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You searched for subject:(turbomachinery). Showing records 1 – 30 of 185 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: 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. (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
Not specified: Masters Thesis or Doctoral Dissertation

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. Thesis, University of Texas – Austin. Accessed July 20, 2018. http://hdl.handle.net/2152/34143.

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

MLA Handbook (7th Edition):

-3677-5743. “The effect of channel parameters on the adiabatic film cooling effectiveness of shaped holes in crossflow.” 2015. Web. 20 Jul 2018.

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] [Thesis]. University of Texas – Austin; 2015. [cited 2018 Jul 20]. 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
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

-3677-5743. The effect of channel parameters on the adiabatic film cooling effectiveness of shaped holes in crossflow. [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
Not specified: Masters Thesis or Doctoral Dissertation


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 July 20, 2018. http://hdl.handle.net/10222/71602.

MLA Handbook (7th Edition):

Dodsworth, Laura. “Operational Parametric Study of a Prototype Tesla Pump.” 2016. Web. 20 Jul 2018.

Vancouver:

Dodsworth L. Operational Parametric Study of a Prototype Tesla Pump. [Internet] [Masters thesis]. Dalhousie University; 2016. [cited 2018 Jul 20]. 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


University of Cambridge

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

Degree: 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 . (Thesis). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/270611

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):

Schreiber, Christoph. “Inlet Recirculation in Radial Compressors .” 2018. Thesis, University of Cambridge. Accessed July 20, 2018. https://www.repository.cam.ac.uk/handle/1810/270611.

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

MLA Handbook (7th Edition):

Schreiber, Christoph. “Inlet Recirculation in Radial Compressors .” 2018. Web. 20 Jul 2018.

Vancouver:

Schreiber C. Inlet Recirculation in Radial Compressors . [Internet] [Thesis]. University of Cambridge; 2018. [cited 2018 Jul 20]. Available from: https://www.repository.cam.ac.uk/handle/1810/270611.

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

Council of Science Editors:

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

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


University of Cincinnati

4. 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 20, 2018. 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. 20 Jul 2018.

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 2018 Jul 20]. 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 Virginia

5. Gresham, Thomas. Computational Porous Media Modeling of a Brush Seal for Incompressible and Slightly Compressible Flow.

Degree: MS, Mechanical Engineering, 2016, University of Virginia

 Annular seals are critical to the efficient operation of turbomachinery under increasingly high pressure loadings. Brush seals employ rows of bristles to close the gap… (more)

Subjects/Keywords: Brush Seal; Turbomachinery; Fluid Mechanics

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APA (6th Edition):

Gresham, T. (2016). Computational Porous Media Modeling of a Brush Seal for Incompressible and Slightly Compressible Flow. (Doctoral Dissertation). University of Virginia. Retrieved from http://libra.virginia.edu/catalog/libra-oa:11713

Chicago Manual of Style (16th Edition):

Gresham, Thomas. “Computational Porous Media Modeling of a Brush Seal for Incompressible and Slightly Compressible Flow.” 2016. Doctoral Dissertation, University of Virginia. Accessed July 20, 2018. http://libra.virginia.edu/catalog/libra-oa:11713.

MLA Handbook (7th Edition):

Gresham, Thomas. “Computational Porous Media Modeling of a Brush Seal for Incompressible and Slightly Compressible Flow.” 2016. Web. 20 Jul 2018.

Vancouver:

Gresham T. Computational Porous Media Modeling of a Brush Seal for Incompressible and Slightly Compressible Flow. [Internet] [Doctoral dissertation]. University of Virginia; 2016. [cited 2018 Jul 20]. Available from: http://libra.virginia.edu/catalog/libra-oa:11713.

Council of Science Editors:

Gresham T. Computational Porous Media Modeling of a Brush Seal for Incompressible and Slightly Compressible Flow. [Doctoral Dissertation]. University of Virginia; 2016. Available from: http://libra.virginia.edu/catalog/libra-oa:11713


The Ohio State University

6. 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 20, 2018. 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. 20 Jul 2018.

