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You searched for subject:(pressure sensitive paint). Showing records 1 – 22 of 22 total matches.

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The Ohio State University

1. Fang, Shuo. Application of Fast-Responding Pressure-Sensitive Paint to a Hemispherical Dome in Unsteady Transonic Flow.

Degree: MS, Aero/Astro Engineering, 2010, The Ohio State University

  The current work focuses on the application of fast-responding polymer/ceramic pressure-sensitive paint (PSP) as an advanced surface pressure measurement technique for the study of… (more)

Subjects/Keywords: Aerospace Engineering; pressure-sensitive paint; paint; aerodynamics; hemisphere; hemispherical dome; phase-averaging; real-time; lifetime

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APA (6th Edition):

Fang, S. (2010). Application of Fast-Responding Pressure-Sensitive Paint to a Hemispherical Dome in Unsteady Transonic Flow. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1293736583

Chicago Manual of Style (16th Edition):

Fang, Shuo. “Application of Fast-Responding Pressure-Sensitive Paint to a Hemispherical Dome in Unsteady Transonic Flow.” 2010. Masters Thesis, The Ohio State University. Accessed September 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1293736583.

MLA Handbook (7th Edition):

Fang, Shuo. “Application of Fast-Responding Pressure-Sensitive Paint to a Hemispherical Dome in Unsteady Transonic Flow.” 2010. Web. 15 Sep 2019.

Vancouver:

Fang S. Application of Fast-Responding Pressure-Sensitive Paint to a Hemispherical Dome in Unsteady Transonic Flow. [Internet] [Masters thesis]. The Ohio State University; 2010. [cited 2019 Sep 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1293736583.

Council of Science Editors:

Fang S. Application of Fast-Responding Pressure-Sensitive Paint to a Hemispherical Dome in Unsteady Transonic Flow. [Masters Thesis]. The Ohio State University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1293736583


University of Manchester

2. Quinn, Mark Kenneth. Shock diffraction phenomena and their measurement.

Degree: PhD, 2013, University of Manchester

 The motion of shock waves is important in many fields of engineering and increasingly so with medical applications and applications to inertial confinement fusion technologies.… (more)

Subjects/Keywords: 531; Shock Waves; Shock Tube; Pressure Sensitive Paint; Particle Image Velocimetry; Pressure Sensitive Paint; Shadowgraph; Schlieren; Flow Diagnostics; Numerical Simulations; Unsteady Flow; Compressible Flow

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APA (6th Edition):

Quinn, M. K. (2013). Shock diffraction phenomena and their measurement. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/shock-diffraction-phenomena-and-their-measurement(4c41f25a-2ba2-4a4b-aa9c-cdb8bb9ba921).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.576847

Chicago Manual of Style (16th Edition):

Quinn, Mark Kenneth. “Shock diffraction phenomena and their measurement.” 2013. Doctoral Dissertation, University of Manchester. Accessed September 15, 2019. https://www.research.manchester.ac.uk/portal/en/theses/shock-diffraction-phenomena-and-their-measurement(4c41f25a-2ba2-4a4b-aa9c-cdb8bb9ba921).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.576847.

MLA Handbook (7th Edition):

Quinn, Mark Kenneth. “Shock diffraction phenomena and their measurement.” 2013. Web. 15 Sep 2019.

Vancouver:

Quinn MK. Shock diffraction phenomena and their measurement. [Internet] [Doctoral dissertation]. University of Manchester; 2013. [cited 2019 Sep 15]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/shock-diffraction-phenomena-and-their-measurement(4c41f25a-2ba2-4a4b-aa9c-cdb8bb9ba921).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.576847.

Council of Science Editors:

Quinn MK. Shock diffraction phenomena and their measurement. [Doctoral Dissertation]. University of Manchester; 2013. Available from: https://www.research.manchester.ac.uk/portal/en/theses/shock-diffraction-phenomena-and-their-measurement(4c41f25a-2ba2-4a4b-aa9c-cdb8bb9ba921).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.576847


Texas A&M University

3. Liu, Kevin. Parametric Study of Gas Turbine Film-Cooling.

Degree: 2012, Texas A&M University

 In this study, the film-cooling effectiveness in different regions of gas turbine blades was investigated with various film hole/slot configurations and mainstream flow conditions. The… (more)

Subjects/Keywords: Gas Turbine; Film-Cooling; Heat Transfer; Pressure Sensitive Paint; Transient Liquid Crystal

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APA (6th Edition):

Liu, K. (2012). Parametric Study of Gas Turbine Film-Cooling. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11495

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):

Liu, Kevin. “Parametric Study of Gas Turbine Film-Cooling.” 2012. Thesis, Texas A&M University. Accessed September 15, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11495.

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

MLA Handbook (7th Edition):

Liu, Kevin. “Parametric Study of Gas Turbine Film-Cooling.” 2012. Web. 15 Sep 2019.

