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You searched for subject:(turbomachinery). Showing records 1 – 30 of 234 total matches.

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Dalhousie University

1. Dodsworth, Laura. Operational Parametric Study of a Prototype Tesla Pump.

Degree: Master of Applied Science, Department of Mechanical Engineering, 2016, Dalhousie University

 A parametric study of a prototype Tesla pump was performed for various disk pack spacings and rotational speeds. The 15 thou spacing was the most… (more)

Subjects/Keywords: turbomachinery; fluid mechanics; Tesla pump

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APA (6th Edition):

Dodsworth, L. (2016). Operational Parametric Study of a Prototype Tesla Pump. (Masters Thesis). Dalhousie University. Retrieved from http://hdl.handle.net/10222/71602

Chicago Manual of Style (16th Edition):

Dodsworth, Laura. “Operational Parametric Study of a Prototype Tesla Pump.” 2016. Masters Thesis, Dalhousie University. Accessed July 05, 2020. http://hdl.handle.net/10222/71602.

MLA Handbook (7th Edition):

Dodsworth, Laura. “Operational Parametric Study of a Prototype Tesla Pump.” 2016. Web. 05 Jul 2020.

Vancouver:

Dodsworth L. Operational Parametric Study of a Prototype Tesla Pump. [Internet] [Masters thesis]. Dalhousie University; 2016. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10222/71602.

Council of Science Editors:

Dodsworth L. Operational Parametric Study of a Prototype Tesla Pump. [Masters Thesis]. Dalhousie University; 2016. Available from: http://hdl.handle.net/10222/71602


The Ohio State University

2. Giuliani, James Edward. Jet Engine Fan Response to Inlet Distortions Generated by Ingesting Boundary Layer Flow.

Degree: PhD, Aero/Astro Engineering, 2016, The Ohio State University

 Future civil transport designs may incorporate engines integrated into the body of the aircraft to take advantage of efficiency increases due to weight and drag… (more)

Subjects/Keywords: Aerospace Engineering; turbomachinery; CFD; inlets

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APA (6th Edition):

Giuliani, J. E. (2016). Jet Engine Fan Response to Inlet Distortions Generated by Ingesting Boundary Layer Flow. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1468564279

Chicago Manual of Style (16th Edition):

Giuliani, James Edward. “Jet Engine Fan Response to Inlet Distortions Generated by Ingesting Boundary Layer Flow.” 2016. Doctoral Dissertation, The Ohio State University. Accessed July 05, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1468564279.

MLA Handbook (7th Edition):

Giuliani, James Edward. “Jet Engine Fan Response to Inlet Distortions Generated by Ingesting Boundary Layer Flow.” 2016. Web. 05 Jul 2020.

Vancouver:

Giuliani JE. Jet Engine Fan Response to Inlet Distortions Generated by Ingesting Boundary Layer Flow. [Internet] [Doctoral dissertation]. The Ohio State University; 2016. [cited 2020 Jul 05]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1468564279.

Council of Science Editors:

Giuliani JE. Jet Engine Fan Response to Inlet Distortions Generated by Ingesting Boundary Layer Flow. [Doctoral Dissertation]. The Ohio State University; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1468564279


Texas A&M University

3. Gamal Eldin, Ahmed Mohamed. Leakage and rotordynamic effects of pocket damper seals and see-through labyrinth seals.

Degree: 2009, Texas A&M University

 This dissertation discusses research on the leakage and rotordynamic characteristics of pocket damper seals (PDS) and see-through labyrinth seals, presents and evaluates models for labyrinth… (more)

Subjects/Keywords: Turbomachinery; Rotordynamics; Leakage; Seals

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APA (6th Edition):

Gamal Eldin, A. M. (2009). Leakage and rotordynamic effects of pocket damper seals and see-through labyrinth seals. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2084

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Gamal Eldin, Ahmed Mohamed. “Leakage and rotordynamic effects of pocket damper seals and see-through labyrinth seals.” 2009. Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2084.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Gamal Eldin, Ahmed Mohamed. “Leakage and rotordynamic effects of pocket damper seals and see-through labyrinth seals.” 2009. Web. 05 Jul 2020.

Vancouver:

Gamal Eldin AM. Leakage and rotordynamic effects of pocket damper seals and see-through labyrinth seals. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2084.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Gamal Eldin AM. Leakage and rotordynamic effects of pocket damper seals and see-through labyrinth seals. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2084

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Texas A&M University

4. Kim, Tae Ho. Analysis of side end pressurized bump type gas foil bearings: a model anchored to test data.

Degree: 2009, Texas A&M University

 Comprehensive modeling of gas foil bearings (GFBs) anchored to reliable test data will enable the widespread usage of GFBs into novel turbomachinery applications, such as… (more)

Subjects/Keywords: Gas Foil Bearing; Turbomachinery; Rotordynamics

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APA (6th Edition):

Kim, T. H. (2009). Analysis of side end pressurized bump type gas foil bearings: a model anchored to test data. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2088

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Kim, Tae Ho. “Analysis of side end pressurized bump type gas foil bearings: a model anchored to test data.” 2009. Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2088.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Kim, Tae Ho. “Analysis of side end pressurized bump type gas foil bearings: a model anchored to test data.” 2009. Web. 05 Jul 2020.

