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You searched for subject:(aerodynamic loss). Showing records 1 – 17 of 17 total matches.

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Penn State University

1. Topcuoglu, Ilker. Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades.

Degree: 2013, Penn State University

 A detailed review of the literature on losses associated with film cooling is given. An experimental case with two different cooling-hole geometries (Round Cylindrical Hole… (more)

Subjects/Keywords: Film cooling; gas turbine cooling; aerodynamic loss prediction; total pressure loss model

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APA (6th Edition):

Topcuoglu, I. (2013). Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19150

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):

Topcuoglu, Ilker. “Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades.” 2013. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/19150.

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

MLA Handbook (7th Edition):

Topcuoglu, Ilker. “Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades.” 2013. Web. 18 Jan 2021.

Vancouver:

Topcuoglu I. Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/19150.

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

Council of Science Editors:

Topcuoglu I. Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19150

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


Brno University of Technology

2. Faltýnek, Michal. Aerodynamický výpočet spalinového traktu parního kotle: Aerodynamic calculation of flue gas part of steam boiler.

Degree: 2020, Brno University of Technology

 The aim of this thesis is to introduce the reader into theory, which is needed to make an aerodynamic calculation of flue gas part of… (more)

Subjects/Keywords: Aerodynamický výpočet; tlaková ztráta; ventilátor; Aerodynamic calculation; pressure loss; ventilator

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APA (6th Edition):

Faltýnek, M. (2020). Aerodynamický výpočet spalinového traktu parního kotle: Aerodynamic calculation of flue gas part of steam boiler. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/193080

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):

Faltýnek, Michal. “Aerodynamický výpočet spalinového traktu parního kotle: Aerodynamic calculation of flue gas part of steam boiler.” 2020. Thesis, Brno University of Technology. Accessed January 18, 2021. http://hdl.handle.net/11012/193080.

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

MLA Handbook (7th Edition):

Faltýnek, Michal. “Aerodynamický výpočet spalinového traktu parního kotle: Aerodynamic calculation of flue gas part of steam boiler.” 2020. Web. 18 Jan 2021.

Vancouver:

Faltýnek M. Aerodynamický výpočet spalinového traktu parního kotle: Aerodynamic calculation of flue gas part of steam boiler. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11012/193080.

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

Council of Science Editors:

Faltýnek M. Aerodynamický výpočet spalinového traktu parního kotle: Aerodynamic calculation of flue gas part of steam boiler. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/193080

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

3. Mihelish, Matthew Phillip. Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows.

Degree: MS, Mechanical Engineering, 2012, University of North Dakota

  Low pressure turbine research is essential for improving the efficiency of the modern gas turbine engine. At high altitude cruise conditions, the low pressure… (more)

Subjects/Keywords: Aerodynamic Loss; Heat Transfer; Mach Number; Reynolds Numbers; Transition; Vane Cascade

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APA (6th Edition):

Mihelish, M. P. (2012). Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/1259

Chicago Manual of Style (16th Edition):

Mihelish, Matthew Phillip. “Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows.” 2012. Masters Thesis, University of North Dakota. Accessed January 18, 2021. https://commons.und.edu/theses/1259.

MLA Handbook (7th Edition):

Mihelish, Matthew Phillip. “Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows.” 2012. Web. 18 Jan 2021.

Vancouver:

Mihelish MP. Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows. [Internet] [Masters thesis]. University of North Dakota; 2012. [cited 2021 Jan 18]. Available from: https://commons.und.edu/theses/1259.

