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You searched for subject:(turbomachinery). Showing records 1 – 30 of 197 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 December 16, 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. 16 Dec 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 Dec 16]. 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 December 16, 2018. http://hdl.handle.net/10222/71602.

MLA Handbook (7th Edition):

Dodsworth, Laura. “Operational Parametric Study of a Prototype Tesla Pump.” 2016. Web. 16 Dec 2018.

Vancouver:

Dodsworth L. Operational Parametric Study of a Prototype Tesla Pump. [Internet] [Masters thesis]. Dalhousie University; 2016. [cited 2018 Dec 16]. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Schreiber C. Inlet Recirculation in Radial Compressors . [Internet] [Thesis]. University of Cambridge; 2018. [cited 2018 Dec 16]. 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


Texas A&M University

4. 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 December 16, 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. 16 Dec 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 Dec 16]. 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

5. 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 December 16, 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. 16 Dec 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 Dec 16]. 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

6. 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 December 16, 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. 16 Dec 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 Dec 16]. 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

7. 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 December 16, 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. 16 Dec 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 Dec 16]. 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

8. 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 December 16, 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. 16 Dec 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 Dec 16]. 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 Cincinnati

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

GUIDOTTI, EMANUELE. “Analysis of the Unsteady Flow in an Aspirated Counter-Rotating Compressor Using the Nonlinear Harmonic Balance Method.” 2008. Masters Thesis, University of Cincinnati. Accessed December 16, 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. 16 Dec 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 Dec 16]. 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

10. 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 December 16, 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. 16 Dec 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 Dec 16]. 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

11. 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 December 16, 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. 16 Dec 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 Dec 16]. 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


Cranfield University

12. 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 December 16, 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. 16 Dec 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 Dec 16]. 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

13. 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 December 16, 2018. http://hdl.handle.net/10044/1/8450.

MLA Handbook (7th Edition):

Hillary, Brenda. “Indirect measurement of vibration excitation forces.” 1983. Web. 16 Dec 2018.

Vancouver:

Hillary B. Indirect measurement of vibration excitation forces. [Internet] [Doctoral dissertation]. Imperial College London; 1983. [cited 2018 Dec 16]. 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


University of Ottawa

14. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Smith CI. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . [Internet] [Thesis]. University of Ottawa; 2010. [cited 2018 Dec 16]. Available from: http://hdl.handle.net/10393/19660.

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

Council of Science Editors:

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

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


Texas A&M University

15. 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 December 16, 2018. 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. 16 Dec 2018.

Vancouver:

Carpenter IV FL. Practical Aspects of Computational Fluid Dynamics for Turbomachinery. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2018 Dec 16]. 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

16. 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 December 16, 2018. 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. 16 Dec 2018.

Vancouver:

Gary KW. Measurements of the Leakage and Rotordynamic Performance of Interlocking Labyrinth Seals. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2018 Dec 16]. 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

17. 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 December 16, 2018. 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. 16 Dec 2018.

Vancouver:

Dolan M. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. [Internet] [Thesis]. Purdue University; 2015. [cited 2018 Dec 16]. 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 Notre Dame

18. Matthew Aron Bennington. Tip Gap Flow and Casing Treatments in an Axial Compressor</h1>.

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: Turbomachinery; Axial Compressors; Casing Treatments

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APA (6th Edition):

Bennington, M. A. (2009). Tip Gap Flow and Casing Treatments in an Axial Compressor</h1>. (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</h1>.” 2009. Doctoral Dissertation, University of Notre Dame. Accessed December 16, 2018. https://curate.nd.edu/show/qv33rv06h24.

MLA Handbook (7th Edition):

Bennington, Matthew Aron. “Tip Gap Flow and Casing Treatments in an Axial Compressor</h1>.” 2009. Web. 16 Dec 2018.

Vancouver:

Bennington MA. Tip Gap Flow and Casing Treatments in an Axial Compressor</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2009. [cited 2018 Dec 16]. Available from: https://curate.nd.edu/show/qv33rv06h24.

Council of Science Editors:

Bennington MA. Tip Gap Flow and Casing Treatments in an Axial Compressor</h1>. [Doctoral Dissertation]. University of Notre Dame; 2009. Available from: https://curate.nd.edu/show/qv33rv06h24

19. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Xie S. Studies of the ERCOFTAC Centrifugal Pump with OpenFOAM. [Internet] [Thesis]. Chalmers University of Technology; 2010. [cited 2018 Dec 16]. 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

20. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Coppinger M. Aerodynamic performance of an industrial centrifugal compressor variable inlet guide vane system. [Internet] [Doctoral dissertation]. Loughborough University; 1999. [cited 2018 Dec 16]. 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


Texas A&M University

21. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Creary A. MANUFACTURING OF A GAS FOIL BEARINGS FOR PALMED-SIZED TURBOMACHINERY. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2018 Dec 16]. 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

22. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Johnson S. Development of a Pulse Modulator for Active Flow Control in Turbomachinery. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2018 Dec 16]. 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

23. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Joly MM. Multifidelity, Multidisciplinary Optimization of Turbomachines with Shock Interaction. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2018 Dec 16]. Available from: http://hdl.handle.net/1969.1/153360.

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

Council of Science Editors:

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

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


University of Cincinnati

24. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Szabo I. A Numerical Study of Water Injection on Transonic Compressor Rotor Performance. [Internet] [Doctoral dissertation]. University of Cincinnati; 2008. [cited 2018 Dec 16]. 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

25. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Kahl G. Aeroelastic effects of mistuning and coupling in turbomachinery bladings. [Internet] [Thesis]. EPFL; 2002. [cited 2018 Dec 16]. 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

26. 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 December 16, 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. 16 Dec 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 Dec 16]. 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

27. 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 December 16, 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. 16 Dec 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 Dec 16]. 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


KTH

28. 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 December 16, 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. 16 Dec 2018.

Vancouver:

Zhuang Q. Parametric Study on the Aeroelastic Stability of Rotor Seals. [Internet] [Thesis]. KTH; 2012. [cited 2018 Dec 16]. 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


Oklahoma State University

29. 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 December 16, 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. 16 Dec 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 Dec 16]. 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


Texas A&M University

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

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 December 16, 2018. 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. 16 Dec 2018.

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 2018 Dec 16]. 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

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