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Results 1-8 of 8 (Search time: 0.005 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, Inresearcher; Han, Jae-Hungresearcher, JOURNAL OF SPACECRAFT AND ROCKETS, v.42, no.1, pp.66 - 77, 2005-01

2
Extension of flutter prediction parameter for multimode flutter systems

Bae, JS; Kim, JY; Lee, Inresearcher; Matsuzaki, Y; Inman, DJ, JOURNAL OF AIRCRAFT, v.42, no.1, pp.285 - 288, 2005-01

3
Linear and nonlinear aeroelastic analysis of fighter-type wing with control surface

Bae, JS; Yang, SM; Lee, Inresearcher, JOURNAL OF AIRCRAFT, v.39, no.4, pp.697 - 708, 2002

4
Limit cycle oscillation of missile control fin with structural non-linearity

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

5
Nonlinear aeroelastic analysis for a control fin with an actuator

Shin, WH; Lee, Inresearcher; Shin, YS; Bae, JS, JOURNAL OF AIRCRAFT, v.44, no.2, pp.597 - 605, 2007-03

6
Effects of actuator nonlinearity on aeroelastic characteristics of a control fin

Shin, WH; Lee, SJ; Lee, Inresearcher; Bae, JS, JOURNAL OF FLUIDS AND STRUCTURES, v.23, no.7, pp.1093 - 1105, 2007-10

7
Effects of structural nonlinearity on subsonic aeroelastic characteristics of an aircraft wing with control surface

Bae, JS; Inman, DJ; Lee, Inresearcher, JOURNAL OF FLUIDS AND STRUCTURES, v.19, no.6, pp.747 - 763, 2004-07

8
Flutter analysis of a wraparound fin projectile considering rolling motion

Paek, SK; Bae, JS; Lee, Inresearcher, JOURNAL OF SPACECRAFT AND ROCKETS, v.39, no.1, pp.66 - 72, 2002

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