1. Trailing Edge Noise Prediction Using The Nonlinear Disturbance Equations Open Access Author: Erwin, James Paul Title: Trailing Edge Noise Prediction Using The Nonlinear Disturbance Equations Graduate Program: Aerospace Engineering Keywords: computationalacousticspredictionedgetrailingnoisebroadbandcfdfluiddynamics File: Download Erwin-thesis.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorKenneth Steven Brentner, Thesis Advisor/Co-AdvisorPhilip John Morris, Thesis Advisor/Co-Advisor
2. Acoustics of Ducted Rotors Open Access Author: Zentichko, Jacob S Title: Acoustics of Ducted Rotors Graduate Program: Aerospace Engineering Keywords: AcousticsDuctedRotorsCFDFLUENTPSUWOPWOPFSCESMFast Scattering CodeFwocsWilliamsHawkings File: Download Thesis_Jacob_Final.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorKenneth Steven Brentner, Thesis Advisor/Co-Advisor
3. Time dependent actuator disk model for a helicopter rotor in hover Open Access Author: Mentey, Jeswanth Title: Time dependent actuator disk model for a helicopter rotor in hover Graduate Program: Aerospace Engineering Keywords: time dependent actuator diskactuator surfaceactuator linemomentum sourceCFD analysis of rotorUFVShybrid method File: Download JeswanthMentey_MSThesis.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
4. Development of a Trailing-Edge Noise Prediction Method using the Non-Linear Disturbance Equations 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 noisecomputational aeroacousticsnon-linear disturbance equationswind turbine noise File: Download PSUThesisChristiansenFINAL072914.pdf Committee Members: Philip John Morris, Thesis Advisor/Co-AdvisorKenneth Steven Brentner, Thesis Advisor/Co-Advisor
5. ACOUSTIC PREDICTION OF HEAVY LIFT ROTOR CONFIGURATIONS USING MOMENTUM SOURCE METHOD Open Access Author: Mohanamuraly, Pavanakumar Title: ACOUSTIC PREDICTION OF HEAVY LIFT ROTOR CONFIGURATIONS USING MOMENTUM SOURCE METHOD Graduate Program: Aerospace Engineering Keywords: momentum sourcerotorcraft aeroacousticsactuator modelinteractional aeroacoustics File: Download Muraly-thesis.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorKenneth Steven Brentner, Thesis Advisor/Co-Advisor
6. ENHANCEMENTS AND INVESTIGATION OF CAPABILITIES TO THE LANDING GEAR MODEL AND ACOUSTIC PREDICTION SOFTWARE 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: Boeingairframe noiseLGMAPlanding gearacousticsaerospacetrailing edgeaeroacousticsaircraftairframe noisenoisenosie predictionpredictionGulfstream File: Download TRM_Thesis_Final.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorPhilip John Morris, Thesis Advisor/Co-AdvisorKenneth Steven Brentner, Thesis Advisor/Co-Advisor
7. Noise generation mechanisms in short ducted rotors Open Access Author: Padala, V Santhosh Title: Noise generation mechanisms in short ducted rotors Graduate Program: Aerospace Engineering Keywords: aerodynamic noiseducted rotorsunsteady loading responsestrut wakeCFD File: Download SANTHOSH_MSTHESIS.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorKenneth Steven Brentner, Thesis Advisor/Co-Advisor
8. Modifications to Psu-wopwop For Enhanced Noise Prediction Capabilities Open Access Author: Goldman, Benjamin A Title: Modifications to Psu-wopwop For Enhanced Noise Prediction Capabilities Graduate Program: Aerospace Engineering Keywords: BenjaminGoldmanFW-HPSU-WOPWOP File: Download Goldman_Ben-Thesis.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
9. Acoustic Analysis of Compound Helicopters with Trim Variations Open Access Author: Barron, Heather Marie Title: Acoustic Analysis of Compound Helicopters with Trim Variations Graduate Program: Aerospace Engineering Keywords: HelicopterrotorcraftrotorcraftacousticWOPWOPPSU-WOPWOPaerospacecompoundanalysis File: Download Barron_Thesis_v10.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