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 2018 Jul 20]. 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


University of Notre Dame

7. Matthew Aron Bennington. Tip Gap Flow and Casing Treatments in an Axial Compressor.

Degree: PhD, Aerospace and Mechanical Engineering, 2009, University of Notre Dame

  The operating range of modern high-bypass turbofan aircraft engines is limited by the axisymmetric breakdown of flow through the compressor known as stall. The… (more)

Subjects/Keywords: Axial Compressors; Casing Treatments; Turbomachinery

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APA (6th Edition):

Bennington, M. A. (2009). Tip Gap Flow and Casing Treatments in an Axial Compressor. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/qv33rv06h24

Chicago Manual of Style (16th Edition):

Bennington, Matthew Aron. “Tip Gap Flow and Casing Treatments in an Axial Compressor.” 2009. Doctoral Dissertation, University of Notre Dame. Accessed July 20, 2018. https://curate.nd.edu/show/qv33rv06h24.

MLA Handbook (7th Edition):

Bennington, Matthew Aron. “Tip Gap Flow and Casing Treatments in an Axial Compressor.” 2009. Web. 20 Jul 2018.

Vancouver:

Bennington MA. Tip Gap Flow and Casing Treatments in an Axial Compressor. [Internet] [Doctoral dissertation]. University of Notre Dame; 2009. [cited 2018 Jul 20]. Available from: https://curate.nd.edu/show/qv33rv06h24.

Council of Science Editors:

Bennington MA. Tip Gap Flow and Casing Treatments in an Axial Compressor. [Doctoral Dissertation]. University of Notre Dame; 2009. Available from: https://curate.nd.edu/show/qv33rv06h24

8. 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 20, 2018. http://hdl.handle.net/10044/1/8450.

MLA Handbook (7th Edition):

Hillary, Brenda. “Indirect measurement of vibration excitation forces.” 1983. Web. 20 Jul 2018.

Vancouver:

Hillary B. Indirect measurement of vibration excitation forces. [Internet] [Doctoral dissertation]. Imperial College London; 1983. [cited 2018 Jul 20]. 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

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158055

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):

Carpenter IV, Forrest Lafon. “Practical Aspects of Computational Fluid Dynamics for Turbomachinery.” 2016. Thesis, Texas A&M University. Accessed July 20, 2018. http://hdl.handle.net/1969.1/158055.

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

MLA Handbook (7th Edition):

Carpenter IV, Forrest Lafon. “Practical Aspects of Computational Fluid Dynamics for Turbomachinery.” 2016. Web. 20 Jul 2018.

Vancouver:

Carpenter IV FL. Practical Aspects of Computational Fluid Dynamics for Turbomachinery. [Internet] [Thesis]. Texas A&M University; 2016. [cited 2018 Jul 20]. Available from: http://hdl.handle.net/1969.1/158055.

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

Council of Science Editors:

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

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


Texas A&M University

10. 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 20, 2018. 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. 20 Jul 2018.

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 2018 Jul 20]. 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

11. 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 20, 2018. 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. 20 Jul 2018.

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 2018 Jul 20]. 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

12. 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 20, 2018. 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. 20 Jul 2018.

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 2018 Jul 20]. 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

13. 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 20, 2018. 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. 20 Jul 2018.

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 2018 Jul 20]. 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

14. 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 20, 2018. 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. 20 Jul 2018.

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 2018 Jul 20]. 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


University of Ottawa

15. 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 20, 2018. 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. 20 Jul 2018.

Vancouver:

Smith CI. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . [Internet] [Thesis]. University of Ottawa; 2010. [cited 2018 Jul 20]. 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


Cranfield University

16. 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 20, 2018. 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. 20 Jul 2018.

