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Results 1-3 of 3 (Search time: 0.009 seconds).

NO Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date)
1
Dynamic model establishment of a deployable missile control fin with nonlinear hinge

Kim, DK; Bae, JS; Lee, In; Han, Jae-Hung, JOURNAL OF SPACECRAFT AND ROCKETS, v.42, no.1, pp.66 - 77, 2005-01

2
Frequency and time domain flutter computations of a wing with oscillating control surface including shock interference effects

Kwon, HJ; Kim, DH; Lee, In, AEROSPACE SCIENCE AND TECHNOLOGY, v.8, no.6, pp.519 - 532, 2004-09

3
Limit cycle oscillation of missile control fin with structural non-linearity

Bae, JS; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.269, no.3-5, pp.669 - 687, 2004-01

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