Vancouver:

Liu K. Parametric Study of Gas Turbine Film-Cooling. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Sep 15]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11495.

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

Council of Science Editors:

Liu K. Parametric Study of Gas Turbine Film-Cooling. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11495

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


University of Manchester

4. Che Idris, Azam. CHARACTERIZATION OF HIGH SPEED INLETS USING GLOBAL MEASUREMENT TECHNIQUES.

Degree: 2014, University of Manchester

 After the end of the NASA space shuttle programme, there has been resurgence of interestin developing a single stage-to-orbit spacecraft. The key technology to realize… (more)

Subjects/Keywords: scramjet; hypersonic; pressure sensitive paint; Mach 5; high speed inlet; compressible flow

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APA (6th Edition):

Che Idris, A. (2014). CHARACTERIZATION OF HIGH SPEED INLETS USING GLOBAL MEASUREMENT TECHNIQUES. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:235518

Chicago Manual of Style (16th Edition):

Che Idris, Azam. “CHARACTERIZATION OF HIGH SPEED INLETS USING GLOBAL MEASUREMENT TECHNIQUES.” 2014. Doctoral Dissertation, University of Manchester. Accessed September 15, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:235518.

MLA Handbook (7th Edition):

Che Idris, Azam. “CHARACTERIZATION OF HIGH SPEED INLETS USING GLOBAL MEASUREMENT TECHNIQUES.” 2014. Web. 15 Sep 2019.

Vancouver:

Che Idris A. CHARACTERIZATION OF HIGH SPEED INLETS USING GLOBAL MEASUREMENT TECHNIQUES. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2019 Sep 15]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:235518.

Council of Science Editors:

Che Idris A. CHARACTERIZATION OF HIGH SPEED INLETS USING GLOBAL MEASUREMENT TECHNIQUES. [Doctoral Dissertation]. University of Manchester; 2014. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:235518


University of Cincinnati

5. Aghasi, Paul P. Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 To investigate the viability of using additive manufacturing technology for flat plate film cooling experiments a new experiential facility was constructed using gas analysis and… (more)

Subjects/Keywords: Aerospace Materials; Film Cooling; Heat transfer; mass transfer; pressure sensitive paint; roughness; 3D printing

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APA (6th Edition):

Aghasi, P. P. (2016). Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893416

Chicago Manual of Style (16th Edition):

Aghasi, Paul P. “Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes.” 2016. Masters Thesis, University of Cincinnati. Accessed September 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893416.

MLA Handbook (7th Edition):

Aghasi, Paul P. “Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes.” 2016. Web. 15 Sep 2019.

Vancouver:

Aghasi PP. Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes. [Internet] [Masters thesis]. University of Cincinnati; 2016. [cited 2019 Sep 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893416.

Council of Science Editors:

Aghasi PP. Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes. [Masters Thesis]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893416


University of Texas – Austin

6. -6206-5713. Simultaneous high-speed displacement and surface pressure measurements of a compliant panel under a Mach 2 compression ramp interaction.

Degree: MSin Engineering, Aerospace Engineering, 2019, University of Texas – Austin

 In this presentation we will discuss a new study of the dynamic response of a compliant panel under a shock wave/boundary layer interaction produced by… (more)

Subjects/Keywords: SWBLI; Pressure-sensitive paint; Digital image correlation; Simultaneous; Compliant; Ramp interaction; Displacement

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APA (6th Edition):

-6206-5713. (2019). Simultaneous high-speed displacement and surface pressure measurements of a compliant panel under a Mach 2 compression ramp interaction. (Masters Thesis). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/2151

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

Chicago Manual of Style (16th Edition):

-6206-5713. “Simultaneous high-speed displacement and surface pressure measurements of a compliant panel under a Mach 2 compression ramp interaction.” 2019. Masters Thesis, University of Texas – Austin. Accessed September 15, 2019. http://dx.doi.org/10.26153/tsw/2151.

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

MLA Handbook (7th Edition):

-6206-5713. “Simultaneous high-speed displacement and surface pressure measurements of a compliant panel under a Mach 2 compression ramp interaction.” 2019. Web. 15 Sep 2019.

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

Vancouver:

-6206-5713. Simultaneous high-speed displacement and surface pressure measurements of a compliant panel under a Mach 2 compression ramp interaction. [Internet] [Masters thesis]. University of Texas – Austin; 2019. [cited 2019 Sep 15]. Available from: http://dx.doi.org/10.26153/tsw/2151.

