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1. Design and Analysis of Rotor Systems with Multiple Trailing Edge Flaps and Resonant Actuators

open_access
Open Access
Author:
Kim, Jun-Sik
Title:
Design and Analysis of Rotor Systems with Multiple Trailing Edge Flaps and Resonant Actuators
Graduate Program:
Aerospace Engineering
Keywords:
helicopter dynamics
vibration reduction
trailing edge flap
piezoelectric
resonant actuator
File:
Download JSKIM-Dissertation-2005-DEC.pdf
Committee Members:
Edward C Smith, Committee Chair/Co-Chair
Kon Well Wang, Committee Chair/Co-Chair
Farhan S Gandhi, Committee Member
Joseph Francis Horn, Committee Member
Mary I Frecker, Committee Member

2. Vibration Reduction of Integrally Bladed Rotors Using Piezoelectric Materials

open_access
Open Access
Author:
Kauffman, Jeffrey Lynn
Title:
Vibration Reduction of Integrally Bladed Rotors Using Piezoelectric Materials
Graduate Program:
Aerospace Engineering
Keywords:
resonance frequency detuning
vibration reduction
turbomachinery damping
piezoelectric device
rotating structures
File:
Download KauffmanPhD.pdf
Committee Members:
George A Lesieutre, Dissertation Advisor/Co-Advisor
George A Lesieutre, Committee Chair/Co-Chair
Stephen Clarke Conlon, Committee Member
Joseph Paul Cusumano, Committee Member
Eric M Mockensturm, Committee Member
Kirsten P Duffy, Special Member
Heath F Hofmann, Special Member

3. Individual Blade Pitch Control (IBC) for Vibration Reduction of Lift-offset Coaxial Rotor Vehicles with Auxiliary Propulsion

open_access
Open Access
Author:
Beyer, Jessica
Title:
Individual Blade Pitch Control (IBC) for Vibration Reduction of Lift-offset Coaxial Rotor Vehicles with Auxiliary Propulsion
Graduate Program:
Aerospace Engineering
Keywords:
individual blade pitch control
compound rotor vehicle
rotorcraft
vibration reduction
XH-59
lift-offset coaxial rotor
File:
Download Thesis_Beyer_Final.pdf
Committee Members:
Amy Pritchett, Program Head/Chair
Edward Smith, Thesis Advisor/Co-Advisor
Sven Schmitz, Thesis Advisor/Co-Advisor
Joseph Francis Horn, Committee Member

4. Fuselage Vibration Reduction of Lift-Offset Coaxial Rotor Vehicles with Auxiliary Propulsion via Individual Blade Pitch Control

open_access
Open Access
Author:
Mawry, Isabella
Title:
Fuselage Vibration Reduction of Lift-Offset Coaxial Rotor Vehicles with Auxiliary Propulsion via Individual Blade Pitch Control
Graduate Program:
Aerospace Engineering
Keywords:
lift-offset
coaxial rotor
compound rotorcraft
rotorcraft
rotor
auxiliary propulsion
fuselage
fuselage vibrations
vibration reduction
active vibration control
File:
Download Mawry_Thesis_-_Final_-_Revised.pdf
Committee Members:
Edward Smith, Thesis Advisor/Co-Advisor
Joseph Francis Horn, Committee Member
Amy Pritchett, Program Head/Chair
Sven Schmitz, Thesis Advisor/Co-Advisor