Vancouver:

Attia OAMM. Finite element static, dynamic, and flutter analysis of rotating composite layered plates and shells. [Internet] [Doctoral dissertation]. Cranfield University; 1996. [cited 2018 Jul 20]. 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

17. Xie, Shasha. Studies of the ERCOFTAC Centrifugal Pump with OpenFOAM.

Degree: 2010, Chalmers University of Technology

 Numerical solutions of the rotor-stator interaction using OpenFOAM-1.5-dev was investigated in the ERCOFTAC Centrifugal Pump, a testcase from the ERCOFTAC Turbomachinery Special Interest Group. The… (more)

Subjects/Keywords: CFD; OpenFOAM; Turbomachinery; GGI; ERCOFTAC Centrifugal Pump

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APA (6th Edition):

Xie, S. (2010). Studies of the ERCOFTAC Centrifugal Pump with OpenFOAM. (Thesis). Chalmers University of Technology. Retrieved from http://studentarbeten.chalmers.se/publication/122638-studies-of-the-ercoftac-centrifugal-pump-with-openfoam

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):

Xie, Shasha. “Studies of the ERCOFTAC Centrifugal Pump with OpenFOAM.” 2010. Thesis, Chalmers University of Technology. Accessed July 20, 2018. http://studentarbeten.chalmers.se/publication/122638-studies-of-the-ercoftac-centrifugal-pump-with-openfoam.

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

MLA Handbook (7th Edition):

Xie, Shasha. “Studies of the ERCOFTAC Centrifugal Pump with OpenFOAM.” 2010. Web. 20 Jul 2018.

Vancouver:

Xie S. Studies of the ERCOFTAC Centrifugal Pump with OpenFOAM. [Internet] [Thesis]. Chalmers University of Technology; 2010. [cited 2018 Jul 20]. Available from: http://studentarbeten.chalmers.se/publication/122638-studies-of-the-ercoftac-centrifugal-pump-with-openfoam.

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

Council of Science Editors:

Xie S. Studies of the ERCOFTAC Centrifugal Pump with OpenFOAM. [Thesis]. Chalmers University of Technology; 2010. Available from: http://studentarbeten.chalmers.se/publication/122638-studies-of-the-ercoftac-centrifugal-pump-with-openfoam

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


Loughborough University

18. 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 https://dspace.lboro.ac.uk/2134/7263 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.324490

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 20, 2018. https://dspace.lboro.ac.uk/2134/7263 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.324490.

MLA Handbook (7th Edition):

Coppinger, Miles. “Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system.” 1999. Web. 20 Jul 2018.

Vancouver:

Coppinger M. Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system. [Internet] [Doctoral dissertation]. Loughborough University; 1999. [cited 2018 Jul 20]. Available from: https://dspace.lboro.ac.uk/2134/7263 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.324490.

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: https://dspace.lboro.ac.uk/2134/7263 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.324490


University of Cincinnati

19. 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 20, 2018. 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. 20 Jul 2018.

Vancouver:

Szabo I. A Numerical Study of Water Injection on Transonic Compressor Rotor Performance. [Internet] [Doctoral dissertation]. University of Cincinnati; 2008. [cited 2018 Jul 20]. 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


EPFL

20. Kahl, Gerhard. Aeroelastic effects of mistuning and coupling in turbomachinery bladings.

Degree: 2002, EPFL

 A numerical method has been developed to study the effects of structural mistuning on the aeroelastic behaviour of turbomachinery cascades. The specific objectives of the… (more)

Subjects/Keywords: Turbomachinery; Unsteady Flows

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APA (6th Edition):

Kahl, G. (2002). Aeroelastic effects of mistuning and coupling in turbomachinery bladings. (Thesis). EPFL. Retrieved from http://infoscience.epfl.ch/record/103718

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):

Kahl, Gerhard. “Aeroelastic effects of mistuning and coupling in turbomachinery bladings.” 2002. Thesis, EPFL. Accessed July 20, 2018. http://infoscience.epfl.ch/record/103718.

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

MLA Handbook (7th Edition):

Kahl, Gerhard. “Aeroelastic effects of mistuning and coupling in turbomachinery bladings.” 2002. Web. 20 Jul 2018.

Vancouver:

Kahl G. Aeroelastic effects of mistuning and coupling in turbomachinery bladings. [Internet] [Thesis]. EPFL; 2002. [cited 2018 Jul 20]. Available from: http://infoscience.epfl.ch/record/103718.

