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You searched for subject:(Turbomachinery). Showing records 1 – 30 of 259 total matches.

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University of Texas – Austin

1. -3677-5743. The effect of channel parameters on the adiabatic film cooling effectiveness of shaped holes in crossflow.

Degree: MSin Engineering, Mechanical engineering, 2015, University of Texas – Austin

 There is limited information in the literature on the behavior of shaped film cooling holes fed by crossflow and even less information on the effect… (more)

Subjects/Keywords: Film cooling; Turbomachinery

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APA (6th Edition):

-3677-5743. (2015). The effect of channel parameters on the adiabatic film cooling effectiveness of shaped holes in crossflow. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/34143

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-3677-5743. “The effect of channel parameters on the adiabatic film cooling effectiveness of shaped holes in crossflow.” 2015. Masters Thesis, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/34143.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-3677-5743. “The effect of channel parameters on the adiabatic film cooling effectiveness of shaped holes in crossflow.” 2015. Web. 24 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-3677-5743. The effect of channel parameters on the adiabatic film cooling effectiveness of shaped holes in crossflow. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/34143.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-3677-5743. The effect of channel parameters on the adiabatic film cooling effectiveness of shaped holes in crossflow. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/34143

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Dalhousie University

2. 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 January 24, 2021. http://hdl.handle.net/10222/71602.

MLA Handbook (7th Edition):

Dodsworth, Laura. “Operational Parametric Study of a Prototype Tesla Pump.” 2016. Web. 24 Jan 2021.

Vancouver:

Dodsworth L. Operational Parametric Study of a Prototype Tesla Pump. [Internet] [Masters thesis]. Dalhousie University; 2016. [cited 2021 Jan 24]. 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


Texas A&M University

3. 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 January 24, 2021. 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. 24 Jan 2021.

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 2021 Jan 24]. 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


Texas A&M University

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

Degree: PhD, Mechanical Engineering, 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. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148052

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. Doctoral Dissertation, Texas A&M University. Accessed January 24, 2021. http://hdl.handle.net/1969.1/148052.

MLA Handbook (7th Edition):

Rasmy Marsis, Emanuel 1983-. “CFD Simulation and Experimental Testing of Multiphase Flow Inside the MVP Electrical Submersible Pump.” 2012. Web. 24 Jan 2021.

Vancouver:

Rasmy Marsis E1. CFD Simulation and Experimental Testing of Multiphase Flow Inside the MVP Electrical Submersible Pump. [Internet] [Doctoral dissertation]. Texas A&M University; 2012. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1969.1/148052.

Council of Science Editors:

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


Texas A&M University

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

Degree: PhD, Mechanical Engineering, 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. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151083

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. Doctoral Dissertation, Texas A&M University. Accessed January 24, 2021. http://hdl.handle.net/1969.1/151083.

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. 24 Jan 2021.

Vancouver:

Abdelfattah SA. Numerical and Experimental Analysis of Multi-Stage Axial Turbine Performance at Design and Off-Design Conditions. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1969.1/151083.

Council of Science Editors:

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


Texas A&M University

6. 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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Carpenter IV FL. Practical Aspects of Computational Fluid Dynamics for Turbomachinery. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Jan 24]. 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

7. 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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Gary KW. Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2021 Jan 24]. 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


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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Dolan M. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. [Internet] [Thesis]. Purdue University; 2015. [cited 2021 Jan 24]. 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 Ottawa

9. 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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Smith CI. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . [Internet] [Thesis]. University of Ottawa; 2010. [cited 2021 Jan 24]. 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

10. 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 January 24, 2021. https://www.repository.cam.ac.uk/handle/1810/270611.

MLA Handbook (7th Edition):

Schreiber, Christoph. “Inlet Recirculation in Radial Compressors.” 2018. Web. 24 Jan 2021.

Vancouver:

Schreiber C. Inlet Recirculation in Radial Compressors. [Internet] [Doctoral dissertation]. University of Cambridge; 2018. [cited 2021 Jan 24]. 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


Cranfield University

11. 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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Attia OAMM. Finite element static, dynamic, and flutter analysis of rotating composite layered plates and shells. [Internet] [Doctoral dissertation]. Cranfield University; 1996. [cited 2021 Jan 24]. 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

12. 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 January 24, 2021. http://hdl.handle.net/10044/1/8450.

MLA Handbook (7th Edition):

Hillary, Brenda. “Indirect measurement of vibration excitation forces.” 1983. Web. 24 Jan 2021.

Vancouver:

Hillary B. Indirect measurement of vibration excitation forces. [Internet] [Doctoral dissertation]. Imperial College London; 1983. [cited 2021 Jan 24]. 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


The Ohio State University

13. 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 January 24, 2021. 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. 24 Jan 2021.

