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You searched for subject:(supersonic jet). Showing records 1 – 30 of 74 total matches.

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Penn State University

1. Miller, Steven Arthur Eric. The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions.

Degree: PhD, Aerospace Engineering, 2009, Penn State University

 Broadband shock-associated noise is a component of jet noise generated by supersonic jets operating off-design. It is characterized by multiple broadband peaks and dominates the… (more)

Subjects/Keywords: Jet; Noise; Supersonic; Fluid Dynamics; Shock; Broadband

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APA (6th Edition):

Miller, S. A. E. (2009). The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9945

Chicago Manual of Style (16th Edition):

Miller, Steven Arthur Eric. “The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions.” 2009. Doctoral Dissertation, Penn State University. Accessed August 10, 2020. https://etda.libraries.psu.edu/catalog/9945.

MLA Handbook (7th Edition):

Miller, Steven Arthur Eric. “The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions.” 2009. Web. 10 Aug 2020.

Vancouver:

Miller SAE. The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions. [Internet] [Doctoral dissertation]. Penn State University; 2009. [cited 2020 Aug 10]. Available from: https://etda.libraries.psu.edu/catalog/9945.

Council of Science Editors:

Miller SAE. The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions. [Doctoral Dissertation]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9945


Penn State University

2. Powers, Russell. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.

Degree: PhD, Aerospace Engineering, 2015, Penn State University

 The noise produced by the supersonic, high temperature jets that exhaust from military aircraft is becoming a hazard to naval personnel and a disturbance to… (more)

Subjects/Keywords: Jet Noise; Supersonic; Aeroacoustics; Noise Reduction

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APA (6th Edition):

Powers, R. (2015). Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/26397

Chicago Manual of Style (16th Edition):

Powers, Russell. “Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.” 2015. Doctoral Dissertation, Penn State University. Accessed August 10, 2020. https://etda.libraries.psu.edu/catalog/26397.

MLA Handbook (7th Edition):

Powers, Russell. “Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.” 2015. Web. 10 Aug 2020.

Vancouver:

Powers R. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. [Internet] [Doctoral dissertation]. Penn State University; 2015. [cited 2020 Aug 10]. Available from: https://etda.libraries.psu.edu/catalog/26397.

Council of Science Editors:

Powers R. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. [Doctoral Dissertation]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/26397


University of Minnesota

3. Kreitzman, Jordan. Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet.

Degree: MS, Aerospace Engineering and Mechanics, 2015, University of Minnesota

 Source terms corresponding to Goldstein's generalized acoustic analogy are computed from a high-fidelity simulation of a supersonic jet issuing from a rectangular nozzle with chevrons.… (more)

Subjects/Keywords: acoustic; chevron; jet; rectangular; source; supersonic

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APA (6th Edition):

Kreitzman, J. (2015). Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet. (Masters Thesis). University of Minnesota. Retrieved from http://hdl.handle.net/11299/174797

Chicago Manual of Style (16th Edition):

Kreitzman, Jordan. “Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet.” 2015. Masters Thesis, University of Minnesota. Accessed August 10, 2020. http://hdl.handle.net/11299/174797.

MLA Handbook (7th Edition):

Kreitzman, Jordan. “Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet.” 2015. Web. 10 Aug 2020.

Vancouver:

Kreitzman J. Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet. [Internet] [Masters thesis]. University of Minnesota; 2015. [cited 2020 Aug 10]. Available from: http://hdl.handle.net/11299/174797.

Council of Science Editors:

Kreitzman J. Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet. [Masters Thesis]. University of Minnesota; 2015. Available from: http://hdl.handle.net/11299/174797


Penn State University

4. Kapusta, Matthew Joseph. simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations.

Degree: MS, Aerospace Engineering, 2015, Penn State University

 The investigation of military jet noise prediction and reduction is an ongoing activity. Supersonic military jets radiate higher noise levels than commercial aircraft and are… (more)

Subjects/Keywords: jet noise reduction; fluidic inserts; supersonic nozzle; supersonic jet flow field; fluid injection

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APA (6th Edition):

Kapusta, M. J. (2015). simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/25662

Chicago Manual of Style (16th Edition):

Kapusta, Matthew Joseph. “simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations.” 2015. Masters Thesis, Penn State University. Accessed August 10, 2020. https://etda.libraries.psu.edu/catalog/25662.

MLA Handbook (7th Edition):

Kapusta, Matthew Joseph. “simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations.” 2015. Web. 10 Aug 2020.

Vancouver:

Kapusta MJ. simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations. [Internet] [Masters thesis]. Penn State University; 2015. [cited 2020 Aug 10]. Available from: https://etda.libraries.psu.edu/catalog/25662.

Council of Science Editors:

Kapusta MJ. simulations of the flow generated by fluidic inserts for supersonic jet noise reduction based on steady RANS simulations. [Masters Thesis]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/25662


University of Cincinnati

5. Mora Sánchez, Pablo A. Investigation of the Noise Radiation from Heated Supersonic Jets.

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

 This work focuses in the investigation of crackle and Mach wave radiation in heated supersonic jets. The skewness and kurtosis of the acoustic pressure signal… (more)

Subjects/Keywords: Aerospace Materials; Supersonic Jet Noise; Crackle; Mach Wave Radiation; Supersonic Heated Jets

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APA (6th Edition):

Mora Sánchez, P. A. (2016). Investigation of the Noise Radiation from Heated Supersonic Jets. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479818582442041

Chicago Manual of Style (16th Edition):

Mora Sánchez, Pablo A. “Investigation of the Noise Radiation from Heated Supersonic Jets.” 2016. Doctoral Dissertation, University of Cincinnati. Accessed August 10, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479818582442041.

MLA Handbook (7th Edition):

Mora Sánchez, Pablo A. “Investigation of the Noise Radiation from Heated Supersonic Jets.” 2016. Web. 10 Aug 2020.

Vancouver:

Mora Sánchez PA. Investigation of the Noise Radiation from Heated Supersonic Jets. [Internet] [Doctoral dissertation]. University of Cincinnati; 2016. [cited 2020 Aug 10]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479818582442041.

