Name
Title
Author
Comments
DR497-02E-260-001A
Final Selection of the Compressor Material
Sausan Khomusi
 
DR497-02E-260-002A
Stress Analysis for the Compressor Rotor
Sauson Khomusi
 
DR497-02E-260-003A
Vibration Modal Analysis for the Compressor Rotor
Sauson Khomusi
 
DR497-02E-260-004A
Stress Analysis
Michael Hildebrand
 
DR497-02E-260-005A
Vibration Modes Analysis
 

TDR497-02E-260-001A
Property Requirements for High Temperature, Stationary Gas Turbines
Michael Hildebrand
 
TDR497-02E-260-002A
Material Considerations for the Compressor Rotor
Sauson Khomusi
 
TDR497-02E-260-003A
Building the 3-D Solid Model of the Compressor
Sauson Khomusi
 
TDR497-02E-260-004A
Importing Bladegen Files into Pro/Engineer
 

DR4907-03GT-260-001
Stress and Temperature Analyses
Shelley Talwar
 
DR4907-03GT-260-002
Structural Evaluation of the Test Rig Compressor (TRC) Rotor
Hugo Leon
 
DR4907-03GT-260-003
Investment Casting Limitations: Test Rig Compressor Manufacturing Issues
Jarett Hunt
 
DR4907-03GT-260-004
3D Turbine Rotor Stress Analysis Including Centrifugal Loads
Shelley Talwar
 
DR4907-03GT-260-005
Turbine Rotor Blade Geometry Modifications and Materials Comparative Analysis
Shelley Talwar
 
DR4907-03GT-260-006
Prototyping And Production
Jarett Hunt
 
DR4907-03GT-261-001
Preliminary Materials Selection for the Turbomachinery
Anne-Marie Bourgeois
 
DR4907-03GT-261-002
Material Selection for the Main Components
Anne-Marie Bourgeois
 

TDR4907-03GT-260-001
Creating a Full or Fractional Rotor Solid Model in Pro/E Wildfire
Hugo Leon
 
TDR4907-03GT-260-002
Simplified Compressor Rotor Fillet Analysis in ProMechanica
Hugo Leon
 
TDR4907-03GT-260-004
3D Stresses Analysis of the Test Rig Compressor (TRC) Rotor using ANSYS
Jarett Hunt
 
TDR4907-03GT-260-005
Stress Analysis Using ANSYS
Shelley Talwar
 
TDR4907-03GT-260-006
Validation of FEA Assumptions for the Test Rig Compressor Structural Evaluation
Hugo Leon
 
TDR4907-03GT-260-007
Validation of FEA Results for the Test Rig Compressor
Hugo Leon
 
TDR4907-03GT-260-008
3D Stresses Analysis of the Test Rig Compressor (TRC) Rotor using ProMechanica
Hugo Leon
 
TDR4907-03GT-260-009
Graphs for Evaluating Test Rig Compressor Gap Clearance
Hugo Leon
 

DR4907-04GT-260-001
Structural Evaluation of the Test Rig Compressor for Revised Blade Geometry
Abby Kenney
 
DR4907-04GT-260-002
Preliminary Conjugate Heat Transfer
Patrick G. Boisvert
 
DR4907-04GT-260-003
Three Dimensional Structural Evaluation of the Turbine Under Centrifugal Loading
Abby Kenney
MISSING
DR4907-04GT-260-004
Preliminary Thermal Stress Analysis of the Turbomachinery Rotors
Abby Kenney
 
DR4907-04GT-261-002
100MW Compressor Layout Concept Evaluation
Brian McAninch
 
DR4907-04GT-261-003
100MW Compressor Intake Design
Brian McAninch
 
DR4907-04GT-261-004
100MW Compressor Stage Design
Brian McAninch
 
DR4907-04GT-261-005
Use of Ceramics in the 100MW Turbine
Patricia Balind
MISSING

TDR4907-04GT-260-001
Step-by-Step Guid to Creating a 2D Profile of a 3D Part in Pro/E
Patrick G. Boisvert
 
TDR4907-04GT-260-002
Step-by-Step Guide to Creating a Preliminary Thermal Distribution Analysis of the Turbomachinery in ANSYS 8.1
Patrick G. Boisvert
 
TDR4907-04GT-260-003
Map and Sweep Meshing Rotary Components Using ANSYS 8.1
Abby Kenney
 
TDR4907-04GT-260-004
Aeroelastic Coupling
Adrian Deutekom, Scott Wilson
Report Number also used by 'Vibration Analysis of Compressor and Turbine' by Adrian Deutekom which is MISSING
TDR4907-04GT-260-005
Procedure for Thermal Stress ANalysis of Rotary Components Using ANSYS 9.0
Abby Kenney
 
TDR4907-04GT-260-006
Aeroelastic Coupling for the Turbine and Compressor
Scott Wilson
MISSING
TDR4907-04GT-260-007
Aeroelastic Analysis of the Compressor and Turbine
Scott Wilson
MISSING
TDR4907-04GT-261-001
Summary of Axial Compressor Theory
Brian McAninch
 

DR4907-05GT-260-001
Structural Evaluation of the Rotary Components
Monika Rostkowska
 