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

Council of Science Editors:

-6206-5713. Simultaneous high-speed displacement and surface pressure measurements of a compliant panel under a Mach 2 compression ramp interaction. [Masters Thesis]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/2151

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


Iowa State University

7. Yang, Zifeng. Experimental investigations on complex vortex flows using advanced flow diagnostic techniques.

Degree: 2009, Iowa State University

 Using advanced diagnostic techniques, two complex vortex flow topics were addressed in the present thesis. First, the characteristics of flow structures around building models in… (more)

Subjects/Keywords: Experiment; Film cooling effectiveness; Particle Image Velocimetry; Pressure Sensitive Paint; Tornado-like vortex; Trailing edge cooling; Aerospace Engineering

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APA (6th Edition):

Yang, Z. (2009). Experimental investigations on complex vortex flows using advanced flow diagnostic techniques. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/10979

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):

Yang, Zifeng. “Experimental investigations on complex vortex flows using advanced flow diagnostic techniques.” 2009. Thesis, Iowa State University. Accessed September 15, 2019. https://lib.dr.iastate.edu/etd/10979.

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

MLA Handbook (7th Edition):

Yang, Zifeng. “Experimental investigations on complex vortex flows using advanced flow diagnostic techniques.” 2009. Web. 15 Sep 2019.

Vancouver:

Yang Z. Experimental investigations on complex vortex flows using advanced flow diagnostic techniques. [Internet] [Thesis]. Iowa State University; 2009. [cited 2019 Sep 15]. Available from: https://lib.dr.iastate.edu/etd/10979.

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

Council of Science Editors:

Yang Z. Experimental investigations on complex vortex flows using advanced flow diagnostic techniques. [Thesis]. Iowa State University; 2009. Available from: https://lib.dr.iastate.edu/etd/10979

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


University of Illinois – Urbana-Champaign

8. Hale, Jason. Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05.

Degree: MS, 4048, 2015, University of Illinois – Urbana-Champaign

 The interaction between an impinging conical shock wave with a plane compressible turbulent boundary layer has been studied at Mach 2.05. Surface oil flow and… (more)

Subjects/Keywords: Taylor Maccoll; Cone Flow; Shock Boundary Layer Interaction (SBLI); Shock Wave Boundary Layer Interaction; Pressure Sensitive Paint; Particle Image Velocimetry; Supersonic

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APA (6th Edition):

Hale, J. (2015). Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/72992

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):

Hale, Jason. “Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05.” 2015. Thesis, University of Illinois – Urbana-Champaign. Accessed September 15, 2019. http://hdl.handle.net/2142/72992.

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

MLA Handbook (7th Edition):

Hale, Jason. “Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05.” 2015. Web. 15 Sep 2019.

Vancouver:

Hale J. Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2015. [cited 2019 Sep 15]. Available from: http://hdl.handle.net/2142/72992.

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

Council of Science Editors:

Hale J. Interaction between a conical shock wave and a plane compressible turbulent boundary layer at Mach 2.05. [Thesis]. University of Illinois – Urbana-Champaign; 2015. Available from: http://hdl.handle.net/2142/72992

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

9. Monastero, Marianne. Validation of 3-D ice accretion documentation and replication method including pressure-sensitive paint.

Degree: MS, 4048, 2014, University of Illinois – Urbana-Champaign

 Accurate representation of ice accretions is important to the study and understanding of aircraft icing. For research and certification purposes, replicas of ice accretions generated… (more)

Subjects/Keywords: icing; Pressure-sensitive Paint; Aerodynamics; Wind Tunnel

…127 Appendix A Pressure Sensitive Paint Method… …165 C.4 Pressure-Sensitive Paint Uncertainty… …Aérospatiales Pressure-sensitive paint Root mean square Rapid-prototype method ix rpm SLA SLD TsAGI… …scale ice shapes made from the 3-D laser scanner method.28 1.2 Pressure-Sensitive Paint The… …pressure-sensitive paint (PSP) method is a technique that was first developed in the… 

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APA (6th Edition):

Monastero, M. (2014). Validation of 3-D ice accretion documentation and replication method including pressure-sensitive paint. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/46651

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):

Monastero, Marianne. “Validation of 3-D ice accretion documentation and replication method including pressure-sensitive paint.” 2014. Thesis, University of Illinois – Urbana-Champaign. Accessed September 15, 2019. http://hdl.handle.net/2142/46651.

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

MLA Handbook (7th Edition):

Monastero, Marianne. “Validation of 3-D ice accretion documentation and replication method including pressure-sensitive paint.” 2014. Web. 15 Sep 2019.

Vancouver:

Monastero M. Validation of 3-D ice accretion documentation and replication method including pressure-sensitive paint. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2014. [cited 2019 Sep 15]. Available from: http://hdl.handle.net/2142/46651.

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

Council of Science Editors:

Monastero M. Validation of 3-D ice accretion documentation and replication method including pressure-sensitive paint. [Thesis]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/46651

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


Virginia Tech

10. Navarra, Kelly R. Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications.

Degree: MS, Mechanical Engineering, 1997, Virginia Tech

 A new pressure-measurement technique which employs the tools of molecular spectroscopy has recently received considerable attention in the fluid mechanics community. Measurements are made via… (more)

Subjects/Keywords: Pressure-sensitive paint; turbomachinery; optical pressure measurement techniques; luminescence quenching.

