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Start Over Graduate Program Aerospace Engineering Degree MS Keyword Acoustics Keyword Acoustics

2. Investigation of Noise Reduction Methods on Supersonic Jets Exhausting from Scale Models of Military Style Nozzles

open_access
Open Access
Author:
Powers, Russell
Title:
Investigation of Noise Reduction Methods on Supersonic Jets Exhausting from Scale Models of Military Style Nozzles
Graduate Program:
Aerospace Engineering
Keywords:
Acoustics
Jet Noise
Noise Reduction
Corrugations
Corrugation
Bevel
Beveled
Experiment
Supersonic
Model
Military
Nozzle
File:
Download RWP_MSThesis_2012_vFINAL.pdf
Committee Members:
Dennis K Mc Laughlin, Thesis Advisor/Co-Advisor

3. A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT

open_access
Open Access
Author:
Walsh, Gregory Daniel
Title:
A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT
Graduate Program:
Aerospace Engineering
Keywords:
Acoustics
Coaxial Helicopter
Rotorcraft
Rotorcraft Acoustics
Helicopter
File:
Download Walsh_Thesis.pdf
Committee Members:
Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
Jacob Willem Langelaan, Committee Member
George A Lesieutre, Committee Member

4. Development of an Acoustic Prediction System for Conceptual Design and Analysis of Rotorcraft

open_access
Open Access
Author:
Jaworski, Thomas
Title:
Development of an Acoustic Prediction System for Conceptual Design and Analysis of Rotorcraft
Graduate Program:
Aerospace Engineering
Keywords:
Acoustics
Rotorcraft
Aerospace
BVI
HSI
Noise
File:
Download Thomas_Jaworski_Thesis_2020_Release.pdf
Committee Members:
Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
Amy Ruth Pritchett, Program Head/Chair
Amy Ruth Pritchett, Committee Member
Eric Greenwood, Committee Member

5. Experiments On The Reduced Noise Benefits of A New Configuration of Fluid Shields In Aircraft Engine Exhaust Nozzles

open_access
Open Access
Author:
Scupski, Nick
Title:
Experiments On The Reduced Noise Benefits of A New Configuration of Fluid Shields In Aircraft Engine Exhaust Nozzles
Graduate Program:
Aerospace Engineering
Keywords:
supersonic
jet
noise
dual stream
tactical
aeroacoustics
single-stream;
dual-stream
Acoustics
Aircraft
Fluid Shield
bypass
core
File:
Download MS_thesis-JetNoise_12-14-20_V12_submitted.pdf
Committee Members:
Dennis K Mc Laughlin, Thesis Advisor/Co-Advisor
Philip John Morris, Thesis Advisor/Co-Advisor
Eric Greenwood, Committee Member
Amy Ruth Pritchett, Program Head/Chair