Search

Start Over Graduate Program Aerospace Engineering Committee Member Cengiz Camci

1. DUCTED FAN INLET/EXIT AND ROTOR TIP FLOW IMPROVEMENTS FOR VERTICAL LIFT SYSTEMS

open_access
Open Access
Author:
Akturk, Ali
Title:
DUCTED FAN INLET/EXIT AND ROTOR TIP FLOW IMPROVEMENTS FOR VERTICAL LIFT SYSTEMS
Graduate Program:
Aerospace Engineering
Keywords:
Ducted fan
Inlet flow distortion
Tip leakage
Tip leakage mitigation
Double ducted fan
Pressure side platform
Fan rotor tip loss
Tip treatment
File:
Download Ali_Akturk-Dissertation.pdf
Committee Members:
Cengiz Camci, Dissertation Advisor/Co-Advisor
Cengiz Camci, Committee Chair/Co-Chair
Savas Yavuzkurt, Committee Member
Dennis K Mc Laughlin, Committee Member
Edward C Smith, Committee Member
Kenneth Steven Brentner, Committee Member
Michael H Krane, Committee Member

2. A TIME ACCURATE PREDICTION OF THE VISCOUS FLOW IN A TURBINE STAGE INCLUDING A ROTOR IN MOTION

open_access
Open Access
Author:
Shavalikul, Akamol
Title:
A TIME ACCURATE PREDICTION OF THE VISCOUS FLOW IN A TURBINE STAGE INCLUDING A ROTOR IN MOTION
Graduate Program:
Aerospace Engineering
Keywords:
CFD
time accurate prediction
turbine flow simulation
tip leakage
File:
Download Akamol_thesis1.pdf
Committee Members:
Cengiz Camci, Dissertation Advisor/Co-Advisor
Cengiz Camci, Committee Chair/Co-Chair
Dennis K Mc Laughlin, Committee Member
Savash Yavuzkurt, Committee Member
Timothy Francis Miller, Committee Member
Michael H Krane, Committee Member

3. AERODYNAMIC AND HEAT TRANSFER ASPECTS OF TIP AND CASING TREATMENTS USED FOR TURBINE TIP LEAKAGE CONTROL

open_access
Open Access
Author:
Gumusel, Baris
Title:
AERODYNAMIC AND HEAT TRANSFER ASPECTS OF TIP AND CASING TREATMENTS USED FOR TURBINE TIP LEAKAGE CONTROL
Graduate Program:
Aerospace Engineering
Keywords:
Turbine Tip Leakage Control
Inclined Squealer Tip
Blade Tip Shape
Casing Treatment
Shroud Heat Transfer
Tip Leakage Desensitization
File:
Download Gumusel.Baris.Dissertation.pdf
Committee Members:
Cengiz Camci, Dissertation Advisor/Co-Advisor
Cengiz Camci, Committee Chair/Co-Chair
Dennis K Mc Laughlin, Committee Member
Savas Yavuzkurt, Committee Member
Timothy Francis Miller, Committee Member

4. PREDICTION OF SAND PARTICLE TRAJECTORIES AND SAND EROSION DAMAGE ON HELICOPTER ROTOR BLADES

open_access
Open Access
Author:
Shin, Bong Gun
Title:
PREDICTION OF SAND PARTICLE TRAJECTORIES AND SAND EROSION DAMAGE ON HELICOPTER ROTOR BLADES
Graduate Program:
Aerospace Engineering
Keywords:
Rotorcraft
Aerodynamics
Particle Trajectory
Sand Erosion
Helicopter rotor blade
File:
Download Dissertation_BongGun_Aerospace_Engineering_May_2010.pdf
Committee Members:
Cengiz Camci, Dissertation Advisor/Co-Advisor
Cengiz Camci, Committee Chair/Co-Chair
Dennis K Mclaughlin, Committee Member
Savas Yavuzkurt, Committee Member
Timothy Francis Miller, Committee Member
Michael H Krane, Committee Member

6. Modeling and Simulation of Radiation from Hypersonic Flows using Monte Carlo Methods

open_access
Open Access
Author:
Sohn, Ilyoup
Title:
Modeling and Simulation of Radiation from Hypersonic Flows using Monte Carlo Methods
Graduate Program:
Aerospace Engineering
Keywords:
Radiation
Hypersonic
Monte Carlo Methods
Nonequilibrium
File:
Download mythesis_Sohn_final.pdf
Committee Members:
Deborah A Levin, Dissertation Advisor/Co-Advisor
Deborah A Levin, Committee Chair/Co-Chair
Cengiz Camci, Committee Member
Michael Matthew Micci, Committee Member
Michael F Modest, Committee Member