Vancouver:

Kim TH. Analysis of side end pressurized bump type gas foil bearings: a model anchored to test data. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2088.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Kim TH. Analysis of side end pressurized bump type gas foil bearings: a model anchored to test data. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2088

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Texas A&M University

5. Niu, Yaying. Dynamic Response of a Rotor-air Bearing System Due to Base Induced Periodic Motions.

Degree: 2010, Texas A&M University

 Oil-free microturbomachinery (MTM) are inevitably subjected to base or foundation excitations: multiple periodic load excitations from internal combustion (IC) engines in turbochargers, for example. Too… (more)

Subjects/Keywords: Gas bearing; Turbomachinery; Base excitation

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APA (6th Edition):

Niu, Y. (2010). Dynamic Response of a Rotor-air Bearing System Due to Base Induced Periodic Motions. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7025

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Niu, Yaying. “Dynamic Response of a Rotor-air Bearing System Due to Base Induced Periodic Motions.” 2010. Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7025.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Niu, Yaying. “Dynamic Response of a Rotor-air Bearing System Due to Base Induced Periodic Motions.” 2010. Web. 05 Jul 2020.

Vancouver:

Niu Y. Dynamic Response of a Rotor-air Bearing System Due to Base Induced Periodic Motions. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7025.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Niu Y. Dynamic Response of a Rotor-air Bearing System Due to Base Induced Periodic Motions. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7025

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Texas A&M University

6. Rasmy Marsis, Emanuel 1983-. CFD Simulation and Experimental Testing of Multiphase Flow Inside the MVP Electrical Submersible Pump.

Degree: 2012, Texas A&M University

 The MVP is a special type of Electrical Submersible Pumps (ESPs) manufactured by Baker Hughes, model no. G470, and is capable of handling multiphase flow… (more)

Subjects/Keywords: Turbomachinery; CFD; Multiphase; ESP; MVP

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APA (6th Edition):

Rasmy Marsis, E. 1. (2012). CFD Simulation and Experimental Testing of Multiphase Flow Inside the MVP Electrical Submersible Pump. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148052

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Rasmy Marsis, Emanuel 1983-. “CFD Simulation and Experimental Testing of Multiphase Flow Inside the MVP Electrical Submersible Pump.” 2012. Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/148052.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Rasmy Marsis, Emanuel 1983-. “CFD Simulation and Experimental Testing of Multiphase Flow Inside the MVP Electrical Submersible Pump.” 2012. Web. 05 Jul 2020.

Vancouver:

Rasmy Marsis E1. CFD Simulation and Experimental Testing of Multiphase Flow Inside the MVP Electrical Submersible Pump. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/148052.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Rasmy Marsis E1. CFD Simulation and Experimental Testing of Multiphase Flow Inside the MVP Electrical Submersible Pump. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148052

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Texas A&M University

7. Abdelfattah, Sherif Alykadry. Numerical and Experimental Analysis of Multi-Stage Axial Turbine Performance at Design and Off-Design Conditions.

Degree: 2013, Texas A&M University

 Computational fluid dynamics or CFD isan importanttool thatis used at various stages in the design of highly complex turbomachinery such as compressorand turbine stages that… (more)

Subjects/Keywords: Turbomachinery; CFD; Secondary Flows; Turbines

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APA (6th Edition):

Abdelfattah, S. A. (2013). Numerical and Experimental Analysis of Multi-Stage Axial Turbine Performance at Design and Off-Design Conditions. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151083

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Abdelfattah, Sherif Alykadry. “Numerical and Experimental Analysis of Multi-Stage Axial Turbine Performance at Design and Off-Design Conditions.” 2013. Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/151083.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Abdelfattah, Sherif Alykadry. “Numerical and Experimental Analysis of Multi-Stage Axial Turbine Performance at Design and Off-Design Conditions.” 2013. Web. 05 Jul 2020.

Vancouver:

Abdelfattah SA. Numerical and Experimental Analysis of Multi-Stage Axial Turbine Performance at Design and Off-Design Conditions. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/151083.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Abdelfattah SA. Numerical and Experimental Analysis of Multi-Stage Axial Turbine Performance at Design and Off-Design Conditions. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151083

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Purdue University

8. Dolan, Matthew. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations.

Degree: MSME, Mechanical Engineering, 2015, Purdue University

Dolan, Matthew P. M.S.M.E., Purdue University, August 2015. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. Major Professor: Dr. Nicole L. Key, School of Mechanical Engineering. Advisors/Committee Members: Nicole L Key, Steven Wereley, Sameer Naik.

Subjects/Keywords: Aerodynamics; Centrifugal Compressor; Facility; Turbomachinery

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APA (6th Edition):

Dolan, M. (2015). Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/1105

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Dolan, Matthew. “Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations.” 2015. Thesis, Purdue University. Accessed July 05, 2020. https://docs.lib.purdue.edu/open_access_theses/1105.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Dolan, Matthew. “Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations.” 2015. Web. 05 Jul 2020.

