Name
Title
Author
Comments
DR497-02E-190-001A
Compressor: Impeller Preliminary Design Using Aungier's Method
Marc Charest
 
DR497-02E-190-002A
Compressor: Impeller Preliminary Design Using Slip Factor Approach
Marc Charest
 
DR497-02E-190-003A
Compressor: Impeller Preliminary Design Using a Refined Slip Factor Approach
Marc Charest
 
DR497-02E-190-004A
Initial Turbine Rotor Sizing Estimate
Steve Elia
 
DR497-02E-190-005A
Modifications to the Test Rig to Allow for Turbine Testing
Brent Muio
 
DR497-02E-190-006A
Compressor: Axial Thrust Estimation
Marc Charest
 
DR497-02E-190-007A
Compressor: Axial Thrust Estimation Using Rigid Body Motion
Marc Charest
 
DR497-02E-190-008A
Compressor: Initial Impeller Analysis and Suggested Further Actions
Marc Charest
 
DR497-02E-190-009A
Compressor: Estimation of Vane Number
Marc Charest
 
DR497-02E-190-010A
Compressor: Outlet Diameter
Marc Charest
 
DR497-02E-190-011A
Compressor: Impeller Analysis and Detailed Design
Marc Charest
 
DR497-02E-190-012A
Compressor: Diffuser Preliminary Design and Analysis
Marc Charest
 
DR497-02E-190-013A
Compressor: Volute Preliminary Sizing
Marc Charest
 
DR497-02E-190-014A
Compressor: Performance Prediction
Marc Charest
 
DR497-02E-190-015A
Turbine Rotor Optimization and CFD Analysis
Steve Elia
 
DR497-02E-190-016A
Turbine Rotor Axial Load Estimation
Steve Elia
 
DR497-02E-190-017A
Preliminary Nozzle Design and Loss Estimation
Steve Elia
 
DR497-02E-190-018A
Preliminary Volute Design and Loss Estimation
Steve Elia
 
Compressor: Recommendations
Marc Charest
 
DR497-02E-190-020A
Parts and Suppliers Used in the Modification of the Turbomachinery Test Rig
Brent Muio
 
DR497-02E-190-021A
Recommendations and Useful Information for the Turbomachinery Test Rig
Brent Muio
 
DR497-02E-190-022A
Preliminary Test Results
Brent Muio
 

TDR497-02E-190-001A
Compressor: Impeller Preliminary Design Using Wilson't Method
Marc Charest
 
TDR497-02E-190-002A
Initial Turbine Rotor Sizing Method
Steve Elia
 
TDR497-02E-190-003A
Gearbox Feasibility
Brent Muio
 
TDR497-02E-190-004A
Compressor: Impeller Preliminary Design Using Aungier's Method
Marc Charest
 

DR4907-03GT-190-001
Compressor and Compressor Casing Design Conversion for High Speed Aerodynamic Test Rig
Tyson Ferguson
 
DR4907-03GT-190-002
Final Turbine Rotor Sizing Estimate
Maher El-Moussa
 
DR4907-03GT-190-005
Revised Stator Design and Theoretical Loss Estimation
Maher El-Moussa
 
DR4907-03GT-190-006
Stator Blade Optimisation and BladeGen+ Analysis
Maher El-Moussa
 
DR4907-03GT-190-007
Stator Blades Optimisation and CFX-5 Analysis
Maher El-Moussa
 
DR4907-03GT-190-008
Turbine Rotor Optimisation and CFX-5 Analysis
Maher El-Moussa
 
DR4907-03GT-190-009
Compressor: Rotor CFD Analysus Using CFX-6
Hamza Abo El Ella
 
DR4907-03GT-190-010
Compressor: Volute Design Modification
Hamza Abo El Ella
Replaced by DR4907-03GT-180-002
DR4907-03GT-190-011
Compressor: Back Cavity Preliminary CFD Analysis for Axial Thrust Prediction
Hamza Abo El Ella
 
Compressor: Back Cavity Preliminary CFD Analysis for Axial Thrust Prediction
Hamza Abo El Ella
 