Council of Science Editors:

Mora Sánchez PA. Investigation of the Noise Radiation from Heated Supersonic Jets. [Doctoral Dissertation]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479818582442041


University of Cincinnati

6. Heeb, Nicholas S. Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2015, University of Cincinnati

 An experimental investigation into the effect of azimuthal variance of chevrons and fluidically enhanced chevrons applied to supersonic jets is presented. Flow field measurements of… (more)

Subjects/Keywords: Aerospace Materials; Supersonic Jet; Aeroacoustics; Jet Noise; Chevrons; Fluidic Injection; Compressible Flow

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APA (6th Edition):

Heeb, N. S. (2015). Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1445342666

Chicago Manual of Style (16th Edition):

Heeb, Nicholas S. “Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets.” 2015. Doctoral Dissertation, University of Cincinnati. Accessed August 10, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1445342666.

MLA Handbook (7th Edition):

Heeb, Nicholas S. “Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets.” 2015. Web. 10 Aug 2020.

Vancouver:

Heeb NS. Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets. [Internet] [Doctoral dissertation]. University of Cincinnati; 2015. [cited 2020 Aug 10]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1445342666.

Council of Science Editors:

Heeb NS. Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets. [Doctoral Dissertation]. University of Cincinnati; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1445342666


Virginia Tech

7. Akhtar, Kareem. A Numerical Study of Supersonic Rectangular Jet Impingement and Applications to Cold Spray Technology.

Degree: PhD, Engineering Science and Mechanics, 2015, Virginia Tech

 Particle-laden supersonic jets impinging on a flat surface are of interest to cold gas-dynamic spray technology. Solid particles are propelled to a high velocity through… (more)

Subjects/Keywords: Cold Spray Simulation; Supersonic jet Impingement; Particle tracking; Deposition Efficiency

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APA (6th Edition):

Akhtar, K. (2015). A Numerical Study of Supersonic Rectangular Jet Impingement and Applications to Cold Spray Technology. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71711

Chicago Manual of Style (16th Edition):

Akhtar, Kareem. “A Numerical Study of Supersonic Rectangular Jet Impingement and Applications to Cold Spray Technology.” 2015. Doctoral Dissertation, Virginia Tech. Accessed August 10, 2020. http://hdl.handle.net/10919/71711.

MLA Handbook (7th Edition):

Akhtar, Kareem. “A Numerical Study of Supersonic Rectangular Jet Impingement and Applications to Cold Spray Technology.” 2015. Web. 10 Aug 2020.

Vancouver:

Akhtar K. A Numerical Study of Supersonic Rectangular Jet Impingement and Applications to Cold Spray Technology. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2020 Aug 10]. Available from: http://hdl.handle.net/10919/71711.

Council of Science Editors:

Akhtar K. A Numerical Study of Supersonic Rectangular Jet Impingement and Applications to Cold Spray Technology. [Doctoral Dissertation]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/71711


University of Manchester

8. Llopis-Pascual, Alberto. Supersonic Coanda Jets For Flight Control Effectors.

Degree: 2017, University of Manchester

 Traditional control surfaces used on aircraft for high lift and manoeuvre control are complex systems requiring robust mechanical design to achieve the desired movement. Circulation… (more)

Subjects/Keywords: Fluidic Controls; Circulation Control; Coanda Jet; Supersonic Coanda; High speed subsonic

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APA (6th Edition):

Llopis-Pascual, A. (2017). Supersonic Coanda Jets For Flight Control Effectors. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:310241

Chicago Manual of Style (16th Edition):

Llopis-Pascual, Alberto. “Supersonic Coanda Jets For Flight Control Effectors.” 2017. Doctoral Dissertation, University of Manchester. Accessed August 10, 2020. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:310241.

MLA Handbook (7th Edition):

Llopis-Pascual, Alberto. “Supersonic Coanda Jets For Flight Control Effectors.” 2017. Web. 10 Aug 2020.

Vancouver:

Llopis-Pascual A. Supersonic Coanda Jets For Flight Control Effectors. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2020 Aug 10]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:310241.

Council of Science Editors:

Llopis-Pascual A. Supersonic Coanda Jets For Flight Control Effectors. [Doctoral Dissertation]. University of Manchester; 2017. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:310241


University of New Mexico

9. Merritt, Elizabeth Catherine. Measurements of railgun generated supersonic plasma jet propagation and two jet oblique merging.

Degree: Physics & Astronomy, 2013, University of New Mexico

 Imploding spherical plasma liners have been proposed as a possible method for creating high-energy-density (HED) laboratory plasmas and as a standoff driver for magneto-inertial fusion… (more)

Subjects/Keywords: plasma jet merging; plasma diagnostics; supersonic jets; shocks

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APA (6th Edition):

Merritt, E. C. (2013). Measurements of railgun generated supersonic plasma jet propagation and two jet oblique merging. (Doctoral Dissertation). University of New Mexico. Retrieved from http://hdl.handle.net/1928/23349

Chicago Manual of Style (16th Edition):

Merritt, Elizabeth Catherine. “Measurements of railgun generated supersonic plasma jet propagation and two jet oblique merging.” 2013. Doctoral Dissertation, University of New Mexico. Accessed August 10, 2020. http://hdl.handle.net/1928/23349.

MLA Handbook (7th Edition):

Merritt, Elizabeth Catherine. “Measurements of railgun generated supersonic plasma jet propagation and two jet oblique merging.” 2013. Web. 10 Aug 2020.

Vancouver:

Merritt EC. Measurements of railgun generated supersonic plasma jet propagation and two jet oblique merging. [Internet] [Doctoral dissertation]. University of New Mexico; 2013. [cited 2020 Aug 10]. Available from: http://hdl.handle.net/1928/23349.

Council of Science Editors:

Merritt EC. Measurements of railgun generated supersonic plasma jet propagation and two jet oblique merging. [Doctoral Dissertation]. University of New Mexico; 2013. Available from: http://hdl.handle.net/1928/23349


Penn State University

10. Day, Benjamin J. TURBULENCE MEASUREMENTS IN SUPERSONIC JETS WITH OPTICAL DEFLECTOMETRY.

Degree: MS, Aerospace Engineering, 2010, Penn State University

 Experiments have been carried out in the Pennsylvania State University High Speed Jet Noise Facility with the purpose of making turbulence measurements in high speed… (more)

Subjects/Keywords: Jet Noise; Turbulence; supersonic; optical deflectometry; BBSAN; broadband shock associated noise; measurements; turbulence measurements

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APA (6th Edition):

Day, B. J. (2010). TURBULENCE MEASUREMENTS IN SUPERSONIC JETS WITH OPTICAL DEFLECTOMETRY. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/10946

Chicago Manual of Style (16th Edition):

Day, Benjamin J. “TURBULENCE MEASUREMENTS IN SUPERSONIC JETS WITH OPTICAL DEFLECTOMETRY.” 2010. Masters Thesis, Penn State University. Accessed August 10, 2020. https://etda.libraries.psu.edu/catalog/10946.