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 2021 Jan 24]. 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

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

Degree: MS, Aerospace Engineering, 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. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035

Chicago Manual of Style (16th Edition):

Johnson, Shalom. “Development of a Pulse Modulator for Active Flow Control in Turbomachinery.” 2011. Masters Thesis, Texas A&M University. Accessed January 24, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035.

MLA Handbook (7th Edition):

Johnson, Shalom. “Development of a Pulse Modulator for Active Flow Control in Turbomachinery.” 2011. Web. 24 Jan 2021.

Vancouver:

Johnson S. Development of a Pulse Modulator for Active Flow Control in Turbomachinery. [Internet] [Masters thesis]. Texas A&M University; 2011. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8035.

Council of Science Editors:

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


Texas A&M University

15. 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 January 24, 2021. 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. 24 Jan 2021.

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 2021 Jan 24]. 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


University of Cambridge

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

APA (6th Edition):

Perovic, D. (2019). Distortion tolerant fan design. (Doctoral Dissertation). University of Cambridge. Retrieved from https://doi.org/10.17863/CAM.39606 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774792

Chicago Manual of Style (16th Edition):

Perovic, Dusan. “Distortion tolerant fan design.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 24, 2021. https://doi.org/10.17863/CAM.39606 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774792.

MLA Handbook (7th Edition):

Perovic, Dusan. “Distortion tolerant fan design.” 2019. Web. 24 Jan 2021.

Vancouver:

Perovic D. Distortion tolerant fan design. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 24]. Available from: https://doi.org/10.17863/CAM.39606 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774792.

Council of Science Editors:

Perovic D. Distortion tolerant fan design. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://doi.org/10.17863/CAM.39606 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774792


University of Cambridge

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

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 January 24, 2021. https://www.repository.cam.ac.uk/handle/1810/292447.

MLA Handbook (7th Edition):

Perovic, Dusan. “Distortion Tolerant Fan Design.” 2019. Web. 24 Jan 2021.

Vancouver:

Perovic D. Distortion Tolerant Fan Design. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 24]. 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


KTH

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

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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Zhuang Q. Parametric Study on the Aeroelastic Stability of Rotor Seals. [Internet] [Thesis]. KTH; 2012. [cited 2021 Jan 24]. 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


Loughborough University

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

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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Coppinger M. Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system. [Internet] [Doctoral dissertation]. Loughborough University; 1999. [cited 2021 Jan 24]. 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

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

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 January 24, 2021. 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. 24 Jan 2021.

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 2021 Jan 24]. 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

21. 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 January 24, 2021. 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. 24 Jan 2021.

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 2021 Jan 24]. 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


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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Davey MW. Influence of Axial Spacing on Spanwise Efficiency of a Transonic Axial Compressor Rotor Stage. [Internet] [Thesis]. Oklahoma State University; 2004. [cited 2021 Jan 24]. 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 Notre Dame

23. 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 January 24, 2021. 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. 24 Jan 2021.

Vancouver:

Perez E. Entropy Generation in a Highly-Loaded, Axial Turbine</h1>. [Internet] [Thesis]. University of Notre Dame; 2014. [cited 2021 Jan 24]. 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


University of Melbourne

24. 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 January 24, 2021. http://hdl.handle.net/11343/234017.

MLA Handbook (7th Edition):

Akolekar, Harshal Deepak. “Understanding loss mechanisms in turbomachinery to increase efficiency.” 2016. Web. 24 Jan 2021.

Vancouver:

Akolekar HD. Understanding loss mechanisms in turbomachinery to increase efficiency. [Internet] [Masters thesis]. University of Melbourne; 2016. [cited 2021 Jan 24]. 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

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

Degree: PhD, Aerospace Engineering, 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 · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Joly, Michael Marie. “Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.” 2014. Doctoral Dissertation, Texas A&M University. Accessed January 24, 2021. http://hdl.handle.net/1969.1/153360.

MLA Handbook (7th Edition):

Joly, Michael Marie. “Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction.” 2014. Web. 24 Jan 2021.

Vancouver:

Joly MM. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1969.1/153360.

Council of Science Editors:

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


Virginia Tech

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

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 January 24, 2021. 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. 24 Jan 2021.

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 2021 Jan 24]. 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


University of Cambridge

27. 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: 621.406; 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://doi.org/10.17863/CAM.17538 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.744449

Chicago Manual of Style (16th Edition):

Schreiber, Christoph. “Inlet recirculation in radial compressors.” 2018. Doctoral Dissertation, University of Cambridge. Accessed January 24, 2021. https://doi.org/10.17863/CAM.17538 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.744449.