Council of Science Editors:

Mihelish MP. Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows. [Masters Thesis]. University of North Dakota; 2012. Available from: https://commons.und.edu/theses/1259


Virginia Tech

4. Chu, Teik Lin. Effects of Mach Number and Flow Incidence on Aerodynamic Losses of Steam Turbine Blades.

Degree: MS, Mechanical Engineering, 1997, Virginia Tech

 An experiment was conducted to investigate the aerodynamic losses of two high-pressure steam turbine nozzles (526A, 525B) subjected to a large range of incident angle… (more)

Subjects/Keywords: Steam Turbine; Nozzle; Aerodynamic Loss; Transonic

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APA (6th Edition):

Chu, T. L. (1997). Effects of Mach Number and Flow Incidence on Aerodynamic Losses of Steam Turbine Blades. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/10093

Chicago Manual of Style (16th Edition):

Chu, Teik Lin. “Effects of Mach Number and Flow Incidence on Aerodynamic Losses of Steam Turbine Blades.” 1997. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/10093.

MLA Handbook (7th Edition):

Chu, Teik Lin. “Effects of Mach Number and Flow Incidence on Aerodynamic Losses of Steam Turbine Blades.” 1997. Web. 18 Jan 2021.

Vancouver:

Chu TL. Effects of Mach Number and Flow Incidence on Aerodynamic Losses of Steam Turbine Blades. [Internet] [Masters thesis]. Virginia Tech; 1997. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/10093.

Council of Science Editors:

Chu TL. Effects of Mach Number and Flow Incidence on Aerodynamic Losses of Steam Turbine Blades. [Masters Thesis]. Virginia Tech; 1997. Available from: http://hdl.handle.net/10919/10093


KTH

5. Guedez, Rafael. Implementation And Validation Of Loss Prediction Methods To An Existing One Dimensional Axial Turbine Design Program.

Degree: Heat and Power Technology, 2011, KTH

  One of the early steps in axial turbine design is the use of one-dimensional (1D) mean line calculations to predict the turbine performance and… (more)

Subjects/Keywords: turbine design; turbomachinery; loss correlations; Kacker-Okapuu; Craig-Cox; Denton; aerodynamic loss; numerical tool; validation process and parametric study

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APA (6th Edition):

Guedez, R. (2011). Implementation And Validation Of Loss Prediction Methods To An Existing One Dimensional Axial Turbine Design Program. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-154033

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):

Guedez, Rafael. “Implementation And Validation Of Loss Prediction Methods To An Existing One Dimensional Axial Turbine Design Program.” 2011. Thesis, KTH. Accessed January 18, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-154033.

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

MLA Handbook (7th Edition):

Guedez, Rafael. “Implementation And Validation Of Loss Prediction Methods To An Existing One Dimensional Axial Turbine Design Program.” 2011. Web. 18 Jan 2021.

Vancouver:

Guedez R. Implementation And Validation Of Loss Prediction Methods To An Existing One Dimensional Axial Turbine Design Program. [Internet] [Thesis]. KTH; 2011. [cited 2021 Jan 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-154033.

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

Council of Science Editors:

Guedez R. Implementation And Validation Of Loss Prediction Methods To An Existing One Dimensional Axial Turbine Design Program. [Thesis]. KTH; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-154033

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


KTH

6. Leung, Pak Wing. Aerodynamic Loss Co-Relations and Flow- Field Investigations of a Transonic Film- Cooled Nozzle Guide Vane.

Degree: Heat and Power Technology, 2015, KTH

  Over the last two decades, most developed countries have reached a consensus that greener energy production is necessary for the world, due to the… (more)

Subjects/Keywords: gas turbine; aerodynamics; secondary flow; external cooling; film cooling; aerodynamic loss; high pressure turbine; nozzle guide vane

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APA (6th Edition):

Leung, P. W. (2015). Aerodynamic Loss Co-Relations and Flow- Field Investigations of a Transonic Film- Cooled Nozzle Guide Vane. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-162130

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):

Leung, Pak Wing. “Aerodynamic Loss Co-Relations and Flow- Field Investigations of a Transonic Film- Cooled Nozzle Guide Vane.” 2015. Thesis, KTH. Accessed January 18, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-162130.

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

MLA Handbook (7th Edition):

Leung, Pak Wing. “Aerodynamic Loss Co-Relations and Flow- Field Investigations of a Transonic Film- Cooled Nozzle Guide Vane.” 2015. Web. 18 Jan 2021.

