Aeroelastic analysis of a wing with freeplay in the subsonic/transonic regions

An efficient aeroelastic analysis where both aerodynamic and structural nonlinearities are considered is performed. The analysis is based on the computational fluid dynamics (CFD) and computational structural-dynamics (CSD) techniques in the time domain. Moving shock wave on the lifting surface, which is the aerodynamic nonlinearity in this study, is taken into account using the transonic small disturbance (TSD) equation. Freeplay, which is the local structural nonlinearity, is,considered in the modal coordinate using fictitious mass method. The aeroelastic response results of a wing with freeplay are presented in the subsonic and transonic regions. Also, the effects of an airfoil thickness on the aeroelastic responses are investigated.
Publisher
JAPAN SOC MECHANICAL ENGINEERS
Issue Date
2005-05
Language
ENG
Keywords

CONTROL SURFACE; NONLINEARITY

Citation

JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING, v.48, no.2, pp.208 - 211

ISSN
1340-8054
URI
http://hdl.handle.net/10203/6610
Appears in Collection
AE-Journal Papers(저널논문)
  • Hit : 559
  • Download : 0
  • Cited 0 times in thomson ci
This item is cited by other documents in WoS
⊙ Detail Information in WoSⓡClick to seewebofscience_button
⊙ Cited 1 items in WoSClick to see citing articles inrecords_button

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0