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APA (6th Edition):

Navarra, K. R. (1997). Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36840

Chicago Manual of Style (16th Edition):

Navarra, Kelly R. “Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications.” 1997. Masters Thesis, Virginia Tech. Accessed September 15, 2019. http://hdl.handle.net/10919/36840.

MLA Handbook (7th Edition):

Navarra, Kelly R. “Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications.” 1997. Web. 15 Sep 2019.

Vancouver:

Navarra KR. Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications. [Internet] [Masters thesis]. Virginia Tech; 1997. [cited 2019 Sep 15]. Available from: http://hdl.handle.net/10919/36840.

Council of Science Editors:

Navarra KR. Development of the Pressure-Sensitive-Paint Technique for Advanced Turbomachinery Applications. [Masters Thesis]. Virginia Tech; 1997. Available from: http://hdl.handle.net/10919/36840

11. Matos, Keth Rousbergue Maciel de. Filmes sensíveis a pressão pela técnica de fotoluminescência.

Degree: Mestrado, Microeletrônica, 2011, University of São Paulo

O presente projeto tem como objetivo contribuir para o desenvolvimento de dispositivos para monitoração de pressão dinâmica do ar. Para isso, foram produzidos filmes sensíveis… (more)

Subjects/Keywords: Azul de metileno; Filme fino de poliestireno; Fotoluminescência; Methylene blue; Photoluminescence; Platina octaetilporfirina; Platinum octaetilporfirina; Porous silicon; Pressure sensitive paint; Silício poroso; Thin film polystyrene; Tinta sensível à pressão

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APA (6th Edition):

Matos, K. R. M. d. (2011). Filmes sensíveis a pressão pela técnica de fotoluminescência. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/3/3140/tde-12082011-110005/ ;

Chicago Manual of Style (16th Edition):

Matos, Keth Rousbergue Maciel de. “Filmes sensíveis a pressão pela técnica de fotoluminescência.” 2011. Masters Thesis, University of São Paulo. Accessed September 15, 2019. http://www.teses.usp.br/teses/disponiveis/3/3140/tde-12082011-110005/ ;.

MLA Handbook (7th Edition):

Matos, Keth Rousbergue Maciel de. “Filmes sensíveis a pressão pela técnica de fotoluminescência.” 2011. Web. 15 Sep 2019.

Vancouver:

Matos KRMd. Filmes sensíveis a pressão pela técnica de fotoluminescência. [Internet] [Masters thesis]. University of São Paulo; 2011. [cited 2019 Sep 15]. Available from: http://www.teses.usp.br/teses/disponiveis/3/3140/tde-12082011-110005/ ;.

Council of Science Editors:

Matos KRMd. Filmes sensíveis a pressão pela técnica de fotoluminescência. [Masters Thesis]. University of São Paulo; 2011. Available from: http://www.teses.usp.br/teses/disponiveis/3/3140/tde-12082011-110005/ ;

12. Gao, Zhihong. Experimental investigation of film cooling effectiveness on gas turbine blades.

Degree: 2009, Texas A&M University

 The hot gas temperature in gas turbine engines is far above the permissible metal temperatures. Advanced cooling technologies must be applied to cool the blades,… (more)

Subjects/Keywords: gas turbine heat transfer; film cooling; Pressure Sensitive paint

…Present Study …..18 2. PRESSURE SENSITIVE PAINT MEASUREMENT THEORY AND DATA… …pressure sensitive paint to measure the film cooling effectiveness for two rows of discrete holes… …pressure sensitive paint (PSP) and transient infrared thermogrpahy technique. Funazaki… …of great pain. In this study, pressure sensitive paint (PSP) is used to… …using Pressure Sensitive Paint (PSP) technique, accurate film cooling effectiveness… 

Page 1 Page 2 Page 3 Page 4 Page 5

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APA (6th Edition):

Gao, Z. (2009). Experimental investigation of film cooling effectiveness on gas turbine blades. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1557

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):

Gao, Zhihong. “Experimental investigation of film cooling effectiveness on gas turbine blades.” 2009. Thesis, Texas A&M University. Accessed September 15, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-1557.

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

MLA Handbook (7th Edition):

Gao, Zhihong. “Experimental investigation of film cooling effectiveness on gas turbine blades.” 2009. Web. 15 Sep 2019.

Vancouver:

Gao Z. Experimental investigation of film cooling effectiveness on gas turbine blades. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Sep 15]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1557.

