1. Bae, J.S., 2002. Aeroelastic characteristics and flutter suppression considering structural nonlinearity. Ph.D Dissertation, Department of Aerospace Engineering. Korea Advanced Institute of Science Technology.
2. Limit cycle oscillation of missile control fin with structural nonlinearity;Bae;Journal of Sound and Vibration,2004
3. Linear and nonlinear aeroelastic analysis of fighter-type wing with control surface;Bae;Journal of Aircraft,2002
4. Nonlinear aeroelastic analysis of deployable missile control fin;Bae;Journal of Spacecraft and Rockets,2004
5. Nonlinear behavior of a typical airfoil section with control surface free-play;Conner;Journal of Fluids and Structures,1997