Name
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Title
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Author
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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
|
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DR497-02E-190-006A
|
Compressor: Axial Thrust Estimation
|
Marc Charest
|
|
DR497-02E-190-007A
|
Compressor: Axial Thrust Estimation Using Rigid Body Motion
|
Marc Charest
|
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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
|
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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
|
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DR497-02E-190-016A
|
Turbine Rotor Axial Load Estimation
|
Steve Elia
|
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DR497-02E-190-017A
|
Preliminary Nozzle Design and Loss Estimation
|
Steve Elia
|
|
DR497-02E-190-018A
|
Preliminary Volute Design and Loss Estimation
|
Steve Elia
|
|
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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
|
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DR4907-03GT-190-010
|
Compressor: Volute Design Modification
|
Hamza Abo El Ella
|
|
DR4907-03GT-190-011
|
Compressor: Back Cavity Preliminary CFD Analysis for Axial Thrust Prediction
|
Hamza Abo El Ella
|
|
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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
|
|
DR4907-04GT-190-005
|
Turbine Pressure Loss Calculations
|
Michael Reimer
|
|
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
|
|
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
|
|
DR4907-05GT-190-002
|
Turbine Volute CFD Analysis: Simulation Results Analysis
|
Bouria Faqihi
|
|
|
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
|
|
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
|
|
|
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 |
2010/11 Turbomachinery Introduction Report |
Turbomachinery Group |
| DR4907-0910-191-001 |
FALL 2009 Overview of CFD |
Neil Armstrong |
| TDR4907-0910-191-001 |
Computational 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 CRX-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 Propert Table Lookups in Excel |
Jeremy Colbeck |
| DR4907-0910-194-001 |
Axial Compressor Fluid Properties |
Chris Sooriyakumaran |
| DR4907-0910-194-002 |
Modificatioins 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 |
|