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You searched for subject:(Supersonic mixing). Showing records 1 – 30 of 30 total matches.

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University of New Mexico

1. Olmstead, Dell. Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column.

Degree: Mechanical Engineering, 2016, University of New Mexico

 An experimental study was performed to elucidate the fundamental physics of shock-induced mixing for a simple three-dimensional interface. The interface studied consists of a gravity… (more)

Subjects/Keywords: Shock; Richtmyer-Meshkov; Kelvin-Helmholtz; mixing; supersonic

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APA (6th Edition):

Olmstead, D. (2016). Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column. (Doctoral Dissertation). University of New Mexico. Retrieved from http://hdl.handle.net/1928/31737

Chicago Manual of Style (16th Edition):

Olmstead, Dell. “Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column.” 2016. Doctoral Dissertation, University of New Mexico. Accessed March 02, 2021. http://hdl.handle.net/1928/31737.

MLA Handbook (7th Edition):

Olmstead, Dell. “Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column.” 2016. Web. 02 Mar 2021.

Vancouver:

Olmstead D. Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column. [Internet] [Doctoral dissertation]. University of New Mexico; 2016. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/1928/31737.

Council of Science Editors:

Olmstead D. Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column. [Doctoral Dissertation]. University of New Mexico; 2016. Available from: http://hdl.handle.net/1928/31737


Indian Institute of Science

2. Varghese, Albin B M. Mixing Enhancement Studies on Supersonic Elliptic Sharp Tipped Shallow (ESTS) Lobed Nozzles.

Degree: MSc Engg, Faculty of Engineering, 2017, Indian Institute of Science

 Rapid mixing and spreading of supersonic jets are two important characteristics in supersonic ejectors, noise reduction in jets and fuel mixing in supersonic combustion. It… (more)

Subjects/Keywords: Elliptic Sharp Tipped Shallow Lobbed Nozzles; Supersonic Jets; Supersonic Ejectors; Supersonic Nozzles; Aeroacoustics; Supersonic Combustion; Supersonic Flow; Jet Mixing Nozzles; Jets-Fluid Dynamics; Supersonic Jet Noise; Jet Mixing Enhancement; Velocimetry; ESTS Lobed Nozzles; Nozzle Geometry; Schlieren Visualisation; Aerospace Engineering

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APA (6th Edition):

Varghese, A. B. M. (2017). Mixing Enhancement Studies on Supersonic Elliptic Sharp Tipped Shallow (ESTS) Lobed Nozzles. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2782

Chicago Manual of Style (16th Edition):

Varghese, Albin B M. “Mixing Enhancement Studies on Supersonic Elliptic Sharp Tipped Shallow (ESTS) Lobed Nozzles.” 2017. Masters Thesis, Indian Institute of Science. Accessed March 02, 2021. http://etd.iisc.ac.in/handle/2005/2782.

MLA Handbook (7th Edition):

Varghese, Albin B M. “Mixing Enhancement Studies on Supersonic Elliptic Sharp Tipped Shallow (ESTS) Lobed Nozzles.” 2017. Web. 02 Mar 2021.

Vancouver:

Varghese ABM. Mixing Enhancement Studies on Supersonic Elliptic Sharp Tipped Shallow (ESTS) Lobed Nozzles. [Internet] [Masters thesis]. Indian Institute of Science; 2017. [cited 2021 Mar 02]. Available from: http://etd.iisc.ac.in/handle/2005/2782.

Council of Science Editors:

Varghese ABM. Mixing Enhancement Studies on Supersonic Elliptic Sharp Tipped Shallow (ESTS) Lobed Nozzles. [Masters Thesis]. Indian Institute of Science; 2017. Available from: http://etd.iisc.ac.in/handle/2005/2782


Penn State University

3. Merck, Andrew Thomas. The Development of a Fast Method for the Calculation of Noise from Supersonic Jets.

Degree: 2018, Penn State University

 The development of a high-speed jet noise prediction method that is significantly less computationally expensive than previous computationally-based methods and which provides a simple user… (more)

Subjects/Keywords: Jet Noise; Aeroacoustics; Acoustics; Empirical Method; Wavepacket; Supersonic; Turbulence; Mixing Noise

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APA (6th Edition):

Merck, A. T. (2018). The Development of a Fast Method for the Calculation of Noise from Supersonic Jets. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15303atm26

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):

Merck, Andrew Thomas. “The Development of a Fast Method for the Calculation of Noise from Supersonic Jets.” 2018. Thesis, Penn State University. Accessed March 02, 2021. https://submit-etda.libraries.psu.edu/catalog/15303atm26.