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

Council of Science Editors:

Gao Z. Experimental investigation of film cooling effectiveness on gas turbine blades. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1557

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

13. Balla, Joseph V. Pressure-Sensitive Paint for Detection of Boundary Layer Transition.

Degree: MS, Aero/Astro Engineering, 2012, The Ohio State University

 A polymer/ceramic pressure-sensitive paint (PSP) system was evaluated to detect the laminar -turbulent transition location. A preliminary investigation was completed at the Wright-Patterson Air Force… (more)

Subjects/Keywords: Aerospace Engineering; Pressure-sensitive paint; boundary-layer; transition

…6 Chapter 2: Pressure-Sensitive Paint… …11 ix Section 2.1: An Introduction to Pressure-Sensitive Paint… …17 Chapter 3: The Ability for Pressure-Sensitive Paint to Resolve Pressure Fluctuations… …20 Chapter 4: Pressure-Sensitive Paint Preparation, Application, and Calibration… …78 Chapter 7: Pressure-Sensitive Paint Tunnel Entries in The Ohio State 6”x22” Transonic… 

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APA (6th Edition):

Balla, J. V. (2012). Pressure-Sensitive Paint for Detection of Boundary Layer Transition. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1345552359

Chicago Manual of Style (16th Edition):

Balla, Joseph V. “Pressure-Sensitive Paint for Detection of Boundary Layer Transition.” 2012. Masters Thesis, The Ohio State University. Accessed September 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1345552359.

MLA Handbook (7th Edition):

Balla, Joseph V. “Pressure-Sensitive Paint for Detection of Boundary Layer Transition.” 2012. Web. 15 Sep 2019.

Vancouver:

Balla JV. Pressure-Sensitive Paint for Detection of Boundary Layer Transition. [Internet] [Masters thesis]. The Ohio State University; 2012. [cited 2019 Sep 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1345552359.

Council of Science Editors:

Balla JV. Pressure-Sensitive Paint for Detection of Boundary Layer Transition. [Masters Thesis]. The Ohio State University; 2012. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1345552359


Iowa State University

14. Zhou, Wenwu. Novel cooling strategies for improved protection of gas turbine blades.

Degree: 2016, Iowa State University

 Modern gas turbines are operating at peak turbine inlet temperature well beyond the maximum endurable temperature of turbine blade material. As a result, hot gas-contacting… (more)

Subjects/Keywords: Aerospace Engineering; Barchan dune; Compressility effect; Improved film cooling of gas turbine; Internal cooling; Pressure Sensitive Paint; (Stereoscopic) Particle Image Velocimetry; Aerospace Engineering

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

APA (6th Edition):

Zhou, W. (2016). Novel cooling strategies for improved protection of gas turbine blades. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/15167

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):

Zhou, Wenwu. “Novel cooling strategies for improved protection of gas turbine blades.” 2016. Thesis, Iowa State University. Accessed September 15, 2019. https://lib.dr.iastate.edu/etd/15167.

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

MLA Handbook (7th Edition):

Zhou, Wenwu. “Novel cooling strategies for improved protection of gas turbine blades.” 2016. Web. 15 Sep 2019.

Vancouver:

Zhou W. Novel cooling strategies for improved protection of gas turbine blades. [Internet] [Thesis]. Iowa State University; 2016. [cited 2019 Sep 15]. Available from: https://lib.dr.iastate.edu/etd/15167.

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

Council of Science Editors:

Zhou W. Novel cooling strategies for improved protection of gas turbine blades. [Thesis]. Iowa State University; 2016. Available from: https://lib.dr.iastate.edu/etd/15167

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


Northeastern University

15. Yao, Yuan. An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique.

Degree: MS, Department of Mechanical and Industrial Engineering, 2019, Northeastern University

 Since the invention of the gas turbine technology, countless engineers and scientists have been trying their best to refine this type of machine. One of… (more)

Subjects/Keywords: Anti-counter-rotating vortices; Blowing ratio; Film cooling; Film cooling effectiveness; Pressure Sensitive Paint; 'V-shaped' film cooling hole; Mechanical engineering; Aerospace engineering

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

APA (6th Edition):

Yao, Y. (2019). An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/D20317909

Chicago Manual of Style (16th Edition):

Yao, Yuan. “An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique.” 2019. Masters Thesis, Northeastern University. Accessed September 15, 2019. http://hdl.handle.net/2047/D20317909.

MLA Handbook (7th Edition):

Yao, Yuan. “An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique.” 2019. Web. 15 Sep 2019.

Vancouver:

Yao Y. An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique. [Internet] [Masters thesis]. Northeastern University; 2019. [cited 2019 Sep 15]. Available from: http://hdl.handle.net/2047/D20317909.