MLA Handbook (7th Edition):

Day, Benjamin J. “TURBULENCE MEASUREMENTS IN SUPERSONIC JETS WITH OPTICAL DEFLECTOMETRY.” 2010. Web. 10 Aug 2020.

Vancouver:

Day BJ. TURBULENCE MEASUREMENTS IN SUPERSONIC JETS WITH OPTICAL DEFLECTOMETRY. [Internet] [Masters thesis]. Penn State University; 2010. [cited 2020 Aug 10]. Available from: https://etda.libraries.psu.edu/catalog/10946.

Council of Science Editors:

Day BJ. TURBULENCE MEASUREMENTS IN SUPERSONIC JETS WITH OPTICAL DEFLECTOMETRY. [Masters Thesis]. Penn State University; 2010. Available from: https://etda.libraries.psu.edu/catalog/10946

11. Karns, Alex Mitchell. Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements.

Degree: MS, Aerospace Engineering, 2014, Penn State University

 The study of military style exhaust nozzles to further understand their acoustic characteristics has been the recent focus of the Pennsylvania State University high-speed jet(more)

Subjects/Keywords: LDV; Laser; Velocimetry; Supersonic Jet

…The system was used to make supersonic jet exhaust measurements in a free-jet facility in an… …specific experiment (namely to probe the flow field of a supersonic jet typically less than… …Mach number and (b) normalized velocity vs. x/D location for varying jet Mach… …D location for varying jet Mach number. The squares indicate 6σ data and the triangles… …Laser Doppler Velocimetry LDA = Laser Doppler Anemometry xii Mj = Jet Mach number m… 

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APA (6th Edition):

Karns, A. M. (2014). Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/22749

Chicago Manual of Style (16th Edition):

Karns, Alex Mitchell. “Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements.” 2014. Masters Thesis, Penn State University. Accessed August 10, 2020. https://etda.libraries.psu.edu/catalog/22749.

MLA Handbook (7th Edition):

Karns, Alex Mitchell. “Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements.” 2014. Web. 10 Aug 2020.

Vancouver:

Karns AM. Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2020 Aug 10]. Available from: https://etda.libraries.psu.edu/catalog/22749.

Council of Science Editors:

Karns AM. Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements. [Masters Thesis]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/22749


University of Cincinnati

12. Cuppoletti, Daniel R. Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

Supersonic jets provide unique challenges in the aeroacoustic field due to very high jet velocities, shock associated noise components, flow dependence on jet expansion, and… (more)

Subjects/Keywords: Aerospace Materials; Jet Noise; Aeroacoustics; Fluid Dynamics; Particle Image Velocimetry; Acoustics; Supersonic

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APA (6th Edition):

Cuppoletti, D. R. (2013). Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384333927

Chicago Manual of Style (16th Edition):

Cuppoletti, Daniel R. “Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques.” 2013. Doctoral Dissertation, University of Cincinnati. Accessed August 10, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384333927.

MLA Handbook (7th Edition):

Cuppoletti, Daniel R. “Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques.” 2013. Web. 10 Aug 2020.

Vancouver:

Cuppoletti DR. Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques. [Internet] [Doctoral dissertation]. University of Cincinnati; 2013. [cited 2020 Aug 10]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384333927.

Council of Science Editors:

Cuppoletti DR. Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques. [Doctoral Dissertation]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384333927


University of Manchester

13. Robertson Welsh, Bradley. On the Influence of Nozzle Geometries on Supersonic Curved Wall Jets.

Degree: 2017, University of Manchester

 Circulation control involves tangentially blowing air around a rounded trailing edge in order to augment the lift of a wing. The advantages of this technique… (more)

Subjects/Keywords: schlieren; shadowgraph; supersonic; curved; wall; jet; circulation control; fluidic thrust vectoring; FTV; CC; irrotational

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APA (6th Edition):

Robertson Welsh, B. (2017). On the Influence of Nozzle Geometries on Supersonic Curved Wall Jets. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:309358

Chicago Manual of Style (16th Edition):

Robertson Welsh, Bradley. “On the Influence of Nozzle Geometries on Supersonic Curved Wall Jets.” 2017. Doctoral Dissertation, University of Manchester. Accessed August 10, 2020. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:309358.

MLA Handbook (7th Edition):

Robertson Welsh, Bradley. “On the Influence of Nozzle Geometries on Supersonic Curved Wall Jets.” 2017. Web. 10 Aug 2020.

Vancouver:

Robertson Welsh B. On the Influence of Nozzle Geometries on Supersonic Curved Wall Jets. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2020 Aug 10]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:309358.

Council of Science Editors:

Robertson Welsh B. On the Influence of Nozzle Geometries on Supersonic Curved Wall Jets. [Doctoral Dissertation]. University of Manchester; 2017. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:309358


Virginia Tech

14. Ecker, Tobias. Turbulence Statistics and Eddy Convection in Heated Supersonic Jets.

Degree: PhD, Aerospace and Ocean Engineering, 2015, Virginia Tech

Supersonic hot jet noise causes significant hearing impairment to the military workforce and results in substantial cost for medical care and treatment. Detailed insight into… (more)

Subjects/Keywords: Doppler global velocimetry; supersonic jets; jet noise; compressible shear layers; eddy convective velocity; radiation efficiency

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APA (6th Edition):

Ecker, T. (2015). Turbulence Statistics and Eddy Convection in Heated Supersonic Jets. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/51687

Chicago Manual of Style (16th Edition):

Ecker, Tobias. “Turbulence Statistics and Eddy Convection in Heated Supersonic Jets.” 2015. Doctoral Dissertation, Virginia Tech. Accessed August 10, 2020. http://hdl.handle.net/10919/51687.

MLA Handbook (7th Edition):

Ecker, Tobias. “Turbulence Statistics and Eddy Convection in Heated Supersonic Jets.” 2015. Web. 10 Aug 2020.

Vancouver:

Ecker T. Turbulence Statistics and Eddy Convection in Heated Supersonic Jets. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2020 Aug 10]. Available from: http://hdl.handle.net/10919/51687.