7. Design, Fabrication, and Testing of an Ultrasonic De-Icing System for Helicopter Rotor Blades

open_access
Open Access
Author:
Palacios, Jose Luis
Title:
Design, Fabrication, and Testing of an Ultrasonic De-Icing System for Helicopter Rotor Blades
Graduate Program:
Aerospace Engineering
Keywords:
dispersion curves
icing rotor blades
ice protection
anti-icing
de-icing
ultrasound
wave structure
high power ultrasound
File:
Download Palacios_PhD_Thesis_2008.pdf
Committee Members:
Edward A Smith, Committee Chair/Co-Chair
Joseph Rose, Committee Chair/Co-Chair
Farhan Gandhi, Committee Member
Cengiz Camci, Committee Member
Bernhard R Tittmann, Committee Member
Kon Well Wang, Committee Member

8. On the Characterization of Noise Sources in Supersonic Shock Containing Jets

open_access
Open Access
Author:
Veltin, Jeremy
Title:
On the Characterization of Noise Sources in Supersonic Shock Containing Jets
Graduate Program:
Aerospace Engineering
Keywords:
jet noise
aeroacoustic
supersonic pitot
schlieren
optical deflectometry
mach wave
correlation
File:
Download Thesis_J_Veltin_Vf.pdf
Committee Members:
D.K. McLaughlin, Dissertation Advisor/Co-Advisor
D.K. McLaughlin, Committee Chair/Co-Chair
Philip John Morris, Committee Chair/Co-Chair
Kenneth Steven Brentner, Committee Member
Cengiz Camci, Committee Member
Anthony A Atchley, Committee Member

9. The Modeling of Homogeneous Condensation in Free-expanding Plumes with the Direct Simulation Monte Carlo Method

open_access
Open Access
Author:
Zhong, Jiaqiang
Title:
The Modeling of Homogeneous Condensation in Free-expanding Plumes with the Direct Simulation Monte Carlo Method
Graduate Program:
Aerospace Engineering
Keywords:
free-expanding plume
condensation
DSMC
File:
Download Zhong-Jiaqiang-thesis.pdf
Committee Members:
Deborah A Levin, Committee Chair/Co-Chair
Kenneth Steven Brentner, Committee Member
Michael Matthew Micci, Committee Member
Cengiz Camci, Committee Member
Vigor Yang, Committee Member

10. DESENSITIZATION OF OVER TIP LEAKAGE IN AN AXIAL TURBINE ROTOR BY TIP SURFACE COOLANT INJECTION

open_access
Open Access
Author:
Rao, Nikhil Molahally
Title:
DESENSITIZATION OF OVER TIP LEAKAGE IN AN AXIAL TURBINE ROTOR BY TIP SURFACE COOLANT INJECTION
Graduate Program:
Aerospace Engineering
Keywords:
Axial turbine
over tip leakage
tip leakage flow
tip surface coolant injection
turbine tip desensitization
File:
Download NikhilThesisF.pdf
Committee Members:
Cengiz Camci, Committee Chair/Co-Chair
Dennis K Mc Laughlin, Committee Member
Lyle Norman Long, Committee Member
Savas Yavuzkurt, Committee Member
Timothy F Miiler, Committee Member

11. NONAXISYMMETRIC ENDWALL CONTOURING AND LEADING EDGE MODIFICATIONS ON TURBINE NOZZLE GUIDE VANES

open_access
Open Access
Author:
Turgut, Ozhan Hulusi
Title:
NONAXISYMMETRIC ENDWALL CONTOURING AND LEADING EDGE MODIFICATIONS ON TURBINE NOZZLE GUIDE VANES
Graduate Program:
Aerospace Engineering
Keywords:
nonaxisymmetric endwall contouring
secondary flows
gas turbine
leading edge fillets
File:
Download OzhanTurgut-Dissertation.pdf
Committee Members:
Cengiz Camci, Dissertation Advisor/Co-Advisor
Cengiz Camci, Committee Chair/Co-Chair
Savas Yavuzkurt, Committee Member
Deborah A Levin, Committee Member
Anil Kamalakant Kulkarni, Committee Member