Council of Science Editors:

Yao Y. An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique. [Masters Thesis]. Northeastern University; 2019. Available from: http://hdl.handle.net/2047/D20317909

16. Quinn, Mark Kenneth. Shock Diffraction Phenomena and their Measurement.

Degree: 2013, University of Manchester

 The motion of shock waves is important in many fields of engineering and increasingly so with medical applications and applications to inertial confinement fusion technologies.… (more)

Subjects/Keywords: Shock Waves; Shock Tube; Pressure Sensitive Paint; Particle Image Velocimetry; Pressure Sensitive Paint; Shadowgraph; Schlieren; Flow Diagnostics; Numerical Simulations; Unsteady Flow; Compressible Flow

…Science 18:58-66, 2013 2. M. K. Quinn, K. Kontis. Pressure-Sensitive Paint Measurements of… …2012 5. M. K. Quinn, L. Yang, K. Kontis. Pressure-Sensitive Paint: Effect of Substrate… …Ireland. Application of Pressure-Sensitive Paint to Low-speed Flow Around a U-Bend of Strong… …sensitive paint (PSP) and traditional pressure transducers were used to quantify the… …velocimetry and pressure-sensitive paint) and compare with simulations using commercial… 

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APA (6th Edition):

Quinn, M. K. (2013). Shock Diffraction Phenomena and their Measurement. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:195566

Chicago Manual of Style (16th Edition):

Quinn, Mark Kenneth. “Shock Diffraction Phenomena and their Measurement.” 2013. Doctoral Dissertation, University of Manchester. Accessed September 15, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:195566.

MLA Handbook (7th Edition):

Quinn, Mark Kenneth. “Shock Diffraction Phenomena and their Measurement.” 2013. Web. 15 Sep 2019.

Vancouver:

Quinn MK. Shock Diffraction Phenomena and their Measurement. [Internet] [Doctoral dissertation]. University of Manchester; 2013. [cited 2019 Sep 15]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:195566.

Council of Science Editors:

Quinn MK. Shock Diffraction Phenomena and their Measurement. [Doctoral Dissertation]. University of Manchester; 2013. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:195566

17. Wright, Joseph. Oxygen-Sensitive Luminophores: A Survey of the Literature and Efforts toward a Novel Porphyrin-Pillared Zirconium Phosphonate.

Degree: MS, Chemistry, 2016, University of Vermont

  Measurement and mapping of the pressure distribution across the surface of a suitably scaled model is an integral step in the design of any… (more)

Subjects/Keywords: luminophore; metalloporphyrin; pressure-sensitive paint; PSP; ruthenium polypyridyl complex; zirconium phosphonate; Chemistry; Physical Chemistry

…x29; PSP pressure-sensitive paint PSS poly(styrene-4-sulfonate) PSU polysulfone… …in pressure-sensitive paints… …incorporated into oxygen- and pressure-sensitive luminophores. ..................96 Figure 14… …SENSITIVE PAINTS 1.1 Definition, Motivation, and Historical Remarks Pressure-sensitive paints… …29 Table 3. Selected performance characteristics of oxygen-sensitive materials based on… 

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APA (6th Edition):

Wright, J. (2016). Oxygen-Sensitive Luminophores: A Survey of the Literature and Efforts toward a Novel Porphyrin-Pillared Zirconium Phosphonate. (Thesis). University of Vermont. Retrieved from https://scholarworks.uvm.edu/graddis/653

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):

Wright, Joseph. “Oxygen-Sensitive Luminophores: A Survey of the Literature and Efforts toward a Novel Porphyrin-Pillared Zirconium Phosphonate.” 2016. Thesis, University of Vermont. Accessed September 15, 2019. https://scholarworks.uvm.edu/graddis/653.

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

MLA Handbook (7th Edition):

Wright, Joseph. “Oxygen-Sensitive Luminophores: A Survey of the Literature and Efforts toward a Novel Porphyrin-Pillared Zirconium Phosphonate.” 2016. Web. 15 Sep 2019.

Vancouver:

Wright J. Oxygen-Sensitive Luminophores: A Survey of the Literature and Efforts toward a Novel Porphyrin-Pillared Zirconium Phosphonate. [Internet] [Thesis]. University of Vermont; 2016. [cited 2019 Sep 15]. Available from: https://scholarworks.uvm.edu/graddis/653.

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

Council of Science Editors:

Wright J. Oxygen-Sensitive Luminophores: A Survey of the Literature and Efforts toward a Novel Porphyrin-Pillared Zirconium Phosphonate. [Thesis]. University of Vermont; 2016. Available from: https://scholarworks.uvm.edu/graddis/653

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


EPFL

18. Jonsson, Magnus. Application of Photoluminescent Measurement Techniques for Quantitative Assessment of Turbine Film Cooling.

Degree: 2010, EPFL

 Reduction of the specific fuel consumption of gas turbines can be achieved by maximizing the turbine inlet temperature. However, this requires a detailed understanding of… (more)

Subjects/Keywords: film cooling; convective heat transfer; photoluminescence; pressure sensitive paint; gas concentration; transient heating experiments; flow measurement; measurement technique; refroidissement par film (film cooling); transfert de chaleur; convection; photo-luminescence; PSP; concentration de gaz; expériences transitoires; Flow Measurements; Heat Transfer; Measurement Techniques

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

APA (6th Edition):

Jonsson, M. (2010). Application of Photoluminescent Measurement Techniques for Quantitative Assessment of Turbine Film Cooling. (Thesis). EPFL. Retrieved from http://infoscience.epfl.ch/record/145890

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):

Jonsson, Magnus. “Application of Photoluminescent Measurement Techniques for Quantitative Assessment of Turbine Film Cooling.” 2010. Thesis, EPFL. Accessed September 15, 2019. http://infoscience.epfl.ch/record/145890.