Vancouver:

Leung PW. Aerodynamic Loss Co-Relations and Flow- Field Investigations of a Transonic Film- Cooled Nozzle Guide Vane. [Internet] [Thesis]. KTH; 2015. [cited 2021 Jan 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-162130.

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

Council of Science Editors:

Leung PW. Aerodynamic Loss Co-Relations and Flow- Field Investigations of a Transonic Film- Cooled Nozzle Guide Vane. [Thesis]. KTH; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-162130

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


Brno University of Technology

7. Kudela, Libor. Aerodynamický výpocet vzduchové části parního kotle: Aerodynamic Calculation of Air Part of Steam Boiler.

Degree: 2018, Brno University of Technology

 The aim of this thesis is to realize analysis of problematics of aerodynamic calculations of steam boilers on the part of combustion air. On the… (more)

Subjects/Keywords: Aerodynamický výpočet; spalovací vzduch; sací trakt; tlaková ztráta; Aerodynamic calculation; combustion air; inlet tract; pressure loss

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APA (6th Edition):

Kudela, L. (2018). Aerodynamický výpocet vzduchové části parního kotle: Aerodynamic Calculation of Air Part of Steam Boiler. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/67137

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):

Kudela, Libor. “Aerodynamický výpocet vzduchové části parního kotle: Aerodynamic Calculation of Air Part of Steam Boiler.” 2018. Thesis, Brno University of Technology. Accessed January 18, 2021. http://hdl.handle.net/11012/67137.

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

MLA Handbook (7th Edition):

Kudela, Libor. “Aerodynamický výpocet vzduchové části parního kotle: Aerodynamic Calculation of Air Part of Steam Boiler.” 2018. Web. 18 Jan 2021.

Vancouver:

Kudela L. Aerodynamický výpocet vzduchové části parního kotle: Aerodynamic Calculation of Air Part of Steam Boiler. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11012/67137.

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

Council of Science Editors:

Kudela L. Aerodynamický výpocet vzduchové části parního kotle: Aerodynamic Calculation of Air Part of Steam Boiler. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/67137

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


Louisiana State University

8. Leedom, David Houston. Numerical investigation of film cooling fluid flow and heat transfer using large eddy simulations.

Degree: MSME, Mechanical Engineering, 2009, Louisiana State University

  Large eddy simulations of film cooling from discrete holes inclined at 35° with a feeding plenum chamber are performed at a density ratio of… (more)

Subjects/Keywords: pressure loss; aerodynamic loss; jetting; adiabatic effectiveness; L/D effects; shaped holes; console

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APA (6th Edition):

Leedom, D. H. (2009). Numerical investigation of film cooling fluid flow and heat transfer using large eddy simulations. (Masters Thesis). Louisiana State University. Retrieved from etd-04142009-142923 ; https://digitalcommons.lsu.edu/gradschool_theses/4261

Chicago Manual of Style (16th Edition):

Leedom, David Houston. “Numerical investigation of film cooling fluid flow and heat transfer using large eddy simulations.” 2009. Masters Thesis, Louisiana State University. Accessed January 18, 2021. etd-04142009-142923 ; https://digitalcommons.lsu.edu/gradschool_theses/4261.

MLA Handbook (7th Edition):

Leedom, David Houston. “Numerical investigation of film cooling fluid flow and heat transfer using large eddy simulations.” 2009. Web. 18 Jan 2021.

Vancouver:

Leedom DH. Numerical investigation of film cooling fluid flow and heat transfer using large eddy simulations. [Internet] [Masters thesis]. Louisiana State University; 2009. [cited 2021 Jan 18]. Available from: etd-04142009-142923 ; https://digitalcommons.lsu.edu/gradschool_theses/4261.