12. COMPARATIVE NUMERICAL ANALYSIS OF FLOW DEVELOPMENT IN THE PRESENCE OF ENDWALL FENCES UPSTREAM OF A VERTICAL CYLINDER IN CROSS FLOW

open_access
Open Access
Author:
Gokce, Zeki Ozgur
Title:
COMPARATIVE NUMERICAL ANALYSIS OF FLOW DEVELOPMENT IN THE PRESENCE OF ENDWALL FENCES UPSTREAM OF A VERTICAL CYLINDER IN CROSS FLOW
Graduate Program:
Aerospace Engineering
Keywords:
horseshoe vortex formation around a vertical cylin
upstream endwall fences
File:
Download Zeki_Ozgur_Gokce_MS_Thesis.pdf
Committee Members:
Cengiz Camci, Thesis Advisor/Co-Advisor
Cengiz Camci, Thesis Advisor/Co-Advisor

13. Conceptualization, Modeling, and Characterization of a Cf Driven Multi-State Lead-lag Bypass Damper

open_access
Open Access
Author:
Marr, Conor Matthew
Title:
Conceptualization, Modeling, and Characterization of a Cf Driven Multi-State Lead-lag Bypass Damper
Graduate Program:
Aerospace Engineering
Keywords:
Damper
Fluidlastic
Hydraulic
CFD
Modeling
Multi-State
Bypass
Passive Damping
Lead-Lag Damper
Ground Resonance
File:
Download CMarrPhDThesis2012FINAL.pdf
Committee Members:
Edward Smith, Committee Chair/Co-Chair
George A Lesieutre, Dissertation Advisor/Co-Advisor
Cengiz Camci, Committee Member
Christopher Rahn, Special Member

14. An Automated Calibration and a Correction Scheme for Total Pressure Gradient Effects of Subminiature Five-Hole Probe

open_access
Open Access
Author:
Town, Jason Edward
Title:
An Automated Calibration and a Correction Scheme for Total Pressure Gradient Effects of Subminiature Five-Hole Probe
Graduate Program:
Aerospace Engineering
Keywords:
Five-hole probe
automated
calibration
correction
total pressure gradient
File:
Download JasonTown_Masters_Thesis.pdf
Committee Members:
Cengiz Camci, Thesis Advisor/Co-Advisor
Savas Yavuzkurt, Thesis Advisor/Co-Advisor

15. ENDWALL SHAPE MODIFICATION USING VORTEX GENERATORS AND FENCES TO IMPROVE GAS TURBINE COOLING AND EFFECTIVENESS

open_access
Open Access
Author:
Gokce, Zeki Ozgur
Title:
ENDWALL SHAPE MODIFICATION USING VORTEX GENERATORS AND FENCES TO IMPROVE GAS TURBINE COOLING AND EFFECTIVENESS
Graduate Program:
Aerospace Engineering
Keywords:
Vortex generator
heat transfer enhancement
gas turbine cooling channel flow
File:
Download Zeki_Ozgur_Gokce_PhD_Thesis_Final_Submission.pdf
Committee Members:
Cengiz Camci, Dissertation Advisor/Co-Advisor
Cengiz Camci, Committee Chair/Co-Chair
Sven Schmitz, Committee Member
Savas Yavuzkurt, Committee Member
Timothy Francis Miller, Committee Member

16. Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades

open_access
Open Access
Author:
Topcuoglu, Ilker
Title:
Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades
Graduate Program:
Aerospace Engineering
Keywords:
Film cooling
gas turbine cooling
aerodynamic loss prediction
total pressure loss model
File:
Download IlkerTopcuoglu-_MS_Thesis.pdf
Committee Members:
Cengiz Camci, Thesis Advisor/Co-Advisor

17. Implementation Of Ducted Fans On A Low Cost Semi-autonomous Lighter-than-air Uninhabited Aerial Vehicle

open_access
Open Access
Author:
Oruc, Ilker
Title:
Implementation Of Ducted Fans On A Low Cost Semi-autonomous Lighter-than-air Uninhabited Aerial Vehicle
Graduate Program:
Aerospace Engineering
Keywords:
airship
blimp
arduino
autopiot
ducted
fans
electric
uninhabited
aerial
vehicle
unmanned
control
sensors
lighter-than-air
File:
Download Ilker_Oruc_-_Thesis.pdf
Committee Members:
Cengiz Camci, Thesis Advisor/Co-Advisor

19. Simulation and Experimental Validation of the Wheel Space of the Axial Flow Turbine Research Facility Under Low Purge Flow Conditions

open_access
Open Access
Author:
Averbach, Michael Alec
Title:
Simulation and Experimental Validation of the Wheel Space of the Axial Flow Turbine Research Facility Under Low Purge Flow Conditions
Graduate Program:
Aerospace Engineering
Keywords:
Gas Turbines
Axial Flow Turbine
AFTRF
Wheel Space
Purge Flow
Ingress
File:
Download Michael_Averbach_MS_Thesis_Sp2014.pdf
Committee Members:
Cengiz Camci, Thesis Advisor/Co-Advisor

