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Publication Type : Conference Proceedings
Thematic Areas : Medical Sciences
Publisher : IOP Conference Series: Materials Science and Engineering
Source : IOP Conference Series: Materials Science and Engineering, Institute of Physics Publishing, Volume 225, Number 1 (2017)
Keywords : CFD analysis, Computational fluid dynamics, Computer software, Fluid structure interaction, Flutter boundaries, Post processing, Pressure variations, Simulation studies, solid modelling, Structural frequencies, Supersonic aircraft, Transonic aerodynamics, Vibrational analysis, Wings
Campus : Kochi
School : School of Medicine
Department : General Surgery
Year : 2017
Abstract : This paper presents the application of Computational Fluid Dynamics (CFD) and Fluid Structure Interaction in ANSYS to do vibrational analysis on an aircraft wing in transonic region. A simulation study is conducted on a wing by modelling it in a solid modelling software. Further CFD analysis is performed at different Mach numbers to identify pressure variations at different locations on the wing. Transient structural analysis is carried out to study the variations in displacement of the wing with time. The post processing is done for determining the structural frequency and thereby to establish the flutter boundary in the transonic range. © Published under licence by IOP Publishing Ltd.
Cite this Research Publication : J. S. Chaitanya, Prasad, A., Pradeep, B., Harsha, P. L. N. Sri, S. Shali, and Nagaraja S. R., “Vibrational Characteristics of AGARD 445.6 Wing in Transonic Flow”, IOP Conference Series: Materials Science and Engineering, vol. 225. Institute of Physics Publishing, 2017.