaries of the aircraft model. Finally, the various effects of launchers and control surfaces are investigated.