Author:
LIANG Feng,XIE Zhifeng,XIA Aiguo,ZHOU Ming
Subject
Mechanical Engineering,Aerospace Engineering
Reference39 articles.
1. Silva WA, Vatsa VN, Biedron RT. Development of unsteady aerodynamic and aeroelastic reduced-order models using the FUN3D code. Belgium: Council of European Aerospace Societies; 2009. Report No.: IFASD-2009-030, LF99-8136.
2. Evaluation of linear, inviscid, viscous, and reduced-order modelling aeroelastic solutions of the AGARD 445.6 wing using root locus analysis;Silva;Int J Comput Fluid Dyn,2014
3. Doi H, Alonso J. Fluid/structure coupled aeroelastic computations for transonic flows in turbomachinery. ASME turbo expo2002: Power for land, sea and air; 2002 Jun 3-6; Amsterdam, Netherlands. New York: ASME; 2002. p. 787-794.
4. Coupled fluid-structure flutter analysis of a transonic fan;Zheng;Chin J Aeronaut,2011
5. Platzer MF, Carta FO. AGARD manual on aeroelasticity in axial-flow turbomachines. Volume 2. structural dynamics and aeroelasticity. London: AGARD; 1988. p. 1-250.
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