TDR4907-05GT-260-001
Structural Evaluation of Rotating Disk
Monika Rostkowska
 

DR4907-06GT-260-001
PROCEDURE FOR CALCULATING CASING THICKNESS: DISK BURST CONTAINMENT
Saad Guled
 
DR4907-06GT-260-003
TURBINE STRESS ANALYSIS
Saad Guled
 
DR4907-06GT-260-004
TURBINE NOZZLE DESIGN
Saad Guled
 
DR4907-06GT-260-005
MECHANICAL DESIGN AND STRESS ANALYSIS OF THE CO2 100 MWe 1st STAGE COMPRESSOR ROTOR
Joshua Armitage
 
DR4907-06GT-261-001
Preliminary Material Selection for N2 Expansion Turbine
Megan Rasila
 
DR4907-06GT-261-002
Casing Thickness Determination for the Nitrogen Expansion Turbine
Megan Rasila
 
DR4907-06GT-261-006
Preliminary Stress Analysis of the Nitrogen Expansion Turbine First Stage Rotor
Megan Rasila
 

TDR4907-06GT-260-001
An Analytical Strss Analysis of a Compressor Rotor
Joshua Armitage
 
TDR4907-06GT-260-002
THE PROCEDURE FOR A STRESS ANALYSIS ON A ROTATING COMPONENT USING ANSYS WORKBENCH
Joshua Armitage
 
TDR4907-06GT-261-001
METHODS OF ATTACHMENT FOR TURBINE BLADES TO DISKS, DISKS TO SHAFT AND SHAFT TO GENERATOR
Megan Rasila
 

DR4907-0708-261-001
Design Requirements for S-CO2 Compressor
Parichit Bagga
DR4907-0708-261-002
Feasibility assessment for the radial stage of the SCO2 compressor
Parichit Bagga
DR4907-0708-261-003
Conceptual Detail Design of the Compressor assembly
Parichit Bagga
DR4907-0708-261-004
Preliminary Design & FEA of 2007-2008 Compressor Stators
Parichit Bagga
DR4907-0708-261-005
FEA Results of 2007-2008 Compressor Rotors
Parichit Bagga
DR4907-0708-261-006
Revised Design Requirements for the S-CO2 Compressor
Parichit Bagga
DR4907-0708-261-007
Recommendations for 2008-2009 Compressor Structural Design
Parichit Bagga
DR4907-0708-262-001
Structural feasibility of a radial turbine for the S-CO2 plant
Nazim Ould-Brahim
DR4907-0708-262-002
Design requirements of the Turbine of the S-CO2 plant
Nazim Ould-Brahim
DR4907-0708-262-003
Design requirements of the Turbine of the S-CO2 plant
Nazim Ould-Brahim
replaces DR4907-0708-262-002
DR4907-0708-262-004
Preliminary Design of the Axial Turbine Assembly for the S-CO2 Plant
Nazim Ould-Brahim
DR4907-0708-262-005
Analytical and Preliminary FEA Analysis of the Turbine Rotors for the S-CO2 Plant
Nazim Ould-Brahim
DR4907-0708-262-006
Recommendations for Future Work on the Structural Aspects of the Turbine for the S-CO2 Plant
Nazim Ould-Brahim
DR4907-0708-263-001
Shaft Design Requirements
Ben Blackman
DR4907-0708-263-002
Preliminary Shaft Design and Deflection Analysis
Ben Blackman
DR4907-0708-263-003
Coupling Selection for Supercritical CO2 Plant
Ben Blackman
DR4907-0708-263-004
Lateral Vibrations Analysis of CO2 Turbomachinery
Ben Blackman
DR4907-0708-263-005
Preliminary Torsional Vibrations Analysis of CO2 Turbomachinery
Ben Blackman
DR4907-0708-263-006
Torsional Vibrations Case Study using ANSYS
Ben Blackman
DR4907-0708-263-007
Shaft Recommendations
Ben Blackman
DR4907-0708-264-001
INL Supercritical CO2 INCONEL Alloy Corrosion Testing Summary
Ryan Petrusenko
DR4907-0708-264-002
Preliminary Design of a S-CO2 Corrosion Test Rig
Ryan Petrusenko
DR4907-0708-264-003
Intermediate Design of a S-CO2 Corrosion Test Rig
Ryan Petrusenko
DR4907-0708-264-004
Stress Analysis of the Turbine Inlet Pipe Section (Pipe 4)
Ryan Petrusenko
DR4907-0708-264-005
Materials Recommendations for the 2008-09 Academic Year
Ryan Petrusenko

TDR4907-0708-262-001
Disk Stress Analysis Tool
Nazim Ould-Brahim
TDR4907-0708-264-001
Thermal and Pressure Loading of a Straight-Section Pipe
Ryan Petrusenko
 

DR4907-0910-260-001
Start Here
Structures Team
 
DR4907-0910-261-001
Bladed Disk Compressor Design
Charles Cholette
 
DR4907-0910-261-002
Compressor Assembly Design
Charles Cholette
 
TDR4907-0910-261-001
Thrust Loading
Charles Cholette
 
DR4907-0910-263-001
Stator Blade Preliminary Modelling
Justin Hawkins
 
DR4907-0910-263-002
Axial Turbomachinery Component Structural Analysis Results
Justin Hawkins
 
TDR4907-0910-263-001
Structural Analysis Method of Axial Turbomachinery Components
Justin Hawkins
 
TDR4907-0910-264-001
ANSYS Tutorial
Beat Riedener
 
TDR4907-0910-264-002
Radial Compressor Modifications
Beat Riedener
 
TDR4907-0910-264-003
Implementation of Momentum Loading
Beat Riedener
 
TDR4907-0910-264-004
Torsional Vibrations
Beat Riedener
 
This page last updated: 13/04/2010