Council of Science Editors:

Ecker T. Turbulence Statistics and Eddy Convection in Heated Supersonic Jets. [Doctoral Dissertation]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/51687


University of Manchester

15. Robertson Welsh, Bradley. On the influence of nozzle geometries on supersonic curved wall jets.

Degree: PhD, 2017, University of Manchester

 Circulation control involves tangentially blowing air around a rounded trailing edge in order to augment the lift of a wing. The advantages of this technique… (more)

Subjects/Keywords: 629.134; CC; FTV; fluidic thrust vectoring; irrotational; jet; circulation control; curved; supersonic; shadowgraph; schlieren; wall

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APA (6th Edition):

Robertson Welsh, B. (2017). On the influence of nozzle geometries on supersonic curved wall jets. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/on-the-influence-of-nozzle-geometries-on-supersonic-curved-wall-jets(bc8817e4-c812-44bc-8dfb-f5d0fdf62a72).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728007

Chicago Manual of Style (16th Edition):

Robertson Welsh, Bradley. “On the influence of nozzle geometries on supersonic curved wall jets.” 2017. Doctoral Dissertation, University of Manchester. Accessed August 10, 2020. https://www.research.manchester.ac.uk/portal/en/theses/on-the-influence-of-nozzle-geometries-on-supersonic-curved-wall-jets(bc8817e4-c812-44bc-8dfb-f5d0fdf62a72).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728007.

MLA Handbook (7th Edition):

Robertson Welsh, Bradley. “On the influence of nozzle geometries on supersonic curved wall jets.” 2017. Web. 10 Aug 2020.

Vancouver:

Robertson Welsh B. On the influence of nozzle geometries on supersonic curved wall jets. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2020 Aug 10]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/on-the-influence-of-nozzle-geometries-on-supersonic-curved-wall-jets(bc8817e4-c812-44bc-8dfb-f5d0fdf62a72).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728007.

Council of Science Editors:

Robertson Welsh B. On the influence of nozzle geometries on supersonic curved wall jets. [Doctoral Dissertation]. University of Manchester; 2017. Available from: https://www.research.manchester.ac.uk/portal/en/theses/on-the-influence-of-nozzle-geometries-on-supersonic-curved-wall-jets(bc8817e4-c812-44bc-8dfb-f5d0fdf62a72).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728007

16. Mayo Jr, David Earl. The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities.

Degree: PhD, Mechanical Engineering, 2019, Virginia Tech

 Increasingly large and powerful engines are required as the mission requirements for tactical aircraft become more advanced. These demands come at the cost of an… (more)

Subjects/Keywords: fluid dynamics; supersonic jets; particle image velocimetry; compressible shear layers; jet noise; turbulence

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

APA (6th Edition):

Mayo Jr, D. E. (2019). The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/93532

Chicago Manual of Style (16th Edition):

Mayo Jr, David Earl. “The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities.” 2019. Doctoral Dissertation, Virginia Tech. Accessed August 10, 2020. http://hdl.handle.net/10919/93532.

MLA Handbook (7th Edition):

Mayo Jr, David Earl. “The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities.” 2019. Web. 10 Aug 2020.

Vancouver:

Mayo Jr DE. The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2020 Aug 10]. Available from: http://hdl.handle.net/10919/93532.

Council of Science Editors:

Mayo Jr DE. The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/93532


University of Arizona

17. Hall, Robert Baldwin, 1937-. ADDITIVE DRAG OF TWO-DIMENSIONAL INLETS .

Degree: 1977, University of Arizona

Subjects/Keywords: Aerodynamics, Supersonic.; Jet engines  – Air intakes.

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APA (6th Edition):

Hall, Robert Baldwin, 1. (1977). ADDITIVE DRAG OF TWO-DIMENSIONAL INLETS . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/289652

Chicago Manual of Style (16th Edition):

Hall, Robert Baldwin, 1937-. “ADDITIVE DRAG OF TWO-DIMENSIONAL INLETS .” 1977. Doctoral Dissertation, University of Arizona. Accessed August 10, 2020. http://hdl.handle.net/10150/289652.

MLA Handbook (7th Edition):

Hall, Robert Baldwin, 1937-. “ADDITIVE DRAG OF TWO-DIMENSIONAL INLETS .” 1977. Web. 10 Aug 2020.

Vancouver:

Hall, Robert Baldwin 1. ADDITIVE DRAG OF TWO-DIMENSIONAL INLETS . [Internet] [Doctoral dissertation]. University of Arizona; 1977. [cited 2020 Aug 10]. Available from: http://hdl.handle.net/10150/289652.

Council of Science Editors:

Hall, Robert Baldwin 1. ADDITIVE DRAG OF TWO-DIMENSIONAL INLETS . [Doctoral Dissertation]. University of Arizona; 1977. Available from: http://hdl.handle.net/10150/289652


The Ohio State University

18. Goparaju, Kalyan. Flow and Acoustic Characteristics of Complex Supersonic Jets.

Degree: PhD, Aero/Astro Engineering, 2017, The Ohio State University

Jet noise has been a major source of concern for commercial and military aviation sectors alike. The need to assuage the adverse impact of jet(more)

Subjects/Keywords: Acoustics; Aerospace Engineering; Fluid Dynamics; jet noise; supersonic jets; LES; twin-jets; underexpanded jets; momentum potential theory; flow decomposition

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

APA (6th Edition):

Goparaju, K. (2017). Flow and Acoustic Characteristics of Complex Supersonic Jets. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1510933315034965

Chicago Manual of Style (16th Edition):

Goparaju, Kalyan. “Flow and Acoustic Characteristics of Complex Supersonic Jets.” 2017. Doctoral Dissertation, The Ohio State University. Accessed August 10, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1510933315034965.

MLA Handbook (7th Edition):

Goparaju, Kalyan. “Flow and Acoustic Characteristics of Complex Supersonic Jets.” 2017. Web. 10 Aug 2020.

Vancouver:

Goparaju K. Flow and Acoustic Characteristics of Complex Supersonic Jets. [Internet] [Doctoral dissertation]. The Ohio State University; 2017. [cited 2020 Aug 10]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1510933315034965.

Council of Science Editors:

Goparaju K. Flow and Acoustic Characteristics of Complex Supersonic Jets. [Doctoral Dissertation]. The Ohio State University; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1510933315034965


University of Alabama

19. Smith, Nicholas Edward. Development of a low density jet flow apparatus.

Degree: 2010, University of Alabama

 An apparatus was designed and constructed to study supersonic fluid flow in a low temperature and low pressure environment similar to the same conditions associated… (more)

Subjects/Keywords: Electronic Thesis or Dissertation;  – thesis; Mechanical Engineering; annular jet; low-density; near-space; propulsion; shadowgraph; supersonic

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

APA (6th Edition):

Smith, N. E. (2010). Development of a low density jet flow apparatus. (Thesis). University of Alabama. Retrieved from http://purl.lib.ua.edu/21243

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, Nicholas Edward. “Development of a low density jet flow apparatus.” 2010. Thesis, University of Alabama. Accessed August 10, 2020. http://purl.lib.ua.edu/21243.

