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Browse "AE-Journal Papers(저널논문)" by Author Bae, JS

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Showing results 1 to 10 of 10

1	Computation of roll moment for projectile with wraparound fins using Euler equation Paek, SK; Park, TS; Bae, JS; Lee, In; Kwon, Jang-Hyuk, JOURNAL OF SPACECRAFT AND ROCKETS, v.36, no.1, pp.53 - 58, 1999
2	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
3	Effects of actuator nonlinearity on aeroelastic characteristics of a control fin Shin, WH; Lee, SJ; Lee, In; Bae, JS, JOURNAL OF FLUIDS AND STRUCTURES, v.23, no.7, pp.1093 - 1105, 2007-10
4	Effects of structural nonlinearity on subsonic aeroelastic characteristics of an aircraft wing with control surface Bae, JS; Inman, DJ; Lee, In, JOURNAL OF FLUIDS AND STRUCTURES, v.19, no.6, pp.747 - 763, 2004-07
5	Extension of flutter prediction parameter for multimode flutter systems Bae, JS; Kim, JY; Lee, In; Matsuzaki, Y; Inman, DJ, JOURNAL OF AIRCRAFT, v.42, no.1, pp.285 - 288, 2005-01
6	Flutter analysis of a wraparound fin projectile considering rolling motion Paek, SK; Bae, JS; Lee, In, JOURNAL OF SPACECRAFT AND ROCKETS, v.39, no.1, pp.66 - 72, 2002
7	Flutter Characteristics of a Morphing Flight Vehicle with Varying Inboard and Outboard Folding Angles Shrestha, Pratik; Jeong, Min-Soo; Lee, In; Bae, JS; Koo, KN, International Journal of Aeronautical and Space Sciences, v.14, no.2, pp.133 - 139, 2013-06
8	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
9	Linear and nonlinear aeroelastic analysis of fighter-type wing with control surface Bae, JS; Yang, SM; Lee, In, JOURNAL OF AIRCRAFT, v.39, no.4, pp.697 - 708, 2002
10	Nonlinear aeroelastic analysis for a control fin with an actuator Shin, WH; Lee, In; Shin, YS; Bae, JS, JOURNAL OF AIRCRAFT, v.44, no.2, pp.597 - 605, 2007-03

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