21. An Investigation of Rim Seal/Disk Cavity Flow and its Interaction with High Pressure Turbine Rotor Flows

open_access
Open Access
Author:
Town, Jason Edward
Title:
An Investigation of Rim Seal/Disk Cavity Flow and its Interaction with High Pressure Turbine Rotor Flows
Graduate Program:
Aerospace Engineering
Keywords:
Rim Seal Cavity
Gas Turbine
Secondary Flow
Rotor Blade Tip Treatments
Rim Seal Cavity Purge
File:
Download Jason_Town_Dissertation_Final.pdf
Committee Members:
Cengiz Camci, Dissertation Advisor/Co-Advisor
Savas Yavuzkurt, Committee Chair/Co-Chair
Horacio Perez Blanco, Committee Member
Dennis K Mclaughlin, Committee Member

22. The Prediction of Unsteady Aerodynamic Loading in High Aspect Ratio Wall Bounded Jets

open_access
Open Access
Author:
Lurie, Michael Brian
Title:
The Prediction of Unsteady Aerodynamic Loading in High Aspect Ratio Wall Bounded Jets
Graduate Program:
Aerospace Engineering
Keywords:
Aerospace
Vibrations
CFD
Computational
Acoustics
Experiment
Turbulence
Free Jet
Wall Jet
Nozzle
File:
Download Lurie-Dissertation_FINAL.pdf
Committee Members:
Philip John Morris, Dissertation Advisor/Co-Advisor
Dennis K Mclaughlin, Committee Member
Cengiz Camci, Committee Member
Stephen A Hambric, Special Member

23. Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface

open_access
Open Access
Author:
Myers, Leighton Montgomery
Title:
Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface
Graduate Program:
Aerospace Engineering
Keywords:
STOVL Aerodynamics
V/STOL Aerodynamics
Experimental Aerodynamics
Impinging Jet
High Speed Jet
File:
Download LeightonMyers-Dissertation-v350z.pdf
Committee Members:
Dennis K Mc Laughlin, Dissertation Advisor/Co-Advisor
Philip John Morris, Committee Member
Cengiz Camci, Committee Member
Stephen R Turns, Committee Member
David Findlay, Special Member

24. Modeling of Energy Transfer in Hypersonic Shocks using High Fidelity Models

open_access
Open Access
Author:
Zhu, Tong
Title:
Modeling of Energy Transfer in Hypersonic Shocks using High Fidelity Models
Graduate Program:
Aerospace Engineering
Keywords:
DIRECT SIMULATION MONTE CARLO
HYPERSONIC SHOCK FLOWS
NONEQUILIBRIUM FLOWS
RADIATION FROM SHOCKS
RELAXATIONS OF NITROGEN
File:
Download Modeling_of_Energy_Transfer_in_Hypersonic_Shocks_using_High_Fidelity_Models.pdf
Committee Members:
Deborah Levin, Dissertation Advisor/Co-Advisor
Deborah Levin, Committee Chair/Co-Chair
Cengiz Camci, Committee Member
Michael Matthew Micci, Committee Member
Adrianus C Van Duin, Committee Member
Marco Panesi, Special Member

25. NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION OF THRUST PRODUCED BY A HOBBY–SCALE PULSEJET ENGINE

open_access
Open Access
Author:
Zhu, Mengyao
Title:
NUMERICAL SIMULATION AND EXPERIMENTAL INVESTIGATION OF THRUST PRODUCED BY A HOBBY–SCALE PULSEJET ENGINE
Graduate Program:
Aerospace Engineering
Keywords:
pulsejet
lax-wendroff
numerical simulation
experiment
thrust
operating frequency
File:
Download Master_thesis_by_Mengyao_Zhu.pdf
Committee Members:
Michael Matthew Micci, Thesis Advisor/Co-Advisor
Cengiz Camci, Thesis Advisor/Co-Advisor

26. STUDY OF MITIGATION OF TURBINE BLADE TIP LEAKAGE FLOWS USING TIP LEAKAGE INTERRUPTER

open_access
Open Access
Author:
Andichamy, Veerandra Chakkarava
Title:
STUDY OF MITIGATION OF TURBINE BLADE TIP LEAKAGE FLOWS USING TIP LEAKAGE INTERRUPTER
Graduate Program:
Aerospace Engineering
Keywords:
Turbine blade tip
Tip leakage flows
leakage vortex
Leakage vortex mitigation
turbine blade tip design
blade tip modification
File:
Download Masters_Thesis_Veerandra_AUG_2017.pdf
Committee Members:
Cengiz Camci, Thesis Advisor/Co-Advisor