MLA Handbook (7th Edition):

Schreiber, Christoph. “Inlet recirculation in radial compressors.” 2018. Web. 24 Jan 2021.

Vancouver:

Schreiber C. Inlet recirculation in radial compressors. [Internet] [Doctoral dissertation]. University of Cambridge; 2018. [cited 2021 Jan 24]. Available from: https://doi.org/10.17863/CAM.17538 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.744449.

Council of Science Editors:

Schreiber C. Inlet recirculation in radial compressors. [Doctoral Dissertation]. University of Cambridge; 2018. Available from: https://doi.org/10.17863/CAM.17538 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.744449


University of Cincinnati

28. Holder, Justin. Fluid Structure Interaction in Compressible Flows.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2020, University of Cincinnati

 One-way fluid structure interaction (FSI) is explored in two independent scenarios. First, a rectangular single expansion ramp nozzle (SERN) is analyzed through CFD. The SERN… (more)

Subjects/Keywords: Aerospace Materials; nozzle; CFD; FEA; FSI; turbomachinery

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APA (6th Edition):

Holder, J. (2020). Fluid Structure Interaction in Compressible Flows. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin159584692691518

Chicago Manual of Style (16th Edition):

Holder, Justin. “Fluid Structure Interaction in Compressible Flows.” 2020. Masters Thesis, University of Cincinnati. Accessed January 24, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ucin159584692691518.

MLA Handbook (7th Edition):

Holder, Justin. “Fluid Structure Interaction in Compressible Flows.” 2020. Web. 24 Jan 2021.

Vancouver:

Holder J. Fluid Structure Interaction in Compressible Flows. [Internet] [Masters thesis]. University of Cincinnati; 2020. [cited 2021 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin159584692691518.

Council of Science Editors:

Holder J. Fluid Structure Interaction in Compressible Flows. [Masters Thesis]. University of Cincinnati; 2020. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin159584692691518


University of Cambridge

29. Jardine, Lachlan. The Effect of Heat Transfer on Turbine Performance.

Degree: PhD, 2019, University of Cambridge

 Despite the blades downstream of the combustor being cooled in most large gas turbines, the effect this cooling has on their performance is still unclear.… (more)

Subjects/Keywords: Thermodynamics; Heat transfer; Turbine; Turbomachinery; CFD

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APA (6th Edition):

Jardine, L. (2019). The Effect of Heat Transfer on Turbine Performance. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/309428

Chicago Manual of Style (16th Edition):

Jardine, Lachlan. “The Effect of Heat Transfer on Turbine Performance.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 24, 2021. https://www.repository.cam.ac.uk/handle/1810/309428.

MLA Handbook (7th Edition):

Jardine, Lachlan. “The Effect of Heat Transfer on Turbine Performance.” 2019. Web. 24 Jan 2021.

Vancouver:

Jardine L. The Effect of Heat Transfer on Turbine Performance. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 24]. Available from: https://www.repository.cam.ac.uk/handle/1810/309428.

Council of Science Editors:

Jardine L. The Effect of Heat Transfer on Turbine Performance. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/309428


Delft University of Technology

30. Johri, Kartikay (author). Data-driven boundary layer loss model for organic rankine cycle turbomachines.

Degree: 2020, Delft University of Technology

There is a requirement for localised efficient electricity generation systems that increase the efficiency of power plants and reduce wasted heat from other engineering applications… (more)

Subjects/Keywords: Turbomachinery; Machine Learning; Axial stator; SU2; CFD

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APA (6th Edition):

Johri, K. (. (2020). Data-driven boundary layer loss model for organic rankine cycle turbomachines. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8199c1ff-2ba5-4d98-a18b-30f7554a8ec2

Chicago Manual of Style (16th Edition):

Johri, Kartikay (author). “Data-driven boundary layer loss model for organic rankine cycle turbomachines.” 2020. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:8199c1ff-2ba5-4d98-a18b-30f7554a8ec2.

MLA Handbook (7th Edition):

Johri, Kartikay (author). “Data-driven boundary layer loss model for organic rankine cycle turbomachines.” 2020. Web. 24 Jan 2021.

Vancouver:

Johri K(. Data-driven boundary layer loss model for organic rankine cycle turbomachines. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:8199c1ff-2ba5-4d98-a18b-30f7554a8ec2.

Council of Science Editors:

Johri K(. Data-driven boundary layer loss model for organic rankine cycle turbomachines. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:8199c1ff-2ba5-4d98-a18b-30f7554a8ec2

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