DR4907-03GT-190-013
Compressor Test Rig Instrumentation
Tyson Ferguson
 
DR4907-03GT-190-014
50 kW Compressor Test Rig System Design
Maher El-Moussa
 
DR4907-03GT-190-015
Test Rig Compressor Rotor Preliminary Re-Design for Manufacture
Tyson Ferguson
 
DR4907-03GT-191-001
Determination of Mechanical Layout for a 100 MW Gas Turbine
Ben Lee
 
DR4907-03GT-191-002
Turbine Cooling Flow
Sean Hutchinson
 
DR4907-03GT-191-003
Preliminary Turbine Aerodynamic Design
Shane McDowell
 
DR4907-03GT-191-004
Preliminary Compressor Sizing
Shane McDowell
 

TDR4907-03GT-190-001
Turbonetics Turbocharger Compressor Rotor, 3D Surface Digitization
Hamza Abo El Ella
 
TDR4907-03GT-190-002
Importing BladeGen+ files into CFX-5
Maher El-Moussa
 
TDR4907-03GT-190-004
Compressor: Rotor Preliminary CFX-5 Simulation
Hamza Abo El Ella
 

DR4907-04GT-190-002
Axial Thrust Contribution From The Compressor Back Cavity CFD Prediction
David Hope
 
DR4907-04GT-190-004
Turbine Volute Calculations
Michael Reimer
MISSING
DR4907-04GT-190-005
Turbine Pressure Loss Calculations
Michael Reimer
MISSING
DR4907-04GT-190-006
Compressor Axial Thrust Analysis
David Hope
 
DR4907-04GT-190-007
Turbomachinery Performance Maps
David Hope
 

TDR4907-04GT-190-002
Aeroelastic Analysis of the Compressor and Turbine
Scott Wilson
 
TDR4907-04GT-190-003
Turbine Volute CFD
Michael Reimer
MISSING
TDR4907-04GT-190-004
Generating Turbomachinery Performance Maps with BladeGen
David Hope
 

DR4907-05GT-190-001A
Turbine Volute CFD Analysis: Setting Up and Running the Simulation
Bouria Faqihi
To be used in conjunction with DR4907-05GT-190-002
DR4907-05GT-190-002
Turbine Volute CFD Analysis: Simulation Results Analysis
Bouria Faqihi
To be used in conjunction with DR4907-05GT-190-001A

TDR4907-05GT-190-001
Turbine Volute New Design Method
Bouria Faqihi
 

DR4907-06GT-190-001
Initial Sizing of a Supercritical Carbon Dioxide Axial Compressor
Joshua Brinkerhoff
 
DR4907-06GT-190-002
Preliminary Design of Axial Compressor
Aliasger Abdulkadir
 
DR4907-06GT-190-003
Meanline and Spanwise Design of Supercritical CO2 Turbine
Wendy Cameron
 
DR4907-06GT-190-004
Preliminary Sizing of a Supercritical CO2 Turbine
Darryl Gilbert
 
DR4907-06GT-190-005
BLADE DESIGN FOR A SUPERCRITICAL CARBON DIOXIDE AXIAL COMPRESSOR
Joshua Brinkerhoff
 
DR4907-06GT-190-006
Compressor Blade Design
Joshua Brinkerhoff
 
DR4907-06GT-190-007
DETAILED DESIGN OF A SUPERCRITICAL CO2 Turbine
"Cameron, Wendy"
 
DR4907-06GT-190-008
MEAN LINE PREDICTION FOR TURBINE EFFICIENCY
Darryl Gilbert
 
DR4907-06GT-190-009
VOLUTE DESIGN
Darryl Gilbert
 
DR4907-06GT-190-010
Preliminary Compressor Design using Real Supercritical Carbon Dioxide Properties.
abdulkadir aliasger
 
DR4907-06GT-190-011
CFD analysis of First Stage Rotor and First Stage Stator.
abdulkadir aliasger
 