Council of Science Editors:

Leedom DH. Numerical investigation of film cooling fluid flow and heat transfer using large eddy simulations. [Masters Thesis]. Louisiana State University; 2009. Available from: etd-04142009-142923 ; https://digitalcommons.lsu.edu/gradschool_theses/4261


Virginia Tech

9. Douglas, Justin W. Effects of Free Stream Turbulence on Compressor Cascade Performance.

Degree: MS, Mechanical Engineering, 2001, Virginia Tech

 The effects of grid generated free-stream turbulence on compressor cascade performance was measured experimentally in the Virginia Tech blow-down wind tunnel. The parameter of key… (more)

Subjects/Keywords: Compressor Cascade; Anemometer; Hotwire; Aerodynamic Loss; Turbulence Grid; Boundary Layer Transition

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APA (6th Edition):

Douglas, J. W. (2001). Effects of Free Stream Turbulence on Compressor Cascade Performance. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31449

Chicago Manual of Style (16th Edition):

Douglas, Justin W. “Effects of Free Stream Turbulence on Compressor Cascade Performance.” 2001. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/31449.

MLA Handbook (7th Edition):

Douglas, Justin W. “Effects of Free Stream Turbulence on Compressor Cascade Performance.” 2001. Web. 18 Jan 2021.

Vancouver:

Douglas JW. Effects of Free Stream Turbulence on Compressor Cascade Performance. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/31449.

Council of Science Editors:

Douglas JW. Effects of Free Stream Turbulence on Compressor Cascade Performance. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/31449


Virginia Tech

10. Carter, Casey Joseph. Aerodynamic Performance of a Flow Controlled Compressor Stator Using an Imbedded Ejector Pump.

Degree: MS, Mechanical Engineering, 2001, Virginia Tech

 A high-turning compressor stator with a unique flow control design was developed and tested. Both boundary layer suction and trailing edge blowing developed from a… (more)

Subjects/Keywords: Flow Control; Compressor Cascade; Trailing Edge Blowing; Aerodynamic Loss; Boundary Layer Suction

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APA (6th Edition):

Carter, C. J. (2001). Aerodynamic Performance of a Flow Controlled Compressor Stator Using an Imbedded Ejector Pump. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31297

Chicago Manual of Style (16th Edition):

Carter, Casey Joseph. “Aerodynamic Performance of a Flow Controlled Compressor Stator Using an Imbedded Ejector Pump.” 2001. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/31297.

MLA Handbook (7th Edition):

Carter, Casey Joseph. “Aerodynamic Performance of a Flow Controlled Compressor Stator Using an Imbedded Ejector Pump.” 2001. Web. 18 Jan 2021.

Vancouver:

Carter CJ. Aerodynamic Performance of a Flow Controlled Compressor Stator Using an Imbedded Ejector Pump. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/31297.

Council of Science Editors:

Carter CJ. Aerodynamic Performance of a Flow Controlled Compressor Stator Using an Imbedded Ejector Pump. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/31297


Virginia Tech

11. Vandeputte, Thomas William. Effects of Flow Control on the Aerodynamics of a Tandem Inlet Guide Vane.

Degree: MS, Mechanical Engineering, 2000, Virginia Tech

 An aerodynamic investigation was performed to assess the effectiveness of combined boundary layer suction and trailing edge blowing at reducing the blade profile losses and… (more)

Subjects/Keywords: flow control; boundary layer suction; aerodynamic loss; trailing edge blowing; inlet guide vane

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APA (6th Edition):

Vandeputte, T. W. (2000). Effects of Flow Control on the Aerodynamics of a Tandem Inlet Guide Vane. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31011

Chicago Manual of Style (16th Edition):

Vandeputte, Thomas William. “Effects of Flow Control on the Aerodynamics of a Tandem Inlet Guide Vane.” 2000. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/31011.

MLA Handbook (7th Edition):

Vandeputte, Thomas William. “Effects of Flow Control on the Aerodynamics of a Tandem Inlet Guide Vane.” 2000. Web. 18 Jan 2021.

Vancouver:

Vandeputte TW. Effects of Flow Control on the Aerodynamics of a Tandem Inlet Guide Vane. [Internet] [Masters thesis]. Virginia Tech; 2000. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/31011.