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

MLA Handbook (7th Edition):

Merck, Andrew Thomas. “The Development of a Fast Method for the Calculation of Noise from Supersonic Jets.” 2018. Web. 02 Mar 2021.

Vancouver:

Merck AT. The Development of a Fast Method for the Calculation of Noise from Supersonic Jets. [Internet] [Thesis]. Penn State University; 2018. [cited 2021 Mar 02]. Available from: https://submit-etda.libraries.psu.edu/catalog/15303atm26.

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

Council of Science Editors:

Merck AT. The Development of a Fast Method for the Calculation of Noise from Supersonic Jets. [Thesis]. Penn State University; 2018. Available from: https://submit-etda.libraries.psu.edu/catalog/15303atm26

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


University of Minnesota

4. Peterson, David Michael. Simulations of injection, mixing, and combustion in supersonic flow using a hybrid RANS/LES approach.

Degree: PhD, Aerospace Engineering and Mechanics, 2011, University of Minnesota

 There is a great need for accurate and reliable numerical simulation of injection, mixing, and combustion in supersonic combustion ramjet engines. This study seeks to… (more)

Subjects/Keywords: Combustion; Hypersonic; LES; Mixing; Scramjet; Supersonic; Aerospace Engineering and Mechanics

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APA (6th Edition):

Peterson, D. M. (2011). Simulations of injection, mixing, and combustion in supersonic flow using a hybrid RANS/LES approach. (Doctoral Dissertation). University of Minnesota. Retrieved from http://purl.umn.edu/117465

Chicago Manual of Style (16th Edition):

Peterson, David Michael. “Simulations of injection, mixing, and combustion in supersonic flow using a hybrid RANS/LES approach.” 2011. Doctoral Dissertation, University of Minnesota. Accessed March 02, 2021. http://purl.umn.edu/117465.

MLA Handbook (7th Edition):

Peterson, David Michael. “Simulations of injection, mixing, and combustion in supersonic flow using a hybrid RANS/LES approach.” 2011. Web. 02 Mar 2021.

Vancouver:

Peterson DM. Simulations of injection, mixing, and combustion in supersonic flow using a hybrid RANS/LES approach. [Internet] [Doctoral dissertation]. University of Minnesota; 2011. [cited 2021 Mar 02]. Available from: http://purl.umn.edu/117465.

Council of Science Editors:

Peterson DM. Simulations of injection, mixing, and combustion in supersonic flow using a hybrid RANS/LES approach. [Doctoral Dissertation]. University of Minnesota; 2011. Available from: http://purl.umn.edu/117465


Georgia Tech

5. Fries, Dan. Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow.

Degree: PhD, Aerospace Engineering, 2020, Georgia Tech

 Jets in crossflow are a canonical example for three-dimensional turbulent mixing. Here, non-reacting and reacting sonic jets in a supersonic crossflow are studied. The influence… (more)

Subjects/Keywords: Jet in Crossflow; Supersonic Flow; Turbulent mixing; Laser ignition; Staged jets

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APA (6th Edition):

Fries, D. (2020). Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/64095

Chicago Manual of Style (16th Edition):

Fries, Dan. “Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow.” 2020. Doctoral Dissertation, Georgia Tech. Accessed March 02, 2021. http://hdl.handle.net/1853/64095.

MLA Handbook (7th Edition):

Fries, Dan. “Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow.” 2020. Web. 02 Mar 2021.

Vancouver:

Fries D. Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow. [Internet] [Doctoral dissertation]. Georgia Tech; 2020. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/1853/64095.

Council of Science Editors:

Fries D. Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow. [Doctoral Dissertation]. Georgia Tech; 2020. Available from: http://hdl.handle.net/1853/64095


University of Maryland

6. Zang, Andrew. FUEL INJECTION IN SCRAMJETS: MIXING ENHANCEMENT AND COMBUSTION CHARACTERIZATION EXPERIMENTS.

Degree: Aerospace Engineering, 2005, University of Maryland

 A two-part experimental study was conducted to address the issues of supersonic fuel mixing enhancement and efficient combustor development. The first part of the study… (more)

Subjects/Keywords: Engineering, Aerospace; scramjet; supersonic combustion; supersonic mixing

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APA (6th Edition):

Zang, A. (2005). FUEL INJECTION IN SCRAMJETS: MIXING ENHANCEMENT AND COMBUSTION CHARACTERIZATION EXPERIMENTS. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/2559

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):

Zang, Andrew. “FUEL INJECTION IN SCRAMJETS: MIXING ENHANCEMENT AND COMBUSTION CHARACTERIZATION EXPERIMENTS.” 2005. Thesis, University of Maryland. Accessed March 02, 2021. http://hdl.handle.net/1903/2559.