Vancouver:

Dolan M. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. [Internet] [Thesis]. Purdue University; 2015. [cited 2020 Jul 05]. Available from: https://docs.lib.purdue.edu/open_access_theses/1105.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Dolan M. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. [Thesis]. Purdue University; 2015. Available from: https://docs.lib.purdue.edu/open_access_theses/1105

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Cincinnati

9. GUIDOTTI, EMANUELE. Analysis of the Unsteady Flow in an Aspirated Counter-Rotating Compressor Using the Nonlinear Harmonic Balance Method.

Degree: MS, Engineering : Aerospace Engineering, 2008, University of Cincinnati

 A multistage frequency domain (nonlinear harmonic) Navier-Stokes unsteady flow solver has been used to analyze the flow field in the MIT (rotor/rotor) counter-rotating compressor. The… (more)

Subjects/Keywords: Energy; cfd; turbomachinery; harmonic balance

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APA (6th Edition):

GUIDOTTI, E. (2008). Analysis of the Unsteady Flow in an Aspirated Counter-Rotating Compressor Using the Nonlinear Harmonic Balance Method. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1218690946

Chicago Manual of Style (16th Edition):

GUIDOTTI, EMANUELE. “Analysis of the Unsteady Flow in an Aspirated Counter-Rotating Compressor Using the Nonlinear Harmonic Balance Method.” 2008. Masters Thesis, University of Cincinnati. Accessed July 05, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1218690946.

MLA Handbook (7th Edition):

GUIDOTTI, EMANUELE. “Analysis of the Unsteady Flow in an Aspirated Counter-Rotating Compressor Using the Nonlinear Harmonic Balance Method.” 2008. Web. 05 Jul 2020.

Vancouver:

GUIDOTTI E. Analysis of the Unsteady Flow in an Aspirated Counter-Rotating Compressor Using the Nonlinear Harmonic Balance Method. [Internet] [Masters thesis]. University of Cincinnati; 2008. [cited 2020 Jul 05]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1218690946.

Council of Science Editors:

GUIDOTTI E. Analysis of the Unsteady Flow in an Aspirated Counter-Rotating Compressor Using the Nonlinear Harmonic Balance Method. [Masters Thesis]. University of Cincinnati; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1218690946


University of Ottawa

10. Smith, Craig I. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance .

Degree: 2010, University of Ottawa

 The temperature of the flow entering a high-pressure turbine stage is inherently non-uniform, as it is produced by several discrete, azimuthally-distributed combustors. In general, however,… (more)

Subjects/Keywords: hot streak; turbomachinery; turbine

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APA (6th Edition):

Smith, C. I. (2010). Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . (Thesis). University of Ottawa. Retrieved from http://hdl.handle.net/10393/19660

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Smith, Craig I. “Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance .” 2010. Thesis, University of Ottawa. Accessed July 05, 2020. http://hdl.handle.net/10393/19660.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Smith, Craig I. “Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance .” 2010. Web. 05 Jul 2020.

Vancouver:

Smith CI. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . [Internet] [Thesis]. University of Ottawa; 2010. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10393/19660.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Smith CI. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . [Thesis]. University of Ottawa; 2010. Available from: http://hdl.handle.net/10393/19660

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Texas A&M University

11. Den, Sean. Analysis of Force Coefficients and Dynamic Pressures for Short-Length (L/D=0.2) Open-Ends Squeeze Film Dampers.

Degree: MS, Mechanical Engineering, 2015, Texas A&M University

 Gas turbine engine manufacturers push for increasingly simpler squeeze film damper (SFD) designs that can still provide necessary damping to suppress rotor vibrations and offer… (more)

Subjects/Keywords: Turbomachinery; Rotordynamics; SFD; Vibration; Bearing

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APA (6th Edition):

Den, S. (2015). Analysis of Force Coefficients and Dynamic Pressures for Short-Length (L/D=0.2) Open-Ends Squeeze Film Dampers. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/174215

Chicago Manual of Style (16th Edition):

Den, Sean. “Analysis of Force Coefficients and Dynamic Pressures for Short-Length (L/D=0.2) Open-Ends Squeeze Film Dampers.” 2015. Masters Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/174215.

MLA Handbook (7th Edition):

Den, Sean. “Analysis of Force Coefficients and Dynamic Pressures for Short-Length (L/D=0.2) Open-Ends Squeeze Film Dampers.” 2015. Web. 05 Jul 2020.

Vancouver:

Den S. Analysis of Force Coefficients and Dynamic Pressures for Short-Length (L/D=0.2) Open-Ends Squeeze Film Dampers. [Internet] [Masters thesis]. Texas A&M University; 2015. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/174215.

Council of Science Editors:

Den S. Analysis of Force Coefficients and Dynamic Pressures for Short-Length (L/D=0.2) Open-Ends Squeeze Film Dampers. [Masters Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/174215

12. Schreiber, Christoph. Inlet Recirculation in Radial Compressors.

Degree: PhD, 2018, University of Cambridge

 Deficient performances of turbocharger compressors inside turbo-charged engines limit the behaviour of the drive train. This problem has shifted the design space for compressors towards… (more)

Subjects/Keywords: Turbomachinery; Radial Compressor; Inlet Recirculation

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APA (6th Edition):

Schreiber, C. (2018). Inlet Recirculation in Radial Compressors. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/270611

Chicago Manual of Style (16th Edition):

Schreiber, Christoph. “Inlet Recirculation in Radial Compressors.” 2018. Doctoral Dissertation, University of Cambridge. Accessed July 05, 2020. https://www.repository.cam.ac.uk/handle/1810/270611.

