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Start Over Committee Member Jose Palacios Committee Member Sven Schmitz

1. Design, Analysis, and Testing of Leading-Edge Protection Tapes for Wind Turbine Blades

open_access
Open Access
Author:
Major, Desirae
Title:
Design, Analysis, and Testing of Leading-Edge Protection Tapes for Wind Turbine Blades
Graduate Program:
Aerospace Engineering
Keywords:
Renewable Energy
Wind Turbines
Annual Energy Production
Leading-edge Protection Tape
Wind Turbine Leading-edge Erosion
File:
Download PSU_Masters_Thesis_Final_Desirae_Major.pdf
Committee Members:
Jose Palacios, Thesis Advisor/Co-Advisor
Sven Schmitz, Thesis Advisor/Co-Advisor
Amy Ruth Pritchett, Committee Member

2. An Aerothermal Study of Ejector-Based, Coandă-Surface-Driven, Gas Turbine Tip Leakage Mitigation Schemes: A Computational and Experimental Approach

restricted
Restricted
Author:
Khokhar, Gohar
Title:
An Aerothermal Study of Ejector-Based, Coandă-Surface-Driven, Gas Turbine Tip Leakage Mitigation Schemes: A Computational and Experimental Approach
Graduate Program:
Aerospace Engineering (PHD)
Keywords:
Ejector-Based
Coandă-Surface-Driven
Gas Turbine Tip Leakage Mitigation
Gas Turbine
Tip Leakage
Ejector
Coanda Surface
File:

No files available due to restrictions.

Committee Members:
Sven Schmitz, Major Field Member
Michael Krane, Outside Unit & Field Member
Jose Palacios, Major Field Member
Cengiz Camci, Chair & Dissertation Advisor
Dennis K Mc Laughlin, Special Member
Amy Pritchett, Program Head/Chair

3. Mid-Fidelity Performance Analysis for Fixed-Pitch Speed-Controlled Multirotor Aircraft

restricted_to_institution
Restricted (Penn State Only)
Author:
Cornelius, Jason
Title:
Mid-Fidelity Performance Analysis for Fixed-Pitch Speed-Controlled Multirotor Aircraft
Graduate Program:
Aerospace Engineering (PHD)
Keywords:
Helicopter
Multirotor
CFD
Rotorcraft
High Performance Computing
GPU
Coaxial
Coaxial Rotor
Machine Learning
Surrogate Models
Dragonfly
Drone
UAS
Urban Air Mobility
Unmanned Aerial Systems
BEMT
Aerodynamics
Aircraft
C81 Tables
OVERFLOW
ARC2D
Airfoil Performance
NASA
Langley TDT
Langley 14-by 22-ft. Subsonic Tunnel Facility
Langley Transonic Dynamics Tunnel
Hybrid BEMT-URANS CFD
Linux Bash Scripting
GPU CFD Acceleration
Gaussian Process Regression
Neural Networks
Conceptual Design
Preliminary Design
File:
Login to Download
Committee Members:
Amy Pritchett, Program Head/Chair
Daniel Haworth, Outside Unit & Field Member
Sven Schmitz, Chair & Dissertation Advisor
Jacob Langelaan, Major Field Member
Jose Palacios, Major Field Member
Edward Smith, Major Field Member
Larry Young, Special Signatory