Showing results 1 to 4 of 4
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 |
Effects of multiple structural nonlinearities on limit cycle oscillation of missile control fin Seo, Young-Jin; Lee, Seung-Jun; Bae, Jae-Sung; Lee, In, JOURNAL OF FLUIDS AND STRUCTURES, v.27, no.4, pp.623 - 635, 2011-05 |
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 |
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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