MLA Handbook (7th Edition):

Schreiber, Christoph. “Inlet Recirculation in Radial Compressors.” 2018. Web. 05 Jul 2020.

Vancouver:

Schreiber C. Inlet Recirculation in Radial Compressors. [Internet] [Doctoral dissertation]. University of Cambridge; 2018. [cited 2020 Jul 05]. Available from: https://www.repository.cam.ac.uk/handle/1810/270611.

Council of Science Editors:

Schreiber C. Inlet Recirculation in Radial Compressors. [Doctoral Dissertation]. University of Cambridge; 2018. Available from: https://www.repository.cam.ac.uk/handle/1810/270611


Texas A&M University

13. Carpenter IV, Forrest Lafon. Practical Aspects of Computational Fluid Dynamics for Turbomachinery.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 The following dissertation examines several aspects of numerical simulations for turbomachinery flows modeled with an in-house Reynolds-averaged Navier-Stokes solver. The impact of the turbulence model… (more)

Subjects/Keywords: Computational Fluid Dynamcs; Turbomachinery

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APA (6th Edition):

Carpenter IV, F. L. (2016). Practical Aspects of Computational Fluid Dynamics for Turbomachinery. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158055

Chicago Manual of Style (16th Edition):

Carpenter IV, Forrest Lafon. “Practical Aspects of Computational Fluid Dynamics for Turbomachinery.” 2016. Doctoral Dissertation, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/158055.

MLA Handbook (7th Edition):

Carpenter IV, Forrest Lafon. “Practical Aspects of Computational Fluid Dynamics for Turbomachinery.” 2016. Web. 05 Jul 2020.

Vancouver:

Carpenter IV FL. Practical Aspects of Computational Fluid Dynamics for Turbomachinery. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/158055.

Council of Science Editors:

Carpenter IV FL. Practical Aspects of Computational Fluid Dynamics for Turbomachinery. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158055


Texas A&M University

14. Gary, Keith William. Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals.

Degree: MS, Mechanical Engineering, 2017, Texas A&M University

 Annular-labyrinth seals restrict leakage in turbomachinery but may provide unwanted destabilizing forces. This work provides measurements of an interlockinglabyrinth gas seal to further the understanding… (more)

Subjects/Keywords: Rotordynamics; Turbomachinery; Labyrinth gas seals

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APA (6th Edition):

Gary, K. W. (2017). Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/169567

Chicago Manual of Style (16th Edition):

Gary, Keith William. “Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals.” 2017. Masters Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/169567.

MLA Handbook (7th Edition):

Gary, Keith William. “Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals.” 2017. Web. 05 Jul 2020.

Vancouver:

Gary KW. Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/169567.

Council of Science Editors:

Gary KW. Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/169567


Cranfield University

15. Attia, Osama Abdel Moniem Mohamied. Finite element static, dynamic, and flutter analysis of rotating composite layered plates and shells.

Degree: PhD, 1996, Cranfield University

 This thesis introduces new conforming and non-conforming finite elements for the static and dynamic analysis of rotating composite layered plates and shells. The elements consider… (more)

Subjects/Keywords: 621.4352; Turbomachinery

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APA (6th Edition):

Attia, O. A. M. M. (1996). Finite element static, dynamic, and flutter analysis of rotating composite layered plates and shells. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/4052 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309622

Chicago Manual of Style (16th Edition):

Attia, Osama Abdel Moniem Mohamied. “Finite element static, dynamic, and flutter analysis of rotating composite layered plates and shells.” 1996. Doctoral Dissertation, Cranfield University. Accessed July 05, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/4052 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309622.

MLA Handbook (7th Edition):

Attia, Osama Abdel Moniem Mohamied. “Finite element static, dynamic, and flutter analysis of rotating composite layered plates and shells.” 1996. Web. 05 Jul 2020.

Vancouver:

Attia OAMM. Finite element static, dynamic, and flutter analysis of rotating composite layered plates and shells. [Internet] [Doctoral dissertation]. Cranfield University; 1996. [cited 2020 Jul 05]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/4052 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309622.

Council of Science Editors:

Attia OAMM. Finite element static, dynamic, and flutter analysis of rotating composite layered plates and shells. [Doctoral Dissertation]. Cranfield University; 1996. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/4052 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309622

16. Hillary, Brenda. Indirect measurement of vibration excitation forces.

Degree: PhD, 1983, Imperial College London

Subjects/Keywords: 534; Turbomachinery

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APA (6th Edition):

Hillary, B. (1983). Indirect measurement of vibration excitation forces. (Doctoral Dissertation). Imperial College London. Retrieved from http://hdl.handle.net/10044/1/8450

Chicago Manual of Style (16th Edition):

Hillary, Brenda. “Indirect measurement of vibration excitation forces.” 1983. Doctoral Dissertation, Imperial College London. Accessed July 05, 2020. http://hdl.handle.net/10044/1/8450.