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

Council of Science Editors:

Kahl G. Aeroelastic effects of mistuning and coupling in turbomachinery bladings. [Thesis]. EPFL; 2002. Available from: http://infoscience.epfl.ch/record/103718

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


EPFL

21. Rottmeier, Fabrice. Experimental investigation of a vibrating axial turbine cascade in presence of upstream generated aerodynamic gusts.

Degree: 2003, EPFL

 An experimental investigation has been conducted in the non-rotating annular test facility of the "Laboratoire de Thermique Appliquée et de Turbomachines" (LTT), "École Polytechnique Fédérale… (more)

Subjects/Keywords: Turbomachinery; Unsteady Flows

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APA (6th Edition):

Rottmeier, F. (2003). Experimental investigation of a vibrating axial turbine cascade in presence of upstream generated aerodynamic gusts. (Thesis). EPFL. Retrieved from http://infoscience.epfl.ch/record/103723

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):

Rottmeier, Fabrice. “Experimental investigation of a vibrating axial turbine cascade in presence of upstream generated aerodynamic gusts.” 2003. Thesis, EPFL. Accessed July 20, 2018. http://infoscience.epfl.ch/record/103723.

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

MLA Handbook (7th Edition):

Rottmeier, Fabrice. “Experimental investigation of a vibrating axial turbine cascade in presence of upstream generated aerodynamic gusts.” 2003. Web. 20 Jul 2018.

Vancouver:

Rottmeier F. Experimental investigation of a vibrating axial turbine cascade in presence of upstream generated aerodynamic gusts. [Internet] [Thesis]. EPFL; 2003. [cited 2018 Jul 20]. Available from: http://infoscience.epfl.ch/record/103723.

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

Council of Science Editors:

Rottmeier F. Experimental investigation of a vibrating axial turbine cascade in presence of upstream generated aerodynamic gusts. [Thesis]. EPFL; 2003. Available from: http://infoscience.epfl.ch/record/103723

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


Virginia Tech

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

Degree: 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. (Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28875

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):

Reagle, Colin James. “Technique for Measuring the Coefficient of Restitution for Microparticle Sand Impacts at High Temperature for Turbomachinery Applications.” 2012. Thesis, Virginia Tech. Accessed July 20, 2018. http://hdl.handle.net/10919/28875.

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

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. 20 Jul 2018.

Vancouver:

Reagle CJ. Technique for Measuring the Coefficient of Restitution for Microparticle Sand Impacts at High Temperature for Turbomachinery Applications. [Internet] [Thesis]. Virginia Tech; 2012. [cited 2018 Jul 20]. Available from: http://hdl.handle.net/10919/28875.

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

Council of Science Editors:

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

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.

Degree: PhD, 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: entropy; entropy generation; turbomachinery; axial turbine

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Perez, Ethan. “Entropy Generation in a Highly-Loaded, Axial Turbine.” 2014. Doctoral Dissertation, University of Notre Dame. Accessed July 20, 2018. https://curate.nd.edu/show/nk322b9128n.

MLA Handbook (7th Edition):

Perez, Ethan. “Entropy Generation in a Highly-Loaded, Axial Turbine.” 2014. Web. 20 Jul 2018.

Vancouver:

Perez E. Entropy Generation in a Highly-Loaded, Axial Turbine. [Internet] [Doctoral dissertation]. University of Notre Dame; 2014. [cited 2018 Jul 20]. Available from: https://curate.nd.edu/show/nk322b9128n.

Council of Science Editors:

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


KTH

24. 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 20, 2018. 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. 20 Jul 2018.

Vancouver:

Zhuang Q. Parametric Study on the Aeroelastic Stability of Rotor Seals. [Internet] [Thesis]. KTH; 2012. [cited 2018 Jul 20]. 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


Texas A&M University

25. 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 20, 2018. 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. 20 Jul 2018.

Vancouver:

Creary A. MANUFACTURING OF A GAS FOIL BEARINGS FOR PALMED-SIZED TURBOMACHINERY. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2018 Jul 20]. 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

26. 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 20, 2018. 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. 20 Jul 2018.

Vancouver:

Johnson S. Development of a Pulse Modulator for Active Flow Control in Turbomachinery. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2018 Jul 20]. 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

27. 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 20, 2018. 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. 20 Jul 2018.