Council of Science Editors:

Vandeputte TW. Effects of Flow Control on the Aerodynamics of a Tandem Inlet Guide Vane. [Masters Thesis]. Virginia Tech; 2000. Available from: http://hdl.handle.net/10919/31011

12. Fiore, Maxime. Influence of cavity flow on turbine aerodynamics : Influence des écoulements de cavité inter-disque sur l'aérodynamique d'une turbine.

Degree: Docteur es, Dynamique des fluides, 2019, Toulouse, ISAE

Afin de faire face aux fortes températures rencontrées par les composantsen aval de la chambre de combustion, des prélèvements d’air plus frais sont réalisésau niveau… (more)

Subjects/Keywords: Aérodynamique turbine; Écoulements de purge en pied d’aube; Espace inter-Disque; Entrefer; Processus de mélange; Pertes; Simulations numériques; Axial turbine aerodynamic; Cavity purge flow; Wheel-Space; Rim seal; Mixing processes; Loss accounting; Exergy analysis; Numerical simulation; 532

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APA (6th Edition):

Fiore, M. (2019). Influence of cavity flow on turbine aerodynamics : Influence des écoulements de cavité inter-disque sur l'aérodynamique d'une turbine. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2019ESAE0013

Chicago Manual of Style (16th Edition):

Fiore, Maxime. “Influence of cavity flow on turbine aerodynamics : Influence des écoulements de cavité inter-disque sur l'aérodynamique d'une turbine.” 2019. Doctoral Dissertation, Toulouse, ISAE. Accessed January 18, 2021. http://www.theses.fr/2019ESAE0013.

MLA Handbook (7th Edition):

Fiore, Maxime. “Influence of cavity flow on turbine aerodynamics : Influence des écoulements de cavité inter-disque sur l'aérodynamique d'une turbine.” 2019. Web. 18 Jan 2021.

Vancouver:

Fiore M. Influence of cavity flow on turbine aerodynamics : Influence des écoulements de cavité inter-disque sur l'aérodynamique d'une turbine. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2019. [cited 2021 Jan 18]. Available from: http://www.theses.fr/2019ESAE0013.

Council of Science Editors:

Fiore M. Influence of cavity flow on turbine aerodynamics : Influence des écoulements de cavité inter-disque sur l'aérodynamique d'une turbine. [Doctoral Dissertation]. Toulouse, ISAE; 2019. Available from: http://www.theses.fr/2019ESAE0013


Virginia Tech

13. Perry, Michael. The Effect of Freestream Turbulence on Separation at Low Reynolds Numbers in a Compressor Cascade.

Degree: MS, Mechanical Engineering, 2007, Virginia Tech

 A parametric study was performed to observe and quantify the effect of varying turbulence intensities on separation and performance in a compressor cascade at low… (more)

Subjects/Keywords: Turbulence Grid; Separation; Compressor Cascade; Hotwire Anemometer; Aerodynamic Loss; Boundary Layer Transition; Oil Flow Visualization

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APA (6th Edition):

Perry, M. (2007). The Effect of Freestream Turbulence on Separation at Low Reynolds Numbers in a Compressor Cascade. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35834

Chicago Manual of Style (16th Edition):

Perry, Michael. “The Effect of Freestream Turbulence on Separation at Low Reynolds Numbers in a Compressor Cascade.” 2007. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/35834.

MLA Handbook (7th Edition):

Perry, Michael. “The Effect of Freestream Turbulence on Separation at Low Reynolds Numbers in a Compressor Cascade.” 2007. Web. 18 Jan 2021.

Vancouver:

Perry M. The Effect of Freestream Turbulence on Separation at Low Reynolds Numbers in a Compressor Cascade. [Internet] [Masters thesis]. Virginia Tech; 2007. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/35834.