MLA Handbook (7th Edition):

Hillary, Brenda. “Indirect measurement of vibration excitation forces.” 1983. Web. 05 Jul 2020.

Vancouver:

Hillary B. Indirect measurement of vibration excitation forces. [Internet] [Doctoral dissertation]. Imperial College London; 1983. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10044/1/8450.

Council of Science Editors:

Hillary B. Indirect measurement of vibration excitation forces. [Doctoral Dissertation]. Imperial College London; 1983. Available from: http://hdl.handle.net/10044/1/8450


Texas A&M University

17. Creary, Andron. MANUFACTURING OF A GAS FOIL BEARINGS FOR PALMED-SIZED TURBOMACHINERY.

Degree: 2010, Texas A&M University

 Compliant Air Foil Bearings are used in a wide variety of applications. The versatility, ease of manufacture, and low cost of foil bearings are a… (more)

Subjects/Keywords: gas foil bearings; LIGA; microfabrication; turbomachinery

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APA (6th Edition):

Creary, A. (2010). MANUFACTURING OF A GAS FOIL BEARINGS FOR PALMED-SIZED TURBOMACHINERY. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-245

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Creary, Andron. “MANUFACTURING OF A GAS FOIL BEARINGS FOR PALMED-SIZED TURBOMACHINERY.” 2010. Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-245.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Creary, Andron. “MANUFACTURING OF A GAS FOIL BEARINGS FOR PALMED-SIZED TURBOMACHINERY.” 2010. Web. 05 Jul 2020.

Vancouver:

Creary A. MANUFACTURING OF A GAS FOIL BEARINGS FOR PALMED-SIZED TURBOMACHINERY. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-245.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Creary A. MANUFACTURING OF A GAS FOIL BEARINGS FOR PALMED-SIZED TURBOMACHINERY. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-245

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Texas A&M University

18. Johnson, Shalom. Development of a Pulse Modulator for Active Flow Control in Turbomachinery.

Degree: 2011, Texas A&M University

 In todays highly maneuverable jet aircraft designs, aircraft are required to have a propulsion system that can operate during sudden accelerations and rapid changes in… (more)

Subjects/Keywords: stall suppression; Turbomachinery; axial compressor; oscillatory blowing

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APA (6th Edition):

Johnson, S. (2011). Development of a Pulse Modulator for Active Flow Control in Turbomachinery. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Johnson, Shalom. “Development of a Pulse Modulator for Active Flow Control in Turbomachinery.” 2011. Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Johnson, Shalom. “Development of a Pulse Modulator for Active Flow Control in Turbomachinery.” 2011. Web. 05 Jul 2020.

Vancouver:

Johnson S. Development of a Pulse Modulator for Active Flow Control in Turbomachinery. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Johnson S. Development of a Pulse Modulator for Active Flow Control in Turbomachinery. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

19. Joly, Michael Marie. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.

Degree: 2014, Texas A&M University

 Research on high-speed air-breathing propulsion aims at developing aircraft with antipodal range and space access. Before reaching high speed at high altitude, the flight vehicle… (more)

Subjects/Keywords: Turbomachinery; Optimization

Turbomachinery for high-speed propulsion 1.1.1 Air turbo rocket from take-off to scramjet operation… …critical in high-pressure turbomachinery components. Strong shock waves impingements on… …high-pressure turbomachinery require multi-disciplinary approaches, where both aerodynamics… …ciplinary Design Optimization (MDO) suitable for turbomachinery applications is proposed… …in this section. 1.2.1 Computational fluid dynamics Turbomachinery high-speed stages… 

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APA (6th Edition):

Joly, M. M. (2014). Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153360

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Joly, Michael Marie. “Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.” 2014. Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/153360.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Joly, Michael Marie. “Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.” 2014. Web. 05 Jul 2020.

Vancouver:

Joly MM. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/153360.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Joly MM. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153360

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Cincinnati

20. Szabo, Istvan. A Numerical Study of Water Injection on Transonic Compressor Rotor Performance.

Degree: PhD, Engineering : Aerospace Engineering, 2008, University of Cincinnati

 In this study, numerical simulations of two-phase flow in a transonic compressor rotor (NASA Rotor 37) were performed. Both flow and droplets governing equations were… (more)

Subjects/Keywords: Engineering; multiphase; compressor; turbomachinery; fogging; injection

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APA (6th Edition):

Szabo, I. (2008). A Numerical Study of Water Injection on Transonic Compressor Rotor Performance. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1212107404

Chicago Manual of Style (16th Edition):

Szabo, Istvan. “A Numerical Study of Water Injection on Transonic Compressor Rotor Performance.” 2008. Doctoral Dissertation, University of Cincinnati. Accessed July 05, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1212107404.

MLA Handbook (7th Edition):

Szabo, Istvan. “A Numerical Study of Water Injection on Transonic Compressor Rotor Performance.” 2008. Web. 05 Jul 2020.

