The effects of rotation in the areas of vibrations, dynamic stability, optimization, and aeroelasticity were studied. The governing equations of motion for the study of vibration and dynamic stability of a rapidly rotating deformable body were developed starting from the nonlinear theory of elasticity. Some common features such as the limitations of the classical theory of elasticity, the choice of axis system, the property of self-adjointness, the phenomenon of frequency splitting, shortcomings of stability methods as applied to gyroscopic systems, and the effect of internal and external damping on stability in gyroscopic systems are identified and discussed, and are then applied to three specific problems
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
Oscillations of a purely gyrostatic system with two degrees of freedom are constituted by elliptic p...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
The structural dynamics of a cantilever turbomachine blade mounted on a spinning and precessing roto...
This thesis provides a vibration analysis of a rotating cantilever beam with an independently rotati...
An aeroelastic investigation of horizontal axis wind turbines is described. The study is divided int...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
The paper addresses the in-plane free vibration analysis of rotating beams using an exact dynamic st...
The gyroplane represents the first successful rotorcraft design and it paved the way for the develop...
An overview of the methods and concepts developed to enhance and predict structural dynamic characte...
This paper investigates the inertial force effect on nonlinear aeroelasticity of flexible wing aircr...
Vibrational stability of large flexible structurally damped spacecraft carrying internal angular mom...
After a short review of dynamic phenomena, identification and analyses concerning the aerospace stru...
An an overview and discussion of those aspects of airframe structural dynamics that have a strong in...
This chapter is focused on a specific type of dynamic aeroelastic stability phenomenon—whirl flutter...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
Oscillations of a purely gyrostatic system with two degrees of freedom are constituted by elliptic p...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
The structural dynamics of a cantilever turbomachine blade mounted on a spinning and precessing roto...
This thesis provides a vibration analysis of a rotating cantilever beam with an independently rotati...
An aeroelastic investigation of horizontal axis wind turbines is described. The study is divided int...
Theoretical and experimental developments in the aeroelastic and aeromechanical stability of helicop...
The paper addresses the in-plane free vibration analysis of rotating beams using an exact dynamic st...
The gyroplane represents the first successful rotorcraft design and it paved the way for the develop...
An overview of the methods and concepts developed to enhance and predict structural dynamic characte...
This paper investigates the inertial force effect on nonlinear aeroelasticity of flexible wing aircr...
Vibrational stability of large flexible structurally damped spacecraft carrying internal angular mom...
After a short review of dynamic phenomena, identification and analyses concerning the aerospace stru...
An an overview and discussion of those aspects of airframe structural dynamics that have a strong in...
This chapter is focused on a specific type of dynamic aeroelastic stability phenomenon—whirl flutter...
The present investigation may be considered as preliminary to the study of automatic stabilizers. We...
Oscillations of a purely gyrostatic system with two degrees of freedom are constituted by elliptic p...
A review is presented of the work done by other investigators on the effects of inertia couplings in...