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

MLA Handbook (7th Edition):

Zang, Andrew. “FUEL INJECTION IN SCRAMJETS: MIXING ENHANCEMENT AND COMBUSTION CHARACTERIZATION EXPERIMENTS.” 2005. Web. 02 Mar 2021.

Vancouver:

Zang A. FUEL INJECTION IN SCRAMJETS: MIXING ENHANCEMENT AND COMBUSTION CHARACTERIZATION EXPERIMENTS. [Internet] [Thesis]. University of Maryland; 2005. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/1903/2559.

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

Council of Science Editors:

Zang A. FUEL INJECTION IN SCRAMJETS: MIXING ENHANCEMENT AND COMBUSTION CHARACTERIZATION EXPERIMENTS. [Thesis]. University of Maryland; 2005. Available from: http://hdl.handle.net/1903/2559

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


Indian Institute of Science

7. Chakraborty, Debasis. Confined Reacting Supersonic Mixing Layer - A DNS Study With Analysis Of Turbulence And Combustion Models.

Degree: PhD, Faculty of Engineering, 2013, Indian Institute of Science

Subjects/Keywords: Supersonic Aerodynamics; Turbulence; Airplanes - Scramjet Engines; Reacting Mixing Layer; Supersonic Reactive Flow; Supersonic Mixing Layer; Reacting Supersonic Mixing Layer; Direct Numerical Simulation (DNS); Supersonic Reacting Flows; Aeronautics

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APA (6th Edition):

Chakraborty, D. (2013). Confined Reacting Supersonic Mixing Layer - A DNS Study With Analysis Of Turbulence And Combustion Models. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2167

Chicago Manual of Style (16th Edition):

Chakraborty, Debasis. “Confined Reacting Supersonic Mixing Layer - A DNS Study With Analysis Of Turbulence And Combustion Models.” 2013. Doctoral Dissertation, Indian Institute of Science. Accessed March 02, 2021. http://etd.iisc.ac.in/handle/2005/2167.

MLA Handbook (7th Edition):

Chakraborty, Debasis. “Confined Reacting Supersonic Mixing Layer - A DNS Study With Analysis Of Turbulence And Combustion Models.” 2013. Web. 02 Mar 2021.

Vancouver:

Chakraborty D. Confined Reacting Supersonic Mixing Layer - A DNS Study With Analysis Of Turbulence And Combustion Models. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2013. [cited 2021 Mar 02]. Available from: http://etd.iisc.ac.in/handle/2005/2167.

Council of Science Editors:

Chakraborty D. Confined Reacting Supersonic Mixing Layer - A DNS Study With Analysis Of Turbulence And Combustion Models. [Doctoral Dissertation]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ac.in/handle/2005/2167


Penn State University

8. Zhang, Liwei. FLOW DYNAMICS AND SCALAR MIXING OF TRANSVERSE JETS INTO CROSSFLOWS .

Degree: 2011, Penn State University

 This research focuses on the simulation of turbulent jets into crossflows under both subsonic and supersonic conditions. The primary objectives are: 1) to establish an… (more)

Subjects/Keywords: large eddy simulation; jet in crossflow; turbulent mixing; jet stability; external excitations; supersonic flow

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APA (6th Edition):

Zhang, L. (2011). FLOW DYNAMICS AND SCALAR MIXING OF TRANSVERSE JETS INTO CROSSFLOWS . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/11676

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):

Zhang, Liwei. “FLOW DYNAMICS AND SCALAR MIXING OF TRANSVERSE JETS INTO CROSSFLOWS .” 2011. Thesis, Penn State University. Accessed March 02, 2021. https://submit-etda.libraries.psu.edu/catalog/11676.

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

MLA Handbook (7th Edition):

Zhang, Liwei. “FLOW DYNAMICS AND SCALAR MIXING OF TRANSVERSE JETS INTO CROSSFLOWS .” 2011. Web. 02 Mar 2021.

