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 language | English |
|---|---|
| Pages (from-to) | 1041-1049 |
| Number of pages | 9 |
| Journal | Journal of Spacecraft and Rockets |
| Volume | 54 |
| Issue number | 5 |
| DOIs | |
| State | Published - 2017 |
| Externally published | Yes |
ASJC Scopus subject areas
- Aerospace Engineering
- Space and Planetary Science
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