10. Computational Modeling of Rotor Blade Performance Degradation Due to Ice Accretion Open Access Author: Brown, Christine Meredyth Title: Computational Modeling of Rotor Blade Performance Degradation Due to Ice Accretion Graduate Program: Aerospace Engineering Keywords: icingCFDturbulence modelingmesh generation File: Download 1-CBrown_MSThesis.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
11. Trailing Edge Noise Prediction Using the Non-Linear Disturbance Equations Open Access Author: Jain, Abhishek Title: Trailing Edge Noise Prediction Using the Non-Linear Disturbance Equations Graduate Program: Aerospace Engineering Keywords: CAACFDTrailing EdgeTurbulenceSynthetic Eddy MethodInflow Boundary Conditions File: Download Thesis_AJ_final1.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorPhilip John Morris, Thesis Advisor/Co-Advisor
12. Tools for Development and Analysis of Rotorcraft Open Access Author: Li, Yaowei Title: Tools for Development and Analysis of Rotorcraft Graduate Program: Aerospace Engineering Keywords: Rotorcraft noise abatement procedure. File: Download Y_Li_MS_Thesis_final.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-Advisor
13. Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction Open Access Author: Corle, Ethan Lewis Title: Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction Graduate Program: Aerospace Engineering Keywords: active flaprotor noiseaeroacousticsgenetic algorithmhelicopter quieting File: Download Corle_MS_Thesis.pdf Committee Members: Sven Schmitz, Thesis Advisor/Co-AdvisorKenneth Steven Brentner, Thesis Advisor/Co-AdvisorGeorge A Lesieutre, Thesis Advisor/Co-Advisor
14. A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT Open Access Author: Walsh, Gregory Daniel Title: A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT Graduate Program: Aerospace Engineering Keywords: AcousticsCoaxial HelicopterRotorcraftRotorcraft AcousticsHelicopter File: Download Walsh_Thesis.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorJacob Willem Langelaan, Committee MemberGeorge A Lesieutre, Committee Member
15. Rotorcraft Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics Open Access Author: Saetti, Umberto Title: Rotorcraft Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics Graduate Program: Aerospace Engineering Keywords: rotorcraftnoisecontrolcontrol systemsdynamic inversionfeedbackflight dynamicsfree wakeCHARMPSUHeloSimPSUWOPWOP File: Download UmbertoSaetti_Thesis_v9.pdf Committee Members: Joseph Francis Horn, Thesis Advisor/Co-AdvisorKenneth Steven Brentner, Committee MemberGeorge A Lesieutre, Committee Member
16. Incorporating Acoustic Assessment into the Design and Analysis of Rotorcraft Open Access Author: Sharma, Kalki Title: Incorporating Acoustic Assessment into the Design and Analysis of Rotorcraft Graduate Program: Aerospace Engineering Keywords: NDARCPSU-WOPWOPWOPItRotorcraft AcousticsNoise PredictionConceptual Design File: Download Kalki_Sharma_MS_Thesis.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorGeorge A Lesieutre, Committee MemberEdward Smith, Committee Member
17. Development of an Acoustic Prediction System for Conceptual Design and Analysis of Rotorcraft Open Access Author: Jaworski, Thomas Title: Development of an Acoustic Prediction System for Conceptual Design and Analysis of Rotorcraft Graduate Program: Aerospace Engineering Keywords: AcousticsRotorcraftAerospaceBVIHSINoise File: Download Thomas_Jaworski_Thesis_2020_Release.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorAmy Ruth Pritchett, Program Head/ChairAmy Ruth Pritchett, Committee MemberEric Greenwood, Committee Member
18. A Preliminary Investigation of Propeller-Wing Interaction Noise for eVTOL Aircraft Open Access Author: Mukherjee, Bhaskar Title: A Preliminary Investigation of Propeller-Wing Interaction Noise for eVTOL Aircraft Graduate Program: Aerospace Engineering Keywords: aeroacousticspropeller-wing aerodynamicspropeller-wing acousticslow speed propeller noiseeVTOLUAMlow-fidelityfundamental noise File: Download Bhaskar_thesis_corrections_ver1.pdf Committee Members: Kenneth Steven Brentner, Thesis Advisor/Co-AdvisorEric Greenwood, Committee MemberAmy Ruth Pritchett, Program Head/Chair