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Start Over Degree MS Committee Member Amy Pritchett Keyword rotorcraft

1. Benefits of Parallel Hybrid Electric Propulsion for Aircraft and Rotorcraft

open_access
Open Access
Author:
Decerio, Dalton
Title:
Benefits of Parallel Hybrid Electric Propulsion for Aircraft and Rotorcraft
Graduate Program:
Aerospace Engineering (MS)
Keywords:
hybrid
electric
aircraft
rotorcraft
conceptual design
optimization
propulsion
File:
Download Decerio_Thesis_Final.pdf
Committee Members:
Amy Pritchett, Program Head/Chair
David K Hall, Thesis Advisor/Co-Advisor
Karen Ann Thole, Committee Member
Edward Smith, Committee Member

2. Structural Design of a Rigid Coaxial Rotor System for Wind Tunnel Testing

open_access
Open Access
Author:
Purzak, Jake
Title:
Structural Design of a Rigid Coaxial Rotor System for Wind Tunnel Testing
Graduate Program:
Aerospace Engineering (MS)
Keywords:
rotorcraft
coaxial
structural design
structural analysis
dragonfly
rotor design
rigid rotor
coaxial test system
wind tunnel test system
File:
Download PurzakJake_MSThesis.pdf
Committee Members:
Amy Pritchett, Program Head/Chair
Jose Palacios, Thesis Advisor/Co-Advisor
Jacob Willem Langelaan, Committee Member
Edward Smith, Committee Member

3. Helicopter Noise Modeling With Varying Fidelity Prediction Systems

open_access
Open Access
Author:
Weist, Lauren
Title:
Helicopter Noise Modeling With Varying Fidelity Prediction Systems
Graduate Program:
Aerospace Engineering (MS)
Keywords:
Acoustics
rotorcraft
noise prediction systems
helicopter noise
File:
Download LWeist_MastersThesis_07182022.pdf
Committee Members:
Amy Pritchett, Program Head/Chair
Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
Eric Greenwood, Committee Member
Joseph Francis Horn, Committee Member

4. 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 (MS)
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