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

MLA Handbook (7th Edition):

Jonsson, Magnus. “Application of Photoluminescent Measurement Techniques for Quantitative Assessment of Turbine Film Cooling.” 2010. Web. 15 Sep 2019.

Vancouver:

Jonsson M. Application of Photoluminescent Measurement Techniques for Quantitative Assessment of Turbine Film Cooling. [Internet] [Thesis]. EPFL; 2010. [cited 2019 Sep 15]. Available from: http://infoscience.epfl.ch/record/145890.

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

Council of Science Editors:

Jonsson M. Application of Photoluminescent Measurement Techniques for Quantitative Assessment of Turbine Film Cooling. [Thesis]. EPFL; 2010. Available from: http://infoscience.epfl.ch/record/145890

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

19. Che Idris, Azam. Characterization of high speed inlets using global measurement techniques.

Degree: PhD, 2014, University of Manchester

 After the end of the NASA space shuttle programme, there has been resurgence of interest in developing a single stage-to-orbit spacecraft. The key technology to… (more)

Subjects/Keywords: 629.134; scramjet; hypersonic; pressure sensitive paint; Mach 5; high speed inlet; compressible flow

…245 B. Pressure Sensitive Paint (PSP) Theory… …generator PIV Particle image velocimetry PSP Pressure sensitive paint PtTFPP Ru(II)… …provide an abundance of information on inlet flow. The pressure sensitive paint method was… …boundary layer interactions TSP Temperature sensitive paint TR Throttling ratio TLC Thin… …Mach number, stagnation pressure and temperature (figure taken from Erdem71)… 

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APA (6th Edition):

Che Idris, A. (2014). Characterization of high speed inlets using global measurement techniques. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/characterization-of-high-speed-inlets-using-global-measurement-techniques(ca8b687b-aff0-4b50-892f-897a962e22ba).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.626963

Chicago Manual of Style (16th Edition):

Che Idris, Azam. “Characterization of high speed inlets using global measurement techniques.” 2014. Doctoral Dissertation, University of Manchester. Accessed September 15, 2019. https://www.research.manchester.ac.uk/portal/en/theses/characterization-of-high-speed-inlets-using-global-measurement-techniques(ca8b687b-aff0-4b50-892f-897a962e22ba).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.626963.

MLA Handbook (7th Edition):

Che Idris, Azam. “Characterization of high speed inlets using global measurement techniques.” 2014. Web. 15 Sep 2019.

Vancouver:

Che Idris A. Characterization of high speed inlets using global measurement techniques. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2019 Sep 15]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/characterization-of-high-speed-inlets-using-global-measurement-techniques(ca8b687b-aff0-4b50-892f-897a962e22ba).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.626963.

Council of Science Editors:

Che Idris A. Characterization of high speed inlets using global measurement techniques. [Doctoral Dissertation]. University of Manchester; 2014. Available from: https://www.research.manchester.ac.uk/portal/en/theses/characterization-of-high-speed-inlets-using-global-measurement-techniques(ca8b687b-aff0-4b50-892f-897a962e22ba).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.626963

20. Jensen, Christopher Douglas. Global Pressure and Temperature Surface Measurements on a NACA 0012 Airfoil in Oscillatory Compressible Flow at Low Reduced Frequencies.

Degree: MS, Aero/Astro Engineering, 2012, The Ohio State University

 A co-axial contra-rotating helicopter in forward flight has stall mechanisms that are intrinsically different from those on a traditional helicopter. Traditional helicopters need a cyclic… (more)

Subjects/Keywords: Aerospace Engineering; PSP; TSP; pressure sensitive paint; aerodynamics; Mach oscillation; freestream oscillation; NACA 0012

…Palluconi, S.. "Temperature-Compensated Fast Pressure-Sensitive Paint" In: Proceedings… …25 Chapter 4: Pressure Sensitive Paint… …31 Section 4.1: Pressure Sensitive Paint Introduction… …32 Section 4.3: Temperature Compensating Pressure Sensitive Paint… …46 Section 5.2: Pressure and Temperature Sensitive Paint Experimental Setup ........... 47… 

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

APA (6th Edition):

Jensen, C. D. (2012). Global Pressure and Temperature Surface Measurements on a NACA 0012 Airfoil in Oscillatory Compressible Flow at Low Reduced Frequencies. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1331075431

Chicago Manual of Style (16th Edition):

Jensen, Christopher Douglas. “Global Pressure and Temperature Surface Measurements on a NACA 0012 Airfoil in Oscillatory Compressible Flow at Low Reduced Frequencies.” 2012. Masters Thesis, The Ohio State University. Accessed September 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1331075431.