Vancouver:

Zhang L. FLOW DYNAMICS AND SCALAR MIXING OF TRANSVERSE JETS INTO CROSSFLOWS . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Mar 02]. Available from: https://submit-etda.libraries.psu.edu/catalog/11676.

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

Council of Science Editors:

Zhang L. FLOW DYNAMICS AND SCALAR MIXING OF TRANSVERSE JETS INTO CROSSFLOWS . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/11676

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

9. Martínez Ferrer, Pedro José. Étude par simulation numérique de l'auto-allumage en écoulement turbulent cisaillé supersonique : Numerical simulation of self-ignition in supersonic turbulent shear flow.

Degree: Docteur es, Energétique, thermique, combustion, 2013, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique

Cette étude est consacrée à l’analyse des écoulements réactifs supersoniques cisailléset, plus particulièrement, des couches de mélange compressibles pouvant se développerdans les moteurs ramjet et… (more)

Subjects/Keywords: Couche de mélange; Combustion supersonique; SImulation numérique directe; Mixing layer; Supersonic combustion; Direct numerical simulation

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APA (6th Edition):

Martínez Ferrer, P. J. (2013). Étude par simulation numérique de l'auto-allumage en écoulement turbulent cisaillé supersonique : Numerical simulation of self-ignition in supersonic turbulent shear flow. (Doctoral Dissertation). Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique. Retrieved from http://www.theses.fr/2013ESMA0018

Chicago Manual of Style (16th Edition):

Martínez Ferrer, Pedro José. “Étude par simulation numérique de l'auto-allumage en écoulement turbulent cisaillé supersonique : Numerical simulation of self-ignition in supersonic turbulent shear flow.” 2013. Doctoral Dissertation, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique. Accessed March 02, 2021. http://www.theses.fr/2013ESMA0018.

MLA Handbook (7th Edition):

Martínez Ferrer, Pedro José. “Étude par simulation numérique de l'auto-allumage en écoulement turbulent cisaillé supersonique : Numerical simulation of self-ignition in supersonic turbulent shear flow.” 2013. Web. 02 Mar 2021.

Vancouver:

Martínez Ferrer PJ. Étude par simulation numérique de l'auto-allumage en écoulement turbulent cisaillé supersonique : Numerical simulation of self-ignition in supersonic turbulent shear flow. [Internet] [Doctoral dissertation]. Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique; 2013. [cited 2021 Mar 02]. Available from: http://www.theses.fr/2013ESMA0018.

Council of Science Editors:

Martínez Ferrer PJ. Étude par simulation numérique de l'auto-allumage en écoulement turbulent cisaillé supersonique : Numerical simulation of self-ignition in supersonic turbulent shear flow. [Doctoral Dissertation]. Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique; 2013. Available from: http://www.theses.fr/2013ESMA0018


Delft University of Technology

10. Pazhev, Ventsislav (author). Experimental Investigation of Transverse Jet Injection into Supersonic Crossflow.

Degree: 2020, Delft University of Technology

Transverse jet injection into supersonic crossflows is encountered with Aerospace applications such as fuel injection in Supersonic Combustion Ramjet (SCRamjet) engines and reaction-jet-based attitude control… (more)

Subjects/Keywords: Supersonic; Jet; Turbulence; SCRamjet; Crossflow; Particle Image Velocimetry (PIV); Schlieren; mixing; trajectory; Nozzles

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APA (6th Edition):

Pazhev, V. (. (2020). Experimental Investigation of Transverse Jet Injection into Supersonic Crossflow. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3dfd72bf-9b4a-4f98-9f95-9f610a466e57

Chicago Manual of Style (16th Edition):

Pazhev, Ventsislav (author). “Experimental Investigation of Transverse Jet Injection into Supersonic Crossflow.” 2020. Masters Thesis, Delft University of Technology. Accessed March 02, 2021. http://resolver.tudelft.nl/uuid:3dfd72bf-9b4a-4f98-9f95-9f610a466e57.

MLA Handbook (7th Edition):

Pazhev, Ventsislav (author). “Experimental Investigation of Transverse Jet Injection into Supersonic Crossflow.” 2020. Web. 02 Mar 2021.

