Search

Start Over Graduate Program Aerospace Engineering Committee Member Kenneth Steven Brentner

21. 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

22. IMPROVED CHEMISTRY MODELS FOR DSMC SIMULATIONS OF IONIZED RAREFIED HYPERSONIC FLOWS

open_access
Open Access
Author:
Ozawa, Takashi
Title:
IMPROVED CHEMISTRY MODELS FOR DSMC SIMULATIONS OF IONIZED RAREFIED HYPERSONIC FLOWS
Graduate Program:
Aerospace Engineering
Keywords:
MD
QCT
Stardust
Ionization
Rarefied gas
DSMC
Hypersonic flows
File:
Download main.pdf
Committee Members:
Deborah A Levin, Committee Chair/Co-Chair
Robert Graham Melton, Committee Member
Michael Matthew Micci, Committee Member
Kenneth Steven Brentner, Committee Member
James Bernhard Anderson, Committee Member

25. The Prediction of Noise and Installation Effects of High-subsonic Dual-stream Jets in Flight

open_access
Open Access
Author:
Saxena, Swati
Title:
The Prediction of Noise and Installation Effects of High-subsonic Dual-stream Jets in Flight
Graduate Program:
Aerospace Engineering
Keywords:
aeroacoustics
subsonic jet noise
dual-stream jets
forward flight
installation effects
turbulence modeling
DES
File:
Download Swati-Dissertation.pdf
Committee Members:
Philip John Morris, Dissertation Advisor/Co-Advisor
Dennis K Mclaughlin, Committee Member
Kenneth Steven Brentner, Committee Member
Victor Ward Sparrow, Committee Member

27. 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

28. Wind Turbine Design Using A Free-wake Vortex Method With Winglet Application

open_access
Open Access
Author:
Maniaci, David Charles
Title:
Wind Turbine Design Using A Free-wake Vortex Method With Winglet Application
Graduate Program:
Aerospace Engineering
Keywords:
Wind turbine
winglet
free-wake
vortex method
rotor aerodynamics
blade design
File:
Download psu-thesis-Dmaniaci-18m_FIN_4-5-13_DateChange.pdf
Committee Members:
Mark David Maughmer, Dissertation Advisor/Co-Advisor
Mark David Maughmer, Committee Chair/Co-Chair
Barnes Warnock Mccormick Jr., Committee Member
Dennis K Mc Laughlin, Committee Member
Kenneth Steven Brentner, Committee Member
Sue Ellen Haupt, Committee Member
Sven Schmitz, Committee Member