Phuriwat Anusonti-Inthra, Ph.D.
Affiliations: | 2002 | Pennsylvania State University, State College, PA, United States |
Area:
Aerospace EngineeringGoogle:
"Phuriwat Anusonti-Inthra"Parents
Sign in to add mentorFarhan S. Gandhi | grad student | 2002 | Penn State | |
(Semi -active control of helicopter vibration using controllable stiffness and damping devices.) |
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Publications
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Misiorowski M, Gandhi F, Anusonti-Inthra P. (2020) Computational Analysis of Rotor-Blown-Wing for Electric Rotorcraft Applications Aiaa Journal. 58: 2921-2932 |
Gandhi F, Anusonti-Inthra P. (2008) Skin design studies for variable camber morphing airfoils Smart Materials and Structures. 17 |
Anusonti-Inthra P, Sarjeant R, Frecker M, et al. (2005) Design of a Comfortable Rotor Airfoil Using Distributed Piezoelectric Actuators Aiaa Journal. 43: 1684-1695 |
Anusonti-Inthra P, Gandhi F. (2004) Cyclic modulation of semi-active controllable dampers for tonal vibration isolation Journal of Sound and Vibration. 275: 107-126 |
Gandhi F, Anusonti-Inthra P. (2003) Adaptive control of semiactive variable stiffness devices for narrow-band disturbance rejection Journal of Intelligent Material Systems and Structures. 14: 191-201 |
Anusonti-Inthra P, Gandhi F, Miller L. (2003) Reduction of helicopter vibration through cyclic control of variable orifice dampers Aeronautical Journal. 107: 657-672 |
Anusonti-Inthra P, Gandhi F, Miller L. (2003) Reduction of helicopter vibration through cyclic control of variable orifice dampers Aeronautical Journal. 107: 657-672 |
Gandhi F, Anusonti-Inthra P. (2002) Helicopter vibration reduction using discrete controllable-stiffness devices at the rotor hub Journal of Aircraft. 39: 668-677 |
Gandhi F, Anusonti-Inthra P. (2001) Helicopter Vibration Reduction Using Discrete Controllable-Stiffness Devices at the Rotor Hub Journal of Aircraft. 39: 668-677 |
Anusonti-Inthra P, Gandhi F. (2001) Optimal control of helicopter vibration through cyclic variations in blade root stiffness Smart Materials and Structures. 10: 86-95 |