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

MLA Handbook (7th Edition):

Smith, Nicholas Edward. “Development of a low density jet flow apparatus.” 2010. Web. 10 Aug 2020.

Vancouver:

Smith NE. Development of a low density jet flow apparatus. [Internet] [Thesis]. University of Alabama; 2010. [cited 2020 Aug 10]. Available from: http://purl.lib.ua.edu/21243.

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

Council of Science Editors:

Smith NE. Development of a low density jet flow apparatus. [Thesis]. University of Alabama; 2010. Available from: http://purl.lib.ua.edu/21243

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


University of New South Wales

20. Freebairn, Gregory. The Physics of Transitional Jet Interactions.

Degree: Engineering & Information Technology, 2010, University of New South Wales

 An experimental and computational study has been undertaken to investigate the interaction between a transverse circular sonic jet and a Mach 6.7 cross flow on… (more)

Subjects/Keywords: Supersonic aerodynamics; Mach 6.7 cross flow; Transverse circular sonic jet; Boundary layer turbulance; Flat plate; Computational Fluid Dynamic (CFD); Heat transfer

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APA (6th Edition):

Freebairn, G. (2010). The Physics of Transitional Jet Interactions. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/45700 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8982/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Freebairn, Gregory. “The Physics of Transitional Jet Interactions.” 2010. Doctoral Dissertation, University of New South Wales. Accessed August 10, 2020. http://handle.unsw.edu.au/1959.4/45700 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8982/SOURCE01?view=true.

MLA Handbook (7th Edition):

Freebairn, Gregory. “The Physics of Transitional Jet Interactions.” 2010. Web. 10 Aug 2020.

Vancouver:

Freebairn G. The Physics of Transitional Jet Interactions. [Internet] [Doctoral dissertation]. University of New South Wales; 2010. [cited 2020 Aug 10]. Available from: http://handle.unsw.edu.au/1959.4/45700 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8982/SOURCE01?view=true.

Council of Science Editors:

Freebairn G. The Physics of Transitional Jet Interactions. [Doctoral Dissertation]. University of New South Wales; 2010. Available from: http://handle.unsw.edu.au/1959.4/45700 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8982/SOURCE01?view=true

21. Mubarak A. K.; Dr. Tide P. S. INVESTIGATION ON SHOCK CELL PARAMETERS IN JETS EMANATING FROM CONICAL, BELL AND DOUBLE PARABOLIC NOZZLES.

Degree: 2018, Cochin University of Science and Technology

Subjects/Keywords: Jet Dynamics of Supersonic Flows; Nozzle Design

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

APA (6th Edition):

S, M. A. K. D. T. P. (2018). INVESTIGATION ON SHOCK CELL PARAMETERS IN JETS EMANATING FROM CONICAL, BELL AND DOUBLE PARABOLIC NOZZLES. (Thesis). Cochin University of Science and Technology. Retrieved from http://dyuthi.cusat.ac.in/purl/5464

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):

S, Mubarak A. K.; Dr. Tide P.. “INVESTIGATION ON SHOCK CELL PARAMETERS IN JETS EMANATING FROM CONICAL, BELL AND DOUBLE PARABOLIC NOZZLES.” 2018. Thesis, Cochin University of Science and Technology. Accessed August 10, 2020. http://dyuthi.cusat.ac.in/purl/5464.

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

MLA Handbook (7th Edition):

S, Mubarak A. K.; Dr. Tide P.. “INVESTIGATION ON SHOCK CELL PARAMETERS IN JETS EMANATING FROM CONICAL, BELL AND DOUBLE PARABOLIC NOZZLES.” 2018. Web. 10 Aug 2020.

Vancouver:

S MAKDTP. INVESTIGATION ON SHOCK CELL PARAMETERS IN JETS EMANATING FROM CONICAL, BELL AND DOUBLE PARABOLIC NOZZLES. [Internet] [Thesis]. Cochin University of Science and Technology; 2018. [cited 2020 Aug 10]. Available from: http://dyuthi.cusat.ac.in/purl/5464.

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

Council of Science Editors:

S MAKDTP. INVESTIGATION ON SHOCK CELL PARAMETERS IN JETS EMANATING FROM CONICAL, BELL AND DOUBLE PARABOLIC NOZZLES. [Thesis]. Cochin University of Science and Technology; 2018. Available from: http://dyuthi.cusat.ac.in/purl/5464

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

22. Magstadt, Andrew S. Investigating the Structures of Turbulence in a Multi-stream, Rectangular, Supersonic Jet.

Degree: PhD, Mechanical and Aerospace Engineering, 2017, Syracuse University

Supersonic flight has become a standard for military aircraft, and is being seriously reconsidered for commercial applications. Engine technologies, enabling increased mission capabilities and… (more)

Subjects/Keywords: Jet; Multi-stream; Rectangular; Supersonic; Turbulence; Engineering

…placed in the supersonic core of the jet. This experiment was performed to calibrate the… …during takeoff in low-bypass and supersonic engines is a result of the external jet flow, which… …propulsion systems than the axisymmetric convergent jet originally used for supersonic flight. As… …understand the structures of turbulence of a complex supersonic jet flow. In the context of… …3.1.1 Facility . . . . . . . 3.1.2 Jet Rig . . . . . . . 3.1.3 Jet Controller . . . 3.1.4 Jet… 

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

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APA (6th Edition):

Magstadt, A. S. (2017). Investigating the Structures of Turbulence in a Multi-stream, Rectangular, Supersonic Jet. (Doctoral Dissertation). Syracuse University. Retrieved from https://surface.syr.edu/etd/745

Chicago Manual of Style (16th Edition):

Magstadt, Andrew S. “Investigating the Structures of Turbulence in a Multi-stream, Rectangular, Supersonic Jet.” 2017. Doctoral Dissertation, Syracuse University. Accessed August 10, 2020. https://surface.syr.edu/etd/745.

MLA Handbook (7th Edition):

Magstadt, Andrew S. “Investigating the Structures of Turbulence in a Multi-stream, Rectangular, Supersonic Jet.” 2017. Web. 10 Aug 2020.

Vancouver:

Magstadt AS. Investigating the Structures of Turbulence in a Multi-stream, Rectangular, Supersonic Jet. [Internet] [Doctoral dissertation]. Syracuse University; 2017. [cited 2020 Aug 10]. Available from: https://surface.syr.edu/etd/745.

