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Start Over Degree MS Committee Member Amy Pritchett Committee Member Sven Schmitz

1. Physics-Infused Reduced-Order Modeling of Aerothermal Loads for Fluid-Thermal-Structural Interactions

open_access
Open Access
Author:
Vargas Venegas, Carlos
Title:
Physics-Infused Reduced-Order Modeling of Aerothermal Loads for Fluid-Thermal-Structural Interactions
Graduate Program:
Aerospace Engineering (MS)
Keywords:
hypersonic
fluid-thermal-structural
aerothermoelasticity
data-driven
physics-driven
physics-based
reduced-order modeling
machine learning
field inversion
aerothermal
turbulent viscous-inviscid interactions
neural ordinary differential equations
direct collocation
optimization
kriging
proper-orthogonal decomposition
latin hypercube sampling
thermoelastic
hypersonic vehicle
RANS
skin-panel
two-dimensional
gaussian process regression
computational fluid dynamics
supported panel
augmentation
augmented
model augmentation
surrogate
POD-kriging
POD
algebraic
differential
algebraic augmentation
differential augmentation
NODE
PIROM
analysis
File:
Download ms-thesis-corrected.pdf
Committee Members:
Daning Huang, Thesis Advisor/Co-Advisor
Puneet Singla, Committee Member
Amy Pritchett, Program Head/Chair
Sven Schmitz, Committee Member

2. A Computational Study of Flow Over a 6:1 Prolate Spheroid at Incidence

open_access
Open Access
Author:
Johnson, Samuel
Title:
A Computational Study of Flow Over a 6:1 Prolate Spheroid at Incidence
Graduate Program:
Aerospace Engineering (MS)
Keywords:
CFD
RANS
LES
Prolate Spheroid
File:
Download SamThesis_10_31.pdf
Committee Members:
Sven Schmitz, Thesis Advisor/Co-Advisor
Thomas S Chyczewski, Jr., Committee Member
Amy Pritchett, Program Head/Chair
Xiang Yang, Committee Member
James George Coder, Committee Member

3. Experimental Scaling of Hovering Rotorcraft Aerodynamics in Hyperbaric Conditions

open_access
Open Access
Author:
Kandias, Constantinos
Title:
Experimental Scaling of Hovering Rotorcraft Aerodynamics in Hyperbaric Conditions
Graduate Program:
Aerospace Engineering (MS)
Keywords:
Rotorcraft
Experimental
Aerospace
Engineering
Aerospace Engineering
Aerodynamics
File:
Download kandias-thesis-ms.pdf
Committee Members:
Mark A Miller, Thesis Advisor/Co-Advisor
Eric Greenwood, Committee Member
Amy Pritchett, Program Head/Chair
Sven Schmitz, Committee Member

4. Computational Analysis of Boundary-Layer Instabilities on a Slotted, Natural-Laminar-Flow Airfoil

open_access
Open Access
Author:
Gosin, Samuel
Title:
Computational Analysis of Boundary-Layer Instabilities on a Slotted, Natural-Laminar-Flow Airfoil
Graduate Program:
Aerospace Engineering (MS)
Keywords:
Computational Fluid Dynamics
Stationary Crossflow
SNLF Airfoils
ILES
RANS
Discrete Roughness Elements
LPSE
Boundary-Layer Transition
Wind-Tunnel Testing
File:
Download Samuel_Gosin_Thesis.pdf
Committee Members:
James George Coder, Thesis Advisor/Co-Advisor
Mark David Maughmer, Committee Member
Amy Pritchett, Program Head/Chair
Sven Schmitz, Committee Member

5. Application of Thrust-Drag and Power Balance Accounting to a Canonical Boundary Layer Ingesting Configuration

open_access
Open Access
Author:
Ibasitas, Matthew
Title:
Application of Thrust-Drag and Power Balance Accounting to a Canonical Boundary Layer Ingesting Configuration
Graduate Program:
Aerospace Engineering (MS)
Keywords:
Boundary Layer
Boundary Layer Ingestion
Ingestion
CFD
Fluid Dynamics
Canonical
Canonical Configuration
Power balance
Performance accounting
Thrust
drag
bookkeeping
performance bookkeeping
accounting
exergy
exergy analysis
exergy accounting
accounting system
performance accounting system
interference drag
dissipation
propulsion system integration
propulsion airframe interaction
interaction effects
BLI
ingestion
File:
Download Final_Thesis.pdf
Committee Members:
Amy Pritchett, Program Head/Chair
David K Hall, Thesis Advisor/Co-Advisor
Sven Schmitz, Committee Member
Mark A Miller, Committee Member

6. 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