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Start Over Graduate Program Aerospace Engineering Keyword noise

1. Trailing Edge Noise Prediction Using The Nonlinear Disturbance Equations

open_access
Open Access
Author:
Erwin, James Paul
Title:
Trailing Edge Noise Prediction Using The Nonlinear Disturbance Equations
Graduate Program:
Aerospace Engineering
Keywords:
computational
acoustics
prediction
edge
trailing
noise
broadband
cfd
fluid
dynamics
File:
Download Erwin-thesis.pdf
Committee Members:
Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
Philip John Morris, Thesis Advisor/Co-Advisor

2. ENHANCEMENTS AND INVESTIGATION OF CAPABILITIES TO THE LANDING GEAR MODEL AND ACOUSTIC PREDICTION SOFTWARE

open_access
Open Access
Author:
Marotta, Taylor Ries
Title:
ENHANCEMENTS AND INVESTIGATION OF CAPABILITIES TO THE LANDING GEAR MODEL AND ACOUSTIC PREDICTION SOFTWARE
Graduate Program:
Aerospace Engineering
Keywords:
Boeing
airframe noise
LGMAP
landing gear
acoustics
aerospace
trailing edge
aeroacoustics
aircraft
airframe noise
noise
nosie prediction
prediction
Gulfstream
File:
Download TRM_Thesis_Final.pdf
Committee Members:
Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
Philip John Morris, Thesis Advisor/Co-Advisor
Kenneth Steven Brentner, Thesis Advisor/Co-Advisor

3. Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft

open_access
Open Access
Author:
Malovrh, Brendon
Title:
Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft
Graduate Program:
Aerospace Engineering
Keywords:
Blade-Vortex Interaction
BVI
noise
acoustic
helicopter
File:
Download MalovrhDissertationFinal.pdf
Committee Members:
Dr Farhan Gandhi, Dissertation Advisor/Co-Advisor
Dr Farhan Gandhi, Committee Chair/Co-Chair
Kenneth Steven Brentner, Committee Member
Edward A Smith, Committee Member
Christopher Rahn, Committee Member
George A Lesieutre, Committee Member
Kevin James Noonan, Special Member

4. Rotorcraft Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics

open_access
Open Access
Author:
Saetti, Umberto
Title:
Rotorcraft Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics
Graduate Program:
Aerospace Engineering
Keywords:
rotorcraft
noise
control
control systems
dynamic inversion
feedback
flight dynamics
free wake
CHARM
PSUHeloSim
PSUWOPWOP
File:
Download UmbertoSaetti_Thesis_v9.pdf
Committee Members:
Joseph Francis Horn, Thesis Advisor/Co-Advisor
Kenneth Steven Brentner, Committee Member
George A Lesieutre, 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