Vancouver:

Szabo I. A Numerical Study of Water Injection on Transonic Compressor Rotor Performance. [Internet] [Doctoral dissertation]. University of Cincinnati; 2008. [cited 2020 Jul 05]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1212107404.

Council of Science Editors:

Szabo I. A Numerical Study of Water Injection on Transonic Compressor Rotor Performance. [Doctoral Dissertation]. University of Cincinnati; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1212107404


Virginia Tech

21. Reagle, Colin James. Technique for Measuring the Coefficient of Restitution for Microparticle Sand Impacts at High Temperature for Turbomachinery Applications.

Degree: PhD, Mechanical Engineering, 2012, Virginia Tech

 Erosion and deposition in gas turbine engines are functions of particle/wall interactions and the Coefficient of Restitution (COR) is a fundamental property of these interactions.… (more)

Subjects/Keywords: Impact; Turbomachinery; Microparticle; Coefficient of Restitution

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APA (6th Edition):

Reagle, C. J. (2012). Technique for Measuring the Coefficient of Restitution for Microparticle Sand Impacts at High Temperature for Turbomachinery Applications. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28875

Chicago Manual of Style (16th Edition):

Reagle, Colin James. “Technique for Measuring the Coefficient of Restitution for Microparticle Sand Impacts at High Temperature for Turbomachinery Applications.” 2012. Doctoral Dissertation, Virginia Tech. Accessed July 05, 2020. http://hdl.handle.net/10919/28875.

MLA Handbook (7th Edition):

Reagle, Colin James. “Technique for Measuring the Coefficient of Restitution for Microparticle Sand Impacts at High Temperature for Turbomachinery Applications.” 2012. Web. 05 Jul 2020.

Vancouver:

Reagle CJ. Technique for Measuring the Coefficient of Restitution for Microparticle Sand Impacts at High Temperature for Turbomachinery Applications. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10919/28875.

Council of Science Editors:

Reagle CJ. Technique for Measuring the Coefficient of Restitution for Microparticle Sand Impacts at High Temperature for Turbomachinery Applications. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/28875


Oklahoma State University

22. Davey, Mark Willis. Influence of Axial Spacing on Spanwise Efficiency of a Transonic Axial Compressor Rotor Stage.

Degree: Mechanical & Aerospace Engineering, 2004, Oklahoma State University

 This study numerically examined the span-wise efficiency of a transonic compressor stage representative of a modern jet engine. Two simulations of a compressor stage with… (more)

Subjects/Keywords: turbomachinery; axial spacing

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APA (6th Edition):

Davey, M. W. (2004). Influence of Axial Spacing on Spanwise Efficiency of a Transonic Axial Compressor Rotor Stage. (Thesis). Oklahoma State University. Retrieved from http://hdl.handle.net/11244/9920

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Davey, Mark Willis. “Influence of Axial Spacing on Spanwise Efficiency of a Transonic Axial Compressor Rotor Stage.” 2004. Thesis, Oklahoma State University. Accessed July 05, 2020. http://hdl.handle.net/11244/9920.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Davey, Mark Willis. “Influence of Axial Spacing on Spanwise Efficiency of a Transonic Axial Compressor Rotor Stage.” 2004. Web. 05 Jul 2020.

Vancouver:

Davey MW. Influence of Axial Spacing on Spanwise Efficiency of a Transonic Axial Compressor Rotor Stage. [Internet] [Thesis]. Oklahoma State University; 2004. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/11244/9920.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Davey MW. Influence of Axial Spacing on Spanwise Efficiency of a Transonic Axial Compressor Rotor Stage. [Thesis]. Oklahoma State University; 2004. Available from: http://hdl.handle.net/11244/9920

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Cambridge

23. Perovic, Dusan. Distortion Tolerant Fan Design.

Degree: PhD, 2019, University of Cambridge

 Boundary Layer Ingestion (BLI) technology could achieve a fuel burn reduction of up to 15%. However, the fans need to operate in severely distorted flow,… (more)

Subjects/Keywords: Boundary Layer Ingestion; BLI; Turbomachinery; Fans

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APA (6th Edition):

Perovic, D. (2019). Distortion Tolerant Fan Design. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/292447

Chicago Manual of Style (16th Edition):

Perovic, Dusan. “Distortion Tolerant Fan Design.” 2019. Doctoral Dissertation, University of Cambridge. Accessed July 05, 2020. https://www.repository.cam.ac.uk/handle/1810/292447.

MLA Handbook (7th Edition):

Perovic, Dusan. “Distortion Tolerant Fan Design.” 2019. Web. 05 Jul 2020.

Vancouver:

Perovic D. Distortion Tolerant Fan Design. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2020 Jul 05]. Available from: https://www.repository.cam.ac.uk/handle/1810/292447.

Council of Science Editors:

Perovic D. Distortion Tolerant Fan Design. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/292447


Texas A&M University

24. Ramirez Alanis, Mauricio Alan. Development and Validation of Test Rig for Measurements of Leakage and Rotordynamic Performance of Interlocking Gas Labyrinth Seals.