Council of Science Editors:

Perry M. The Effect of Freestream Turbulence on Separation at Low Reynolds Numbers in a Compressor Cascade. [Masters Thesis]. Virginia Tech; 2007. Available from: http://hdl.handle.net/10919/35834

14. Hoff, Rein. The aeroplane spin motion and an investigation into factors affecting the aeroplane spin.

Degree: PhD, 2014, Brunel University

 A review of aeroplane spin literature is presented, including early spin research history and lessons learned from spinning trials. Despite many years of experience in… (more)

Subjects/Keywords: 629.132; Flight research; Loss of control; Laser scan of aeroplane; Vision based state estimation; Aerodynamic flow visualisation

…Rock LEV Leading Edge Vortex MAC Mean Aerodynamic Chord MATLAB Matrix Laboratory MEMS… …May 2012 3. Hoff, R.I., Gratton, G.B. Spin Induced Aerodynamic Flow Conditions on Fullscale… …recovery characteristics and also the unsteady aerodynamic flow 15 over wing and tail areas… …Jones, Aerodynamic Theory, 1935 To reduce the risk of spin flight testing, a flight test… …several cases of spin recovery problems encountered during spin flight testing resulting in loss… 

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APA (6th Edition):

Hoff, R. (2014). The aeroplane spin motion and an investigation into factors affecting the aeroplane spin. (Doctoral Dissertation). Brunel University. Retrieved from http://bura.brunel.ac.uk/handle/2438/10537 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.646241

Chicago Manual of Style (16th Edition):

Hoff, Rein. “The aeroplane spin motion and an investigation into factors affecting the aeroplane spin.” 2014. Doctoral Dissertation, Brunel University. Accessed January 18, 2021. http://bura.brunel.ac.uk/handle/2438/10537 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.646241.

MLA Handbook (7th Edition):

Hoff, Rein. “The aeroplane spin motion and an investigation into factors affecting the aeroplane spin.” 2014. Web. 18 Jan 2021.

Vancouver:

Hoff R. The aeroplane spin motion and an investigation into factors affecting the aeroplane spin. [Internet] [Doctoral dissertation]. Brunel University; 2014. [cited 2021 Jan 18]. Available from: http://bura.brunel.ac.uk/handle/2438/10537 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.646241.

Council of Science Editors:

Hoff R. The aeroplane spin motion and an investigation into factors affecting the aeroplane spin. [Doctoral Dissertation]. Brunel University; 2014. Available from: http://bura.brunel.ac.uk/handle/2438/10537 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.646241


Virginia Tech

15. Raven, Hans Rafael. Flow Control Optimization for Improvement of Fan Noise Reduction.

Degree: MS, Mechanical Engineering, 2004, Virginia Tech

 The study of the flow of a fan blade was conducted to improve tonal fan noise reduction by optimizing an existing flow control configuration. The… (more)

Subjects/Keywords: Fan; Computational Fluid Dynamics; CFD; Fan Noise Reduction; Cascade Testing; Flow Control; Wake Management; Trailing Edge Blowing; Suction Surface Blowing; Aerodynamic Loss

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APA (6th Edition):

Raven, H. R. (2004). Flow Control Optimization for Improvement of Fan Noise Reduction. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30847

Chicago Manual of Style (16th Edition):

Raven, Hans Rafael. “Flow Control Optimization for Improvement of Fan Noise Reduction.” 2004. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/30847.

MLA Handbook (7th Edition):

Raven, Hans Rafael. “Flow Control Optimization for Improvement of Fan Noise Reduction.” 2004. Web. 18 Jan 2021.

Vancouver:

Raven HR. Flow Control Optimization for Improvement of Fan Noise Reduction. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/30847.