DR4907-06GT-190-012
Loss Estimation in a 100 MW Axial Compressor
Joshua Brinkerhoff
 
DR4907-06GT-191-001
Nitrogen Expansion Turbin- Determination of Number of Stages and Stage Pressure Ratios
Matthew Ridgway
 
DR4907-06GT-191-002
Nitrogen Expansion Turbine- Determining Optimum Operating Rotational Speed
Matthew Ridgway
 
DR4907-06GT-191-003
Nitrogen Expansion Turbine- Preliminary Geometric RPM
Matthew Ridgway
 
DR4907-06GT-191-004
Preliminary Nitrogen Expansion Turbine Geometry Operating at 3600 RPM
Mark McLaughlin
 
DR4907-06GT-191-005
DESIGN OF THE FOUR-STAGE AXIAL FLOW NITROGEN EXPANSION TURBINE OPERATING AT 3600 RPM
Mark McLaughlin
 

TDR4907-06GT-190-001
Determining the Gas Properties of Supercritical Carbon Dioxide
Joshua Brinkerhoff
 
TDR4907-06GT-190-002
TURBINE BLADE DESIGN METHOD: PRESCRIBED SURFACE-CURVATURE DISTRIBUTION
"Cameron, Wendy"
 
TDR4907-06GT-190-003
Blade Geomety Creation using PRO/E
abdulkadir aliasger
 
TDR4907-06GT-191-001
Turbine MeanLine Design Software Revision C and Testing
Gordon MacIsaac
 
TDR4907-06GT-191-002
Turbine StreamLine Curvature Software Revision A and Testing
Gordon MacIsaac
 
TDR4907-06GT-191-003
NASA Fluid Properties Subroutine Revision A and Data validation
Gordon MacIsaac
 

DR4907-0708-191-001
Preliminary Turbine Design
Daniel McGuire
DR4907-0708-191-002
MEANLINE DESIGN AND PERFORMANCE PREDICTION
Daniel McGuire
DR4907-0708-192-001
Preliminary Design of a Hybrid Axial-Radial Compressor
Patrick Enright
DR4907-0708-192-002
Initial 3D Design of a Combined Axial-Radial Compressor
Patrick Enright
DR4907-0708-193-001
Optimization of Plant Ducting
Andrea Pietila
DR4907-0708-193-002
Optimization of Plant Ducting
Andrea Pietila
Replaces GT4907-0708-193-001
DR4907-0708-193-003
1D Approximation for Volute Sizing
Andrea Pietila
DR4907-0708-193-004
Centrifugal Compressor Pipe Diffuser Design
Andrea Pietila
DR4907-0708-194-001
100MW Plant Journal Bearing Design
Mark Bernans
DR4907-0708-194-002
100MW Plant Journal Bearing Design
Mark Bernans
Replaces GT4907-0708-194-001

TDR4907-0708-191-001
Aerodynamic Feasibility of a Radial Turbine
Daniel McGuire
TDR4907-0708-191-002
MEANLINE DESIGN AND LOSS PREDICTION CODE
Daniel McGuire
TDR4907-0708-191-003
TURBINE BLADE PROFILING PERLIMINARIES
Daniel McGuire
TDR4907-0708-194-003
Stability in Gas Bearings
Mark Bernans
 
DR4907-0809-190-002
Preliminary Axial Compressor CFD Analysis
Kendall MacLean
TDR4907-0809-190-001
Structured Blade Mesh Feasibility
Kendall MacLean
TDR4907-0809-190-002
Compressor CFD Analysis with CFX-11
Kendall MacLean
TDR4907-0809-190-003
Compressor Domain Creation
Kendall MacLean
DR4907-0809-191-001
Creation of a Scaled Compressor Map
Dustin Wywrot
DR4907-0809-191-002
2008-2009 Diffuser Re-design
Dustin Wywrot
DR4907-0809-191-003
Compressor Axial Rotor Blade Re-design
Dustin Wywrot
DR4907-0809-191-004
Overview of Current Compressor Design
Dustin Wywrot
TDR4907-0809-191-001
Preliminary CFD Analysis of a Turbomachinery Blade
Dustin Wywrot
TDR4907-0809-191-002
Use of NIST Tables to Determine Fluid Properties
Dustin Wywrot
DR4907-0809-192-001
2008-2009 Turbine Design Summary
Zi Zhang
TDR4907-0809-192-001
Meanline Profiling and Solid Modelling of Turbine Rotor Blade Using Pro/E
Zi Zhang
TDR4907-0809-192-002
Turbine Stage Temperature and Pressure Estimation
Zi Zhang
TDR4907-0809-192-003
Revised Turbine Stage Temperature and Pressure Estimation and Their Effect on Blade Geometry
Zi Zhang
TDR4907-0809-192-004
Turbine Blade Structural Design Interation
Zi Zhang