Degree: MS, Mechanical Engineering, 2017, Texas A&M University

 Understanding the rotordynamic and leakage characteristics of gas annular seals is important for the design of efficient and reliable turbomachinery. This work sets the foundation… (more)

Subjects/Keywords: Rotordynamic; Magnetic Bearings; Seals; Interlocking; Labyrinth; Turbomachinery

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APA (6th Edition):

Ramirez Alanis, M. A. (2017). Development and Validation of Test Rig for Measurements of Leakage and Rotordynamic Performance of Interlocking Gas Labyrinth Seals. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/169653

Chicago Manual of Style (16th Edition):

Ramirez Alanis, Mauricio Alan. “Development and Validation of Test Rig for Measurements of Leakage and Rotordynamic Performance of Interlocking Gas Labyrinth Seals.” 2017. Masters Thesis, Texas A&M University. Accessed July 05, 2020. http://hdl.handle.net/1969.1/169653.

MLA Handbook (7th Edition):

Ramirez Alanis, Mauricio Alan. “Development and Validation of Test Rig for Measurements of Leakage and Rotordynamic Performance of Interlocking Gas Labyrinth Seals.” 2017. Web. 05 Jul 2020.

Vancouver:

Ramirez Alanis MA. Development and Validation of Test Rig for Measurements of Leakage and Rotordynamic Performance of Interlocking Gas Labyrinth Seals. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/1969.1/169653.

Council of Science Editors:

Ramirez Alanis MA. Development and Validation of Test Rig for Measurements of Leakage and Rotordynamic Performance of Interlocking Gas Labyrinth Seals. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/169653


KTH

25. Zhuang, Qingyuan. Parametric Study on the Aeroelastic Stability of Rotor Seals.

Degree: Heat and Power Technology, 2012, KTH

  Labyrinth seals are widely used in rotating machinery and have been shown to experience aeroelastic instabilities. The rapid development of computational fluid dynamics now… (more)

Subjects/Keywords: Aeromechanics; turbomachinery; labyrinth seal; flutter; CFD; FEM

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APA (6th Edition):

Zhuang, Q. (2012). Parametric Study on the Aeroelastic Stability of Rotor Seals. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-116689

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Zhuang, Qingyuan. “Parametric Study on the Aeroelastic Stability of Rotor Seals.” 2012. Thesis, KTH. Accessed July 05, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-116689.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Zhuang, Qingyuan. “Parametric Study on the Aeroelastic Stability of Rotor Seals.” 2012. Web. 05 Jul 2020.

Vancouver:

Zhuang Q. Parametric Study on the Aeroelastic Stability of Rotor Seals. [Internet] [Thesis]. KTH; 2012. [cited 2020 Jul 05]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-116689.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Zhuang Q. Parametric Study on the Aeroelastic Stability of Rotor Seals. [Thesis]. KTH; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-116689

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Notre Dame

26. Ethan Perez. Entropy Generation in a Highly-Loaded, Axial Turbine</h1>.

Degree: Aerospace and Mechanical Engineering, 2014, University of Notre Dame

  Entropy generation in a highly-loaded, axial turbine stage was investigated at on and off-design conditions. Deviation angle, total pressure, total temperature, and specific entropy… (more)

Subjects/Keywords: axial turbine; entropy; turbomachinery; entropy generation

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APA (6th Edition):

Perez, E. (2014). Entropy Generation in a Highly-Loaded, Axial Turbine</h1>. (Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/nk322b9128n

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Perez, Ethan. “Entropy Generation in a Highly-Loaded, Axial Turbine</h1>.” 2014. Thesis, University of Notre Dame. Accessed July 05, 2020. https://curate.nd.edu/show/nk322b9128n.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Perez, Ethan. “Entropy Generation in a Highly-Loaded, Axial Turbine</h1>.” 2014. Web. 05 Jul 2020.

Vancouver:

Perez E. Entropy Generation in a Highly-Loaded, Axial Turbine</h1>. [Internet] [Thesis]. University of Notre Dame; 2014. [cited 2020 Jul 05]. Available from: https://curate.nd.edu/show/nk322b9128n.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Perez E. Entropy Generation in a Highly-Loaded, Axial Turbine</h1>. [Thesis]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/nk322b9128n

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Loughborough University

27. Coppinger, Miles. Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system.

Degree: PhD, 1999, Loughborough University

 Industrial centrifugal air compressors can require a combination of a large range of mass flow, high efficiency, constant pressure ratio, and constant rotational speed, specifically… (more)

Subjects/Keywords: 629.1323; Turbomachinery; CFD

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APA (6th Edition):

Coppinger, M. (1999). Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/7263

Chicago Manual of Style (16th Edition):

Coppinger, Miles. “Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system.” 1999. Doctoral Dissertation, Loughborough University. Accessed July 05, 2020. http://hdl.handle.net/2134/7263.

MLA Handbook (7th Edition):

Coppinger, Miles. “Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system.” 1999. Web. 05 Jul 2020.

Vancouver:

Coppinger M. Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system. [Internet] [Doctoral dissertation]. Loughborough University; 1999. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/2134/7263.