Council of Science Editors:

Raven HR. Flow Control Optimization for Improvement of Fan Noise Reduction. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/30847


Georgia Tech

16. Murch, Austin Matthew. Aerodynamic Modeling of Post-Stall and Spin Dynamics of Large Transport Airplanes.

Degree: MS, Aerospace Engineering, 2007, Georgia Tech

 This work addressed aerodynamic modeling methods for prediction of post-stall flight dynamics of large transport aircraft. This was accomplished by applying historically successful modeling methods… (more)

Subjects/Keywords: Aerodynamic modeling; Post-stall; Spin; Flight dynamics; Transport; Forced oscillation; Rotary balance; Free-spin; Direct resolution; Kalviste; Excess roll rate; Loss-of-control; Upsets; Modeling; Wind tunnel testing

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APA (6th Edition):

Murch, A. M. (2007). Aerodynamic Modeling of Post-Stall and Spin Dynamics of Large Transport Airplanes. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/18855

Chicago Manual of Style (16th Edition):

Murch, Austin Matthew. “Aerodynamic Modeling of Post-Stall and Spin Dynamics of Large Transport Airplanes.” 2007. Masters Thesis, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/18855.

MLA Handbook (7th Edition):

Murch, Austin Matthew. “Aerodynamic Modeling of Post-Stall and Spin Dynamics of Large Transport Airplanes.” 2007. Web. 18 Jan 2021.

Vancouver:

Murch AM. Aerodynamic Modeling of Post-Stall and Spin Dynamics of Large Transport Airplanes. [Internet] [Masters thesis]. Georgia Tech; 2007. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/18855.

Council of Science Editors:

Murch AM. Aerodynamic Modeling of Post-Stall and Spin Dynamics of Large Transport Airplanes. [Masters Thesis]. Georgia Tech; 2007. Available from: http://hdl.handle.net/1853/18855


University of Oxford

17. O'Dowd, Devin Owen. Aero-thermal performance of transonic high-pressure turbine blade tips.

Degree: PhD, 2010, University of Oxford

 This thesis presents an experimental and theoretical study of unshrouded tips on gas turbine blades with and without winglets. The goal of the winglet tip… (more)

Subjects/Keywords: 629.132; Aerodynamics and heat transfer; Aero engines; Mathematical modeling (engineering); Turbomachinery hypersonics and aerodynamics; High-Pressure Turbine; Experimental; High-Speed Linear Cascade; Transonic Flow Conditions; Cooled Winglet; Tip Gap Survey; Over-tip Leakage Flow; Heat Transfer Measurement Techniques; Infrared Thermography; Spatially-resolved; Heat Flux Reconstruction; Impulse Technique; Unshrouded Blade Tip Heat Transfer; Film Cooling Effectiveness; Net Heat Flux Reduction; Aerodynamic Loss; Three-hole Probe; 2-D Corner Conduction; Lateral Corner Correction Coefficient

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APA (6th Edition):

O'Dowd, D. O. (2010). Aero-thermal performance of transonic high-pressure turbine blade tips. (Doctoral Dissertation). University of Oxford. Retrieved from http://ora.ox.ac.uk/objects/uuid:e7b8e7d0-4973-4757-b4df-415723e7562f ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.580863

Chicago Manual of Style (16th Edition):

O'Dowd, Devin Owen. “Aero-thermal performance of transonic high-pressure turbine blade tips.” 2010. Doctoral Dissertation, University of Oxford. Accessed January 18, 2021. http://ora.ox.ac.uk/objects/uuid:e7b8e7d0-4973-4757-b4df-415723e7562f ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.580863.

MLA Handbook (7th Edition):

O'Dowd, Devin Owen. “Aero-thermal performance of transonic high-pressure turbine blade tips.” 2010. Web. 18 Jan 2021.

Vancouver:

O'Dowd DO. Aero-thermal performance of transonic high-pressure turbine blade tips. [Internet] [Doctoral dissertation]. University of Oxford; 2010. [cited 2021 Jan 18]. Available from: http://ora.ox.ac.uk/objects/uuid:e7b8e7d0-4973-4757-b4df-415723e7562f ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.580863.

Council of Science Editors:

O'Dowd DO. Aero-thermal performance of transonic high-pressure turbine blade tips. [Doctoral Dissertation]. University of Oxford; 2010. Available from: http://ora.ox.ac.uk/objects/uuid:e7b8e7d0-4973-4757-b4df-415723e7562f ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.580863

.