MLA Handbook (7th Edition):

Jensen, Christopher Douglas. “Global Pressure and Temperature Surface Measurements on a NACA 0012 Airfoil in Oscillatory Compressible Flow at Low Reduced Frequencies.” 2012. Web. 15 Sep 2019.

Vancouver:

Jensen CD. Global Pressure and Temperature Surface Measurements on a NACA 0012 Airfoil in Oscillatory Compressible Flow at Low Reduced Frequencies. [Internet] [Masters thesis]. The Ohio State University; 2012. [cited 2019 Sep 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1331075431.

Council of Science Editors:

Jensen CD. Global Pressure and Temperature Surface Measurements on a NACA 0012 Airfoil in Oscillatory Compressible Flow at Low Reduced Frequencies. [Masters Thesis]. The Ohio State University; 2012. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1331075431

21. Blake, Sarah Anne. Turbine blade platform film cooling with simulated stator-rotor purge flow with varied seal width and upstream wake with vortex.

Degree: 2009, Texas A&M University

 The turbine blade platform can be protected from hot mainstream gases by injecting cooler air through the gap between stator and rotor. The effectiveness of… (more)

Subjects/Keywords: gas turbine; rotor; platform; film cooling; vane; unsteady wake; passage vortex; stator-rotor seal; slot injection; pressure-sensitive paint; film cooling effectiveness

…45°. Pressure-Sensitive Paint Measurement Technique In each test, the film cooling… …Figure 6. 14 Figure 6: Calibration Curve for Pressure-Sensitive Paint Relating Intensity… …pressure of oxygen in the mixture of air and nitrogen near the surface. First, the paint must be… …continues onto the pressure side of the vane, but the pressure gradient across the passage causes… …the pressure-side leg to move across the passage toward the suction side of the adjacent… 

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APA (6th Edition):

Blake, S. A. (2009). Turbine blade platform film cooling with simulated stator-rotor purge flow with varied seal width and upstream wake with vortex. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1340

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):

Blake, Sarah Anne. “Turbine blade platform film cooling with simulated stator-rotor purge flow with varied seal width and upstream wake with vortex.” 2009. Thesis, Texas A&M University. Accessed September 15, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-1340.

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

MLA Handbook (7th Edition):

Blake, Sarah Anne. “Turbine blade platform film cooling with simulated stator-rotor purge flow with varied seal width and upstream wake with vortex.” 2009. Web. 15 Sep 2019.

Vancouver:

Blake SA. Turbine blade platform film cooling with simulated stator-rotor purge flow with varied seal width and upstream wake with vortex. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Sep 15]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1340.

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

Council of Science Editors:

Blake SA. Turbine blade platform film cooling with simulated stator-rotor purge flow with varied seal width and upstream wake with vortex. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1340

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

22. Herges, Thomas. The effects of micro-vortex generators on normal shock wave/boundary layer interactions.

Degree: PhD, 4048, 2014, University of Illinois – Urbana-Champaign

 Shock wave/boundary-layer interactions (SWBLIs) are complex flow phenomena that are important in the design and performance of internal supersonic and transonic flow fields such as… (more)

Subjects/Keywords: shock wave boundary layer interactions (SWBLI); normal shock wave; boundary layer; supersonic flow; vortex generators; SWBLI control; shock wave unsteadiness; supersonic inlet; supersonic inlet control; inlet buzz; optical diagnostic techniques; camera housing; schlieren imaging; surface oil flow visualization; pressure sensitive paint; particle image velocimetry; shear stress measurements; format figure references in Microsoft Word

pressure-sensitive paint uncertainty parameter (Equation (13)) acoustic… …implementing schlieren photography, surface oil-flow visualization, pressure-sensitive paint, and… …access for schlieren photography, surface oil-flow visualization, pressure-sensitive paint… …sensitive paint (PSP), and particle image velocimetry (PIV). Both time… …x29; static pressure, kPa stagnation pressure, kPa freestream static pressure, kPa… 

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

APA (6th Edition):

Herges, T. (2014). The effects of micro-vortex generators on normal shock wave/boundary layer interactions. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/46573

Chicago Manual of Style (16th Edition):

Herges, Thomas. “The effects of micro-vortex generators on normal shock wave/boundary layer interactions.” 2014. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed September 15, 2019. http://hdl.handle.net/2142/46573.

MLA Handbook (7th Edition):

Herges, Thomas. “The effects of micro-vortex generators on normal shock wave/boundary layer interactions.” 2014. Web. 15 Sep 2019.

Vancouver:

Herges T. The effects of micro-vortex generators on normal shock wave/boundary layer interactions. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2014. [cited 2019 Sep 15]. Available from: http://hdl.handle.net/2142/46573.

Council of Science Editors:

Herges T. The effects of micro-vortex generators on normal shock wave/boundary layer interactions. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/46573

.