Council of Science Editors:

Magstadt AS. Investigating the Structures of Turbulence in a Multi-stream, Rectangular, Supersonic Jet. [Doctoral Dissertation]. Syracuse University; 2017. Available from: https://surface.syr.edu/etd/745

23. Berry, Matthew. Investigating the Interaction of a Supersonic Single Expansion Ramp Nozzle and Sonic Wall Jet.

Degree: PhD, Mechanical and Aerospace Engineering, 2017, Syracuse University

  For nearly 80 years, the jet engine has set the pace for aviation technology around the world. Complexity of design has compounded upon each… (more)

Subjects/Keywords: Aircraft; Jet; SERN; Supersonic; Turbulence; Engineering

…representing the jet as two canonical flows; a rectangular supersonic nozzle and a sonic wall jet… …3 Experimental Approach 3.1 Facility . . . . . . . . . . . 3.2 Jet Rig… …3.3 Jet Nozzle . . . . . . . . . 3.3.1 Scaling Parameters 3.4 Schlieren Imaging… …5 2.1 Schematic of jet shear layer described in Moore (1977) [2]… …Magstadt (2017) [1] schematic of developing jet… 

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APA (6th Edition):

Berry, M. (2017). Investigating the Interaction of a Supersonic Single Expansion Ramp Nozzle and Sonic Wall Jet. (Doctoral Dissertation). Syracuse University. Retrieved from https://surface.syr.edu/etd/819

Chicago Manual of Style (16th Edition):

Berry, Matthew. “Investigating the Interaction of a Supersonic Single Expansion Ramp Nozzle and Sonic Wall Jet.” 2017. Doctoral Dissertation, Syracuse University. Accessed August 10, 2020. https://surface.syr.edu/etd/819.

MLA Handbook (7th Edition):

Berry, Matthew. “Investigating the Interaction of a Supersonic Single Expansion Ramp Nozzle and Sonic Wall Jet.” 2017. Web. 10 Aug 2020.

Vancouver:

Berry M. Investigating the Interaction of a Supersonic Single Expansion Ramp Nozzle and Sonic Wall Jet. [Internet] [Doctoral dissertation]. Syracuse University; 2017. [cited 2020 Aug 10]. Available from: https://surface.syr.edu/etd/819.

Council of Science Editors:

Berry M. Investigating the Interaction of a Supersonic Single Expansion Ramp Nozzle and Sonic Wall Jet. [Doctoral Dissertation]. Syracuse University; 2017. Available from: https://surface.syr.edu/etd/819

24. Poubeau, Adèle. Simulation des émissions d'un moteur à propergol solide : vers une modélisation multi-échelle de l'impact atmosphérique des lanceurs : Large eddy simulations of a solidrocket motor jet : towards a multi-scale modeling of the atmospheric impact of rocket emissions.

Degree: Docteur es, Mécanique des fluides, 2015, Université Toulouse III – Paul Sabatier

Les lanceurs ont un impact sur la composition de l'atmosphere, et en particulier sur l'ozone stratospherique. Parmi tous les types de propulsion, les moteurs à… (more)

Subjects/Keywords: Computational Fluid Dynamics (CFD); Solid Rocket Motor; Supersonic jet; Combustion; Large Eddy Simulation (LES); Solid Rocket Booster; Diffusion flame

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APA (6th Edition):

Poubeau, A. (2015). Simulation des émissions d'un moteur à propergol solide : vers une modélisation multi-échelle de l'impact atmosphérique des lanceurs : Large eddy simulations of a solidrocket motor jet : towards a multi-scale modeling of the atmospheric impact of rocket emissions. (Doctoral Dissertation). Université Toulouse III – Paul Sabatier. Retrieved from http://www.theses.fr/2015TOU30039

Chicago Manual of Style (16th Edition):

Poubeau, Adèle. “Simulation des émissions d'un moteur à propergol solide : vers une modélisation multi-échelle de l'impact atmosphérique des lanceurs : Large eddy simulations of a solidrocket motor jet : towards a multi-scale modeling of the atmospheric impact of rocket emissions.” 2015. Doctoral Dissertation, Université Toulouse III – Paul Sabatier. Accessed August 10, 2020. http://www.theses.fr/2015TOU30039.

MLA Handbook (7th Edition):

Poubeau, Adèle. “Simulation des émissions d'un moteur à propergol solide : vers une modélisation multi-échelle de l'impact atmosphérique des lanceurs : Large eddy simulations of a solidrocket motor jet : towards a multi-scale modeling of the atmospheric impact of rocket emissions.” 2015. Web. 10 Aug 2020.

Vancouver:

Poubeau A. Simulation des émissions d'un moteur à propergol solide : vers une modélisation multi-échelle de l'impact atmosphérique des lanceurs : Large eddy simulations of a solidrocket motor jet : towards a multi-scale modeling of the atmospheric impact of rocket emissions. [Internet] [Doctoral dissertation]. Université Toulouse III – Paul Sabatier; 2015. [cited 2020 Aug 10]. Available from: http://www.theses.fr/2015TOU30039.

Council of Science Editors:

Poubeau A. Simulation des émissions d'un moteur à propergol solide : vers une modélisation multi-échelle de l'impact atmosphérique des lanceurs : Large eddy simulations of a solidrocket motor jet : towards a multi-scale modeling of the atmospheric impact of rocket emissions. [Doctoral Dissertation]. Université Toulouse III – Paul Sabatier; 2015. Available from: http://www.theses.fr/2015TOU30039


University of Western Ontario

25. Li, Feng. Particle Attrition with Supersonic Nozzles in a High Temperature Fluidized Bed.

Degree: 2011, University of Western Ontario

 Fluidized beds are widely used for a variety of processes such as food, pharmaceutical, petrochemical and energy production. As a typical application of fluidized beds,… (more)

Subjects/Keywords: Supersonic nozzle; fluidized bed; fluid coking; high temperature; particle attrition; twin jet; CFD; Chemical Engineering; Petroleum Engineering

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

APA (6th Edition):

Li, F. (2011). Particle Attrition with Supersonic Nozzles in a High Temperature Fluidized Bed. (Thesis). University of Western Ontario. Retrieved from https://ir.lib.uwo.ca/etd/147

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):

Li, Feng. “Particle Attrition with Supersonic Nozzles in a High Temperature Fluidized Bed.” 2011. Thesis, University of Western Ontario. Accessed August 10, 2020. https://ir.lib.uwo.ca/etd/147.

