Intergrid transformation for aircraft aeroelastic simulations

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Badcock, K J ^a   Moosa Rampurawala, A ^a   Richards, B E ^a  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROELASTICITY; BLENDING; FUSELAGES; STRUCTURAL DYNAMICS; VARIABLE SPEED TRANSMISSIONS;

AERO-ELASTIC SIMULATIONS; AEROELASTIC COMPUTATIONS; COMPONENT INTERFACES; LEVEL TRANSFORMATION; STRUCTURAL COMPONENT; STRUCTURAL DYNAMICS MODELS; TRANSFORMATION METHODOLOGIES; TRANSFORMATION SCHEME;

FIGHTER AIRCRAFT;

EID: 85067322473     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3512     Document Type: Conference Paper

References (7)

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3. Goura, G.S.L., Time Marching Analysis of Flutter Using Computational Fluid Dynamics, PhD thesis, University of Glasgow, 2001.
4. X. Z. Huang and S. Zan, Wing and Fin Buffet on the Standard Dynamic Model, IAR/NRC Canada, RTO Report,RTO-TR-26 AC/323(AVT)TP/19
5. Chen, P.C. and Jadic, I., Interfacing Fluid and Structural Models via Innovative Structural Boundary Element Method, AIAA Journal, vol 36, number 2, pp 282-287, 1998.
6. Melville, R., Nonlinear Simulation of Aeroelastic Instability, AIAA 2001-0570, 2001.
7. C. Farhat, P. Geuzaine and G. Brown, Application of Three Field Nonlinear Fluid-structure Formulation to the Prediction of the Aeroelastic Parameters of an F-16 Fighter, Computers and Fluids, vol 32, pp 3-29, 2003.