27. A design strategy for a 6:1 supersonic mixed-flow compressor stage and its viscous flow-based performance analysis

open_access
Open Access
Author:
Sadagopan, Aravinth
Title:
A design strategy for a 6:1 supersonic mixed-flow compressor stage and its viscous flow-based performance analysis
Graduate Program:
Aerospace Engineering
Keywords:
mixed-flow compressor
mean-line design
turbomachinery
computational fluid dynamics
shock stability
aerospace propulsion
Bezier curves
NASA Rotor 37
Supersonic Diffuser
6:1
pressure-ratio
blade optimization
File:
Download MS_thesis_Aravinth_Sadagopan_May_2019.pdf
Committee Members:
Cengiz Camci, Thesis Advisor/Co-Advisor

28. Conceptual development of casing Patterns to reduce the aerodynamic losses in an axial turbine stage

open_access
Open Access
Author:
Ranka, Amrat Arvind
Title:
Conceptual development of casing Patterns to reduce the aerodynamic losses in an axial turbine stage
Graduate Program:
Aerospace Engineering
Keywords:
Turbines
axial gas turbine
casing grooves
computational fluid dynamics
CFD
Tip-Leakage losses
Tip-mitigation studies
Turbomachinery
AFTRF
leakage Vortex
Horseshoe Vortex
File:
Download Final_thesis.pdf
Committee Members:
Cengiz Camci, Thesis Advisor/Co-Advisor
Dr. Sven Schmitz, Committee Member
Amy Ruth Pritchett, Program Head/Chair

29. SIMULATION OF SUPERSONIC JET NOISE REDUCTION USING FLUID INSERTS FOR LOW BYPASS RATIO TURBOFANS

open_access
Open Access
Author:
Prasad, Chitrarth
Title:
SIMULATION OF SUPERSONIC JET NOISE REDUCTION USING FLUID INSERTS FOR LOW BYPASS RATIO TURBOFANS
Graduate Program:
Aerospace Engineering
Keywords:
supersonic
noise reduction
Large eddy simulation
Proper Orthogonal Decomposition
Doak's Momentum Potential Theory
File:
Download Simulation_of_supersonic_jet_noise_Prasad_dissertation_PSU.pdf
Committee Members:
Philip Morris, Dissertation Advisor/Co-Advisor
Philip John Morris, Committee Chair/Co-Chair
Kenneth Steven Brentner, Committee Member
Cengiz Camci, Committee Member
Daniel Connell Haworth, Outside Member
Amy Ruth Pritchett, Program Head/Chair

30. AN INVESTIGATION OF USING TIP LEAKAGE INTERRUPTER AND BLADE SLIT TO MITIGATE AERODYNAMIC LOSSES IN AXIAL TURBINE STAGE

open_access
Open Access
Author:
Andichamy, Veerandra Chakkarava
Title:
AN INVESTIGATION OF USING TIP LEAKAGE INTERRUPTER AND BLADE SLIT TO MITIGATE AERODYNAMIC LOSSES IN AXIAL TURBINE STAGE
Graduate Program:
Aerospace Engineering
Keywords:
Axial Turbines
Tip Leakage Flow
Blade Slit
TLI
Turbomachinery
File:
Download Thesis_draft_Veerandra_Andichamy_Dec_4.pdf
Committee Members:
Cengiz Camci, Dissertation Advisor/Co-Advisor
Cengiz Camci, Committee Chair/Co-Chair
Savas Yavuzkurt, Outside Member
Jose Palacios, Committee Member
Michael P Kinzel, Committee Member
Yong W Kim, Special Member
Amy Ruth Pritchett, Program Head/Chair

31. Aeroacoustic Characterization of Dual-Stream, Supersonic, Rectangular Exhaust Jets

open_access
Open Access
Author:
Hromisin, Scott Michael
Title:
Aeroacoustic Characterization of Dual-Stream, Supersonic, Rectangular Exhaust Jets
Graduate Program:
Aerospace Engineering
Keywords:
Aeroacoustics
Jet Noise
Supersonic jets
Multi-stream jets
File:
Download Hromisin_PhD_Dissertation_-_26Nov19_edit.pdf
Committee Members:
Philip John Morris, Dissertation Advisor/Co-Advisor
Philip John Morris, Committee Chair/Co-Chair
Cengiz Camci, Committee Member
Jose Palacios, Committee Member
Robert Francis Kunz, Outside Member
Dennis K Mc Laughlin, Special Member
Amy Ruth Pritchett, Program Head/Chair