Council of Science Editors:

Coppinger M. Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system. [Doctoral Dissertation]. Loughborough University; 1999. Available from: http://hdl.handle.net/2134/7263


Delft University of Technology

28. Spazzoli, S. (author). Supercritical CO2 Power Cycle for Solar Applications: Thermodynamic Analysis and 1D Turbomachinery Design.

Degree: 2016, Delft University of Technology

Supercritical CO2 (s-CO2) Brayton cycle is indicated as one of the possible substitutes of the traditional steam cycle, that is currently used to produce the… (more)

Subjects/Keywords: turbomachinery design; power cycle; supercritical CO2

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APA (6th Edition):

Spazzoli, S. (. (2016). Supercritical CO2 Power Cycle for Solar Applications: Thermodynamic Analysis and 1D Turbomachinery Design. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:466260b5-24eb-4979-912d-5c2080370021

Chicago Manual of Style (16th Edition):

Spazzoli, S (author). “Supercritical CO2 Power Cycle for Solar Applications: Thermodynamic Analysis and 1D Turbomachinery Design.” 2016. Masters Thesis, Delft University of Technology. Accessed July 05, 2020. http://resolver.tudelft.nl/uuid:466260b5-24eb-4979-912d-5c2080370021.

MLA Handbook (7th Edition):

Spazzoli, S (author). “Supercritical CO2 Power Cycle for Solar Applications: Thermodynamic Analysis and 1D Turbomachinery Design.” 2016. Web. 05 Jul 2020.

Vancouver:

Spazzoli S(. Supercritical CO2 Power Cycle for Solar Applications: Thermodynamic Analysis and 1D Turbomachinery Design. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Jul 05]. Available from: http://resolver.tudelft.nl/uuid:466260b5-24eb-4979-912d-5c2080370021.

Council of Science Editors:

Spazzoli S(. Supercritical CO2 Power Cycle for Solar Applications: Thermodynamic Analysis and 1D Turbomachinery Design. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:466260b5-24eb-4979-912d-5c2080370021


Delft University of Technology

29. Francés Mollá, V. (author). 3D-simulation of multi-stage turbomachinery by means of a non-reflecting mixing plane interface.

Degree: 2017, Delft University of Technology

Turbomachines have experienced a fast development over the last years, and are present in a wide range of devices involved in the generation of electricity… (more)

Subjects/Keywords: turbomachinery; CFD; mixing plane; multi-stage; NRBC

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APA (6th Edition):

Francés Mollá, V. (. (2017). 3D-simulation of multi-stage turbomachinery by means of a non-reflecting mixing plane interface. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:324b6057-aeab-4ad8-ab24-5aa1a62819a0

Chicago Manual of Style (16th Edition):

Francés Mollá, V (author). “3D-simulation of multi-stage turbomachinery by means of a non-reflecting mixing plane interface.” 2017. Masters Thesis, Delft University of Technology. Accessed July 05, 2020. http://resolver.tudelft.nl/uuid:324b6057-aeab-4ad8-ab24-5aa1a62819a0.

MLA Handbook (7th Edition):

Francés Mollá, V (author). “3D-simulation of multi-stage turbomachinery by means of a non-reflecting mixing plane interface.” 2017. Web. 05 Jul 2020.

Vancouver:

Francés Mollá V(. 3D-simulation of multi-stage turbomachinery by means of a non-reflecting mixing plane interface. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Jul 05]. Available from: http://resolver.tudelft.nl/uuid:324b6057-aeab-4ad8-ab24-5aa1a62819a0.

Council of Science Editors:

Francés Mollá V(. 3D-simulation of multi-stage turbomachinery by means of a non-reflecting mixing plane interface. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:324b6057-aeab-4ad8-ab24-5aa1a62819a0


University of Melbourne

30. Akolekar, Harshal Deepak. Understanding loss mechanisms in turbomachinery to increase efficiency.

Degree: 2016, University of Melbourne

 The improvement in the design of any mechanical device is always carried out to increase its efficiency. Turbomachinery, more specifically, the low pressure turbine (LPT)… (more)

Subjects/Keywords: turbomachinery; efficiency; Denton's analysis; loss breakdown

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Akolekar, H. D. (2016). Understanding loss mechanisms in turbomachinery to increase efficiency. (Masters Thesis). University of Melbourne. Retrieved from http://hdl.handle.net/11343/234017

Chicago Manual of Style (16th Edition):

Akolekar, Harshal Deepak. “Understanding loss mechanisms in turbomachinery to increase efficiency.” 2016. Masters Thesis, University of Melbourne. Accessed July 05, 2020. http://hdl.handle.net/11343/234017.

MLA Handbook (7th Edition):

Akolekar, Harshal Deepak. “Understanding loss mechanisms in turbomachinery to increase efficiency.” 2016. Web. 05 Jul 2020.

Vancouver:

Akolekar HD. Understanding loss mechanisms in turbomachinery to increase efficiency. [Internet] [Masters thesis]. University of Melbourne; 2016. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/11343/234017.

Council of Science Editors:

Akolekar HD. Understanding loss mechanisms in turbomachinery to increase efficiency. [Masters Thesis]. University of Melbourne; 2016. Available from: http://hdl.handle.net/11343/234017

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