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Nonlinear aeroelastic analysis of a rolling wraparound fin

  • Hyoung Jin Na
  • , Chun Gon Kim
  • , In Lee
  • , Jung Young Kim
  • , Su Bin Bae

Research output: Contribution to journal › Article › peer-review

6 Scopus citations

Abstract

The nonlinear aeroelastic characteristics of a rolling wraparound fin with freeplay nonlinearity are investigated. The aerodynamic forces are computed by solving the Euler equations in a body-fixed rotating coordinate frame. The nonlinear static and normal mode analyses for a rotating wraparound fin are performed usingMSCNastran. The V-g method, the traditional incremental damping approach to compute the flutter velocity, is used for aeroelastic analysis in the frequency domain, and the results are shown to compare with the time-history responses obtained by integration of the equations of motion using minimum state approximation time-domain aerodynamics. The effects of the freeplay nonlinearity and rolling motion of a wraparound fin on aeroelastic characteristics are investigated.

Original languageEnglish
Pages (from-to)1041-1049
Number of pages9
JournalJournal of Spacecraft and Rockets
Volume54
Issue number5
DOIs
StatePublished - 2017
Externally publishedYes

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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