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

MLA Handbook (7th Edition):

Li, Feng. “Particle Attrition with Supersonic Nozzles in a High Temperature Fluidized Bed.” 2011. Web. 10 Aug 2020.

Vancouver:

Li F. Particle Attrition with Supersonic Nozzles in a High Temperature Fluidized Bed. [Internet] [Thesis]. University of Western Ontario; 2011. [cited 2020 Aug 10]. Available from: https://ir.lib.uwo.ca/etd/147.

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

Council of Science Editors:

Li F. Particle Attrition with Supersonic Nozzles in a High Temperature Fluidized Bed. [Thesis]. University of Western Ontario; 2011. Available from: https://ir.lib.uwo.ca/etd/147

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


University of Western Ontario

26. Hamidi, Majid. Development And Study Of Measurement Methods For Jets And Bogging In A Fluidized Bed.

Degree: 2015, University of Western Ontario

 In the Fluid Coking process, if the local concentration of liquid is very high, particles may stick together which can eventually result in process upset… (more)

Subjects/Keywords: Fluidized bed; bogging detection; capacitance measurements; agglomerate breakage; bubble properties; supersonic jet fluctuation; Process Control and Systems

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

APA (6th Edition):

Hamidi, M. (2015). Development And Study Of Measurement Methods For Jets And Bogging In A Fluidized Bed. (Thesis). University of Western Ontario. Retrieved from https://ir.lib.uwo.ca/etd/2679

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):

Hamidi, Majid. “Development And Study Of Measurement Methods For Jets And Bogging In A Fluidized Bed.” 2015. Thesis, University of Western Ontario. Accessed August 10, 2020. https://ir.lib.uwo.ca/etd/2679.

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

MLA Handbook (7th Edition):

Hamidi, Majid. “Development And Study Of Measurement Methods For Jets And Bogging In A Fluidized Bed.” 2015. Web. 10 Aug 2020.

Vancouver:

Hamidi M. Development And Study Of Measurement Methods For Jets And Bogging In A Fluidized Bed. [Internet] [Thesis]. University of Western Ontario; 2015. [cited 2020 Aug 10]. Available from: https://ir.lib.uwo.ca/etd/2679.

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

Council of Science Editors:

Hamidi M. Development And Study Of Measurement Methods For Jets And Bogging In A Fluidized Bed. [Thesis]. University of Western Ontario; 2015. Available from: https://ir.lib.uwo.ca/etd/2679

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

27. Esteves López, Natalia. Etude du transfert de protons dans les systèmes moléculaires : Proton transfer along molecular wires.

Degree: Docteur es, Chimie, physique, 2017, Aix Marseille Université

Une des meilleures sources d’énergie verte serait d’être capable de casser une molécule d’eau à partir du rayonnement visible fourni par le soleil, afin de… (more)

Subjects/Keywords: Transfert de protons; Phase gazeuse; Matrices cryogéniques; Spectroscopie; IR et UV-Visible; Jet supersonique; Proton transfer; Gas phase; Cryogenic matrices; Spectroscopy; IR and UV-Visible; Supersonic jet

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APA (6th Edition):

Esteves López, N. (2017). Etude du transfert de protons dans les systèmes moléculaires : Proton transfer along molecular wires. (Doctoral Dissertation). Aix Marseille Université. Retrieved from http://www.theses.fr/2017AIXM0178

Chicago Manual of Style (16th Edition):

Esteves López, Natalia. “Etude du transfert de protons dans les systèmes moléculaires : Proton transfer along molecular wires.” 2017. Doctoral Dissertation, Aix Marseille Université. Accessed August 10, 2020. http://www.theses.fr/2017AIXM0178.

MLA Handbook (7th Edition):

Esteves López, Natalia. “Etude du transfert de protons dans les systèmes moléculaires : Proton transfer along molecular wires.” 2017. Web. 10 Aug 2020.

Vancouver:

Esteves López N. Etude du transfert de protons dans les systèmes moléculaires : Proton transfer along molecular wires. [Internet] [Doctoral dissertation]. Aix Marseille Université 2017. [cited 2020 Aug 10]. Available from: http://www.theses.fr/2017AIXM0178.

Council of Science Editors:

Esteves López N. Etude du transfert de protons dans les systèmes moléculaires : Proton transfer along molecular wires. [Doctoral Dissertation]. Aix Marseille Université 2017. Available from: http://www.theses.fr/2017AIXM0178

28. 李, 權羲; イ, ゴンヒー. 旋回を伴う二重同軸超音速噴流に関する研究 : センカイ オ トモナウ ニジュウ ドウジク チョウオンソク フンリュウ ニカンスル ケンキュウ; STUDY OF SUPERSONIC DUAL, COAXIAL, SWIRLING JET.

Degree: Saga University / 佐賀大学

Supersonic jet with a secondary annular stream has been quite interested with regard to the mixing enhancement of the two streams, the suppression of the jet noise emanated from a turbofan engine and the gas laser cutting or welding in industrial manufac

Subjects/Keywords: Supersonic Swirling Jet; Coaxial Jet; Swirl Nozzle; Shock Wave; Recirculation Region; Pressure Distibution

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APA (6th Edition):

李, 權羲; イ, . (n.d.). 旋回を伴う二重同軸超音速噴流に関する研究 : センカイ オ トモナウ ニジュウ ドウジク チョウオンソク フンリュウ ニカンスル ケンキュウ; STUDY OF SUPERSONIC DUAL, COAXIAL, SWIRLING JET. (Thesis). Saga University / 佐賀大学. Retrieved from http://portal.dl.saga-u.ac.jp/handle/123456789/8335

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

李, 權羲; イ, ゴンヒー. “旋回を伴う二重同軸超音速噴流に関する研究 : センカイ オ トモナウ ニジュウ ドウジク チョウオンソク フンリュウ ニカンスル ケンキュウ; STUDY OF SUPERSONIC DUAL, COAXIAL, SWIRLING JET.” Thesis, Saga University / 佐賀大学. Accessed August 10, 2020. http://portal.dl.saga-u.ac.jp/handle/123456789/8335.