DR4907-0910-190-001
2009/10 Turbomachinery Introduction Report
Turbomachinery Group
 
DR4907-0910-191-001
FALL 2009 Overview of CFD
Neil Armstrong
TDR4907-0910-191-001
Computation Fluid Dynamics
Neil Armstrong
 
TDR4907-0910-191-002
Domain Creation
Neil Armstrong
 
TDR4907-0910-191-003
Meshing
Neil Armstrong
 
TDR4907-0910-191-004
CFX-Pre and CFX-Solver
Neil Armstrong
 
TDR4907-0910-191-005
Post-Processing
Neil Armstrong
 
TDR4907-0910-191-006
First Stage Turbine Nozzle CFD Walkthrough
Neil Armstrong
 
DR4907-0910-192-001
Turbine Nozzle Construction for a Two Stage Axial Turbine
Abraham Bach
DR4907-0910-192-002
2009/10 Turbine Design Summary
Abraham Bach
 
TDR4907-0910-192-001
Turbine Blade Profiling: Modifying and Exporting Blade Profiles in PRO/E
Abraham Bach
 
TDR4907-0910-192-002
Turbine Nozzle Design: Avoiding Inlet Shock
Abraham Bach
 
DR4907-0910-193-001
FALL 2009 Work Completed Towards Radial Compressor Stage Design
Jeremy Colbeck
 
DR4907-0910-193-002
Compressor Design Updates: Centrifugal Stage
Jeremy Colbeck
 
TDR4907-0910-193-001
Impeller Hub and Shroud Contour Generator: ContourGT
Jeremy Colbeck
 
TDR4907-0910-193-002
Impeller Meanline Blade Loading Estimation
Jeremy Colbeck
 
TDR4907-0910-193-003
Enabling Automatic Fluid Property Table Lookups in Excel
Jeremy Colbeck
 
DR4907-0910-194-001
Axial Compressor Fluid Properties
Chris Sooriyakumaran
 
DR4907-0910-194-002
Modifications to Axial Compressor 2010
Chris Sooriyakumaran
 
TDR4907-0910-194-001
Creating Airfoils with AIRFOIL_GEN.m
Chris Sooriyakumaran
 
TDR4907-0910-194-002
Modelling Compressor Blades
Chris Sooriyakumaran
 
TDR4907-0910-194-003
Blade Loading Analysis for an Axial Compressor
Chris Sooriyakumaran
 
TDR4907-0910-195-001
Recommendations for CAMLD and CAMLO
Simon Stör
 




TDR4907-1011-191-001
Importing Assembled Models into ANSYS
Matthew Hutichson
 
DR4907-1011-194-001
Preliminary Free Power Turbine Study
Devin O'Brien
 
TDR4907-1011-195-001
Fall 2010 Axial Compressor Analysis
Derek Goyette
 
TDR4907-1011-195-002
Creating Charts in ANSYS CFX-Post
Derek Goyette
 
TDR4907-1011-192-001
Map Network Drives
Colin Johnson
 
TDR4907-1011-193-001
Inserting New Blade Profiles into Pressure Distribution Spreadsheet
Curtis Lee
 
DR4907-1011-193-001
Fall 2010 Diffuser Analysis and Model Redesign
Curtis Lee
 

This page last updated: 14/02/2011