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Start Over Graduate Program Aerospace Engineering Degree MS Committee Member Philip John Morris

1. A Cartesian Immersed Boundary Method Study of Damaged and Undamaged Airfoil Performance

open_access
Open Access
Author:
Goss, Adam
Title:
A Cartesian Immersed Boundary Method Study of Damaged and Undamaged Airfoil Performance
Graduate Program:
Aerospace Engineering
Keywords:
Performance
Damaged Airfoil
Survivability
Immersed Boundary
Cartesian
Computational Aerodynamics
File:
Download GossMSThesis.pdf
Committee Members:
Philip John Morris, Thesis Advisor/Co-Advisor
Philip John Morris, Thesis Advisor/Co-Advisor

2. Numerical Simulations of Two-Dimensional Laminar Flow Over Bluff Bodies Using the Immersed Boundary Method with Cartesian Grids

open_access
Open Access
Author:
Stergiou, Jonathan Chris
Title:
Numerical Simulations of Two-Dimensional Laminar Flow Over Bluff Bodies Using the Immersed Boundary Method with Cartesian Grids
Graduate Program:
Aerospace Engineering
Keywords:
fluid
computational
cylinder
immersed boundary
cfd
dynamics
bluff body
File:
Download JonathanStergiou_DissertationMS.pdf
Committee Members:
Philip John Morris, Thesis Advisor/Co-Advisor
Sue Ellen Haupt, Thesis Advisor/Co-Advisor

3. 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

5. Development of a Trailing-Edge Noise Prediction Method using the Non-Linear Disturbance Equations

open_access
Open Access
Author:
Christiansen, Monica Danielle
Title:
Development of a Trailing-Edge Noise Prediction Method using the Non-Linear Disturbance Equations
Graduate Program:
Aerospace Engineering
Keywords:
trailing edge noise
computational aeroacoustics
non-linear disturbance equations
wind turbine noise
File:
Download PSUThesisChristiansenFINAL072914.pdf
Committee Members:
Philip John Morris, Thesis Advisor/Co-Advisor
Kenneth Steven Brentner, Thesis Advisor/Co-Advisor

9. 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

11. Determining Optimum Conditions For Dual Time Stepping Using Convergence Acceleration Techniques in Computational Aeroacoustics

open_access
Open Access
Author:
Rout, Vikram
Title:
Determining Optimum Conditions For Dual Time Stepping Using Convergence Acceleration Techniques in Computational Aeroacoustics
Graduate Program:
Aerospace Engineering
Keywords:
DRP
Dual Time Stepping
Implicit Residual Smoothing
Multigrid
File:
Download Thesis_Vikram_Rout_Final.pdf
Committee Members:
Philip John Morris, Thesis Advisor/Co-Advisor

13. simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations

open_access
Open Access
Author:
Kapusta, Matthew Joseph
Title:
simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations
Graduate Program:
Aerospace Engineering
Keywords:
jet noise reduction
fluidic inserts
supersonic nozzle
supersonic jet flow field
fluid injection
File:
Download Kapusta_MS.pdf
Committee Members:
Philip John Morris, Thesis Advisor/Co-Advisor

15. Mechanical Properties and Deformation Behaviors of Nanoporous Anodic Aluminum Oxide Membrane

open_access
Open Access
Author:
Dai, Jingyao
Title:
Mechanical Properties and Deformation Behaviors of Nanoporous Anodic Aluminum Oxide Membrane
Graduate Program:
Aerospace Engineering
Keywords:
Ceramics
Fracture
Nanoporous
Anodic Aluminum Oxide
Nanoindentation
File:
Download JingyaoDai-MSThesis.pdf
Committee Members:
Namiko Yamamoto, Thesis Advisor/Co-Advisor
Jogender Singh, Committee Member
Philip John Morris, Committee Member

16. DESIGN AND ANALYSIS OF THE MXS-R WINGLETS AND AIRFOILS TO IMPROVE AERODYNAMIC PERFORMANCE IN THE RED BULL AIR RACES

open_access
Open Access
Author:
Grasser, Nicholas Jared
Title:
DESIGN AND ANALYSIS OF THE MXS-R WINGLETS AND AIRFOILS TO IMPROVE AERODYNAMIC PERFORMANCE IN THE RED BULL AIR RACES
Graduate Program:
Aerospace Engineering
Keywords:
Aircraft Design
Aerodynamics
Airplane Simulation
Winglets
Airfoils
Red Bull
Air Racing
MXS-R
Airplane Performance
Airplane Design
File:
Download Grasser_-_MS_Thesis.pdf
Committee Members:
Mark David Maughmer, Thesis Advisor/Co-Advisor
Sven Schmitz, Committee Member
Philip John Morris, Committee Member

18. A Computational Study of Gaseous Jets Submerged in a Liquid Co-flow

open_access
Open Access
Author:
Fronzeo, Melissa A
Title:
A Computational Study of Gaseous Jets Submerged in a Liquid Co-flow
Graduate Program:
Aerospace Engineering
Keywords:
Computational fluid dynamics
multiphase flow
jets
submerged jets
ventilated cavities
File:
Download Fronzeo_Masters_Thesis.pdf
Committee Members:
Michael P Kinzel, Thesis Advisor/Co-Advisor
Jules Washington Lindau V, Committee Member
Zachary P Berger, Committee Member
Philip John Morris, Committee Member

19. Bounding Methods in Computational Fluid Dynamics for use in a Sequential Decision Process

open_access
Open Access
Author:
Valenti, Justin D
Title:
Bounding Methods in Computational Fluid Dynamics for use in a Sequential Decision Process
Graduate Program:
Aerospace Engineering
Keywords:
Computational Fluid Dynamics
Sequential Design Process
Trade Space Exploration
Design
Sequential Design
Bounding
Numerical Uncertainty
Discretization Uncertainty
File:
Download ValentiJ_MS_Thesis_FINAL.pdf
Committee Members:
Michael P Kinzel, Thesis Advisor/Co-Advisor
Simon Walter Miller, Committee Member
Mark David Maughmer, Committee Member
Philip John Morris, Committee Member

22. 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