Vancouver:

Joly MM. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2018 Jul 20]. 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


Oklahoma State University

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

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 20, 2018. 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. 20 Jul 2018.

Vancouver:

Davey MW. Influence of Axial Spacing on Spanwise Efficiency of a Transonic Axial Compressor Rotor Stage. [Internet] [Thesis]. Oklahoma State University; 2004. [cited 2018 Jul 20]. 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

29. Paul Louis Mikrut. Vibration of Axial Turbomachinery Blades: Measurement and Fluid-Structure Interactions.

Degree: PhD, Aerospace and Mechanical Engineering, 2012, University of Notre Dame

  The focus of this dissertation is on turbomachinery blade vibration measurements and unsteady fluid-structure interactions. Vibration of turbomachinery blades are critical to jet engine… (more)

Subjects/Keywords: aerodynamic damping; damping; PIV; particle image velocimetry; measurement; turbomachinery; blade image velocimetry; aeroelasticity; vibration; fluid-structure interaction; BIV; axial turbomachinery

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

APA (6th Edition):

Mikrut, P. L. (2012). Vibration of Axial Turbomachinery Blades: Measurement and Fluid-Structure Interactions. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/js956d5972t

Chicago Manual of Style (16th Edition):

Mikrut, Paul Louis. “Vibration of Axial Turbomachinery Blades: Measurement and Fluid-Structure Interactions.” 2012. Doctoral Dissertation, University of Notre Dame. Accessed July 20, 2018. https://curate.nd.edu/show/js956d5972t.

MLA Handbook (7th Edition):

Mikrut, Paul Louis. “Vibration of Axial Turbomachinery Blades: Measurement and Fluid-Structure Interactions.” 2012. Web. 20 Jul 2018.

Vancouver:

Mikrut PL. Vibration of Axial Turbomachinery Blades: Measurement and Fluid-Structure Interactions. [Internet] [Doctoral dissertation]. University of Notre Dame; 2012. [cited 2018 Jul 20]. Available from: https://curate.nd.edu/show/js956d5972t.

Council of Science Editors:

Mikrut PL. Vibration of Axial Turbomachinery Blades: Measurement and Fluid-Structure Interactions. [Doctoral Dissertation]. University of Notre Dame; 2012. Available from: https://curate.nd.edu/show/js956d5972t


Penn State University

30. Dey, Debashis. AERODYNAMIC TIP DESENSITIZATION IN AXIAL FLOW TURBINES.

Degree: PhD, Aerospace Engineering, 2001, Penn State University

 The leakage flow near the tip of unshrouded rotor blades in axial turbines imposes significant thermal loads on the blade. It is also responsible for… (more)

Subjects/Keywords: gas turbine; turbomachinery heat transfer; turbomachinery aerodynamics; tip leakage

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

APA (6th Edition):

Dey, D. (2001). AERODYNAMIC TIP DESENSITIZATION IN AXIAL FLOW TURBINES. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/5894

Chicago Manual of Style (16th Edition):

Dey, Debashis. “AERODYNAMIC TIP DESENSITIZATION IN AXIAL FLOW TURBINES.” 2001. Doctoral Dissertation, Penn State University. Accessed July 20, 2018. https://etda.libraries.psu.edu/catalog/5894.

MLA Handbook (7th Edition):

Dey, Debashis. “AERODYNAMIC TIP DESENSITIZATION IN AXIAL FLOW TURBINES.” 2001. Web. 20 Jul 2018.

Vancouver:

Dey D. AERODYNAMIC TIP DESENSITIZATION IN AXIAL FLOW TURBINES. [Internet] [Doctoral dissertation]. Penn State University; 2001. [cited 2018 Jul 20]. Available from: https://etda.libraries.psu.edu/catalog/5894.

Council of Science Editors:

Dey D. AERODYNAMIC TIP DESENSITIZATION IN AXIAL FLOW TURBINES. [Doctoral Dissertation]. Penn State University; 2001. Available from: https://etda.libraries.psu.edu/catalog/5894

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