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

李, 權羲; イ, ゴンヒー. “旋回を伴う二重同軸超音速噴流に関する研究 : センカイ オ トモナウ ニジュウ ドウジク チョウオンソク フンリュウ ニカンスル ケンキュウ; STUDY OF SUPERSONIC DUAL, COAXIAL, SWIRLING JET.” Web. 10 Aug 2020.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

李, 權羲; イ . 旋回を伴う二重同軸超音速噴流に関する研究 : センカイ オ トモナウ ニジュウ ドウジク チョウオンソク フンリュウ ニカンスル ケンキュウ; STUDY OF SUPERSONIC DUAL, COAXIAL, SWIRLING JET. [Internet] [Thesis]. Saga University / 佐賀大学; [cited 2020 Aug 10]. Available from: http://portal.dl.saga-u.ac.jp/handle/123456789/8335.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.

Council of Science Editors:

李, 權羲; イ . 旋回を伴う二重同軸超音速噴流に関する研究 : センカイ オ トモナウ ニジュウ ドウジク チョウオンソク フンリュウ ニカンスル ケンキュウ; STUDY OF SUPERSONIC DUAL, COAXIAL, SWIRLING JET. [Thesis]. Saga University / 佐賀大学; Available from: http://portal.dl.saga-u.ac.jp/handle/123456789/8335

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.


Université Paris-Sud – Paris XI

29. Kintz, Harold. Réalisation de couches minces nanocomposites par un procédé original couplant la pyrolyse laser et la pulvérisation magnétron : application aux cellules solaires tout silicium de troisième génération : Elaboration of nanostructured thin films by laser pyrolysis and magnetron sputtering combined process : application to all silicon third generation solar cells.

Degree: Docteur es, Chimie des matériaux, 2013, Université Paris-Sud – Paris XI

Ce travail porte sur la synthèse de couches minces de nanoparticules de silicium (np-Si) encapsulées dans une matrice diélectrique en vue d’une application en tant… (more)

Subjects/Keywords: Silicium; Nanostructures; Cellule solaire; Dopage; Couche mince; Pyrolyse laser; Pulvérisation magnétron; Jet supersonique; Confinement quantique; Silicon; Nanomaterial; Solar cell; Doping; Thin films; Laser pyrolysis; Magnetron sputtering; Supersonic jet; Quantum confinement

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

APA (6th Edition):

Kintz, H. (2013). Réalisation de couches minces nanocomposites par un procédé original couplant la pyrolyse laser et la pulvérisation magnétron : application aux cellules solaires tout silicium de troisième génération : Elaboration of nanostructured thin films by laser pyrolysis and magnetron sputtering combined process : application to all silicon third generation solar cells. (Doctoral Dissertation). Université Paris-Sud – Paris XI. Retrieved from http://www.theses.fr/2013PA112357

Chicago Manual of Style (16th Edition):

Kintz, Harold. “Réalisation de couches minces nanocomposites par un procédé original couplant la pyrolyse laser et la pulvérisation magnétron : application aux cellules solaires tout silicium de troisième génération : Elaboration of nanostructured thin films by laser pyrolysis and magnetron sputtering combined process : application to all silicon third generation solar cells.” 2013. Doctoral Dissertation, Université Paris-Sud – Paris XI. Accessed August 10, 2020. http://www.theses.fr/2013PA112357.

MLA Handbook (7th Edition):

Kintz, Harold. “Réalisation de couches minces nanocomposites par un procédé original couplant la pyrolyse laser et la pulvérisation magnétron : application aux cellules solaires tout silicium de troisième génération : Elaboration of nanostructured thin films by laser pyrolysis and magnetron sputtering combined process : application to all silicon third generation solar cells.” 2013. Web. 10 Aug 2020.

Vancouver:

Kintz H. Réalisation de couches minces nanocomposites par un procédé original couplant la pyrolyse laser et la pulvérisation magnétron : application aux cellules solaires tout silicium de troisième génération : Elaboration of nanostructured thin films by laser pyrolysis and magnetron sputtering combined process : application to all silicon third generation solar cells. [Internet] [Doctoral dissertation]. Université Paris-Sud – Paris XI; 2013. [cited 2020 Aug 10]. Available from: http://www.theses.fr/2013PA112357.

Council of Science Editors:

Kintz H. Réalisation de couches minces nanocomposites par un procédé original couplant la pyrolyse laser et la pulvérisation magnétron : application aux cellules solaires tout silicium de troisième génération : Elaboration of nanostructured thin films by laser pyrolysis and magnetron sputtering combined process : application to all silicon third generation solar cells. [Doctoral Dissertation]. Université Paris-Sud – Paris XI; 2013. Available from: http://www.theses.fr/2013PA112357


Brno University of Technology

30. Kincová, Daniela. Zavedení a provoz supersonického business jetu: Launching and Operating Issues of Supersonic Business Jet.

Degree: 2019, Brno University of Technology

 This thesis is dealing with problematic about launching and operating supersonic business jets. Nowadays, after Concorde retirement, there are no more any supersonic aircrafts in… (more)

Subjects/Keywords: Nadzvuková přeprava; Nadzvukový Business jet; Aerion; Concorde; rázová vlna; sonický třesk; vysokorychlostní létání; konstrukce nadzvukového letounu; hluk; emise; spotřeba paliva; létání ve vysokých výškách; analýza leteckého trhu; poptávka po nadzvukových business jetech; náklady na provoz; dopravní nadzvuková komise; porovnání podzvukového a nadzvukového business jetu.; Supersonic Transport; Supersonic Business jet; Aerion; Concorde; Shock wave; sonic boom; highspeed flying; supersonic aircraft design; aircraft noise; emission; fuel consumption; high altitude flying; business aviation market analysis; market demand for supersonic business jet; life cycle cost; Supersonic Transport Group; comparison between subsonic and supersonic business jet.

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

APA (6th Edition):

Kincová, D. (2019). Zavedení a provoz supersonického business jetu: Launching and Operating Issues of Supersonic Business Jet. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/40126

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):

Kincová, Daniela. “Zavedení a provoz supersonického business jetu: Launching and Operating Issues of Supersonic Business Jet.” 2019. Thesis, Brno University of Technology. Accessed August 10, 2020. http://hdl.handle.net/11012/40126.

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

MLA Handbook (7th Edition):

Kincová, Daniela. “Zavedení a provoz supersonického business jetu: Launching and Operating Issues of Supersonic Business Jet.” 2019. Web. 10 Aug 2020.

Vancouver:

Kincová D. Zavedení a provoz supersonického business jetu: Launching and Operating Issues of Supersonic Business Jet. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2020 Aug 10]. Available from: http://hdl.handle.net/11012/40126.

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

Council of Science Editors:

Kincová D. Zavedení a provoz supersonického business jetu: Launching and Operating Issues of Supersonic Business Jet. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/40126

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

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