Vancouver:

Pazhev V(. Experimental Investigation of Transverse Jet Injection into Supersonic Crossflow. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Mar 02]. Available from: http://resolver.tudelft.nl/uuid:3dfd72bf-9b4a-4f98-9f95-9f610a466e57.

Council of Science Editors:

Pazhev V(. Experimental Investigation of Transverse Jet Injection into Supersonic Crossflow. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:3dfd72bf-9b4a-4f98-9f95-9f610a466e57


Indian Institute of Science

11. Karthick, S K. Experimental Studies on Gaseous Mixing in a Low Area Ratio Rectangular Supersonic Confined Jet.

Degree: PhD, Engineering, 2018, Indian Institute of Science

 When a supersonic jet passes through a confined passage, it is called as supersonic confined jet. They are encountered in many aerospace applications such as… (more)

Subjects/Keywords: Supersonic Confined Jet; Mixed Length (LMIX); Non-mixed Length; Acetone Planar Laser Induced Fluorescence; Planar Particle Image Velocimetry; Modal Decomposition; Mixing Length; Supersonic Gaseous Ejector; Supersonic Gaseous Mixing; Planar Laser Mie Scattering; Acetone PLIF; Supersonic Ejector; Aerospace Engineering

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APA (6th Edition):

Karthick, S. K. (2018). Experimental Studies on Gaseous Mixing in a Low Area Ratio Rectangular Supersonic Confined Jet. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/4054

Chicago Manual of Style (16th Edition):

Karthick, S K. “Experimental Studies on Gaseous Mixing in a Low Area Ratio Rectangular Supersonic Confined Jet.” 2018. Doctoral Dissertation, Indian Institute of Science. Accessed March 02, 2021. http://etd.iisc.ac.in/handle/2005/4054.

MLA Handbook (7th Edition):

Karthick, S K. “Experimental Studies on Gaseous Mixing in a Low Area Ratio Rectangular Supersonic Confined Jet.” 2018. Web. 02 Mar 2021.

Vancouver:

Karthick SK. Experimental Studies on Gaseous Mixing in a Low Area Ratio Rectangular Supersonic Confined Jet. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2018. [cited 2021 Mar 02]. Available from: http://etd.iisc.ac.in/handle/2005/4054.

Council of Science Editors:

Karthick SK. Experimental Studies on Gaseous Mixing in a Low Area Ratio Rectangular Supersonic Confined Jet. [Doctoral Dissertation]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/4054


Indian Institute of Science

12. Shivakanth Chary, P. Linear Stability Models for Reacting Mixing Layers.

Degree: MSc Engg, Faculty of Engineering, 2018, Indian Institute of Science

 We develop a physics-based reduced-order model of the aero-acoustic sound sources in reacting mixing layers as a method for fast and accurate predictions of the… (more)

Subjects/Keywords: Aeroacoustic Theory; Supersonic Mixing Layers; Aeroacoustic Sound Sources - Model; Compressible Reacting Mixing Layers; Coherent Structures; Supersonic Reacting Mixing Layers; Linear Stability Equations; Linear Parabolized Stability Equations; PSE Equations; Linear Stability Models; Aerospace Engineering

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APA (6th Edition):

Shivakanth Chary, P. (2018). Linear Stability Models for Reacting Mixing Layers. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3267

Chicago Manual of Style (16th Edition):

Shivakanth Chary, P. “Linear Stability Models for Reacting Mixing Layers.” 2018. Masters Thesis, Indian Institute of Science. Accessed March 02, 2021. http://etd.iisc.ac.in/handle/2005/3267.

MLA Handbook (7th Edition):

Shivakanth Chary, P. “Linear Stability Models for Reacting Mixing Layers.” 2018. Web. 02 Mar 2021.

Vancouver:

Shivakanth Chary P. Linear Stability Models for Reacting Mixing Layers. [Internet] [Masters thesis]. Indian Institute of Science; 2018. [cited 2021 Mar 02]. Available from: http://etd.iisc.ac.in/handle/2005/3267.

Council of Science Editors:

Shivakanth Chary P. Linear Stability Models for Reacting Mixing Layers. [Masters Thesis]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3267

13. Opgenorth, Matthew James. Computational Fluid Dynamic Optimization and Design for the Airborne Laser System.

Degree: PhD, Mechanical Engineering, 2010, U of Denver

  The Airborne Laser (ABL) was designed to destroy any ballistic missile shortly after launch that could be a threat to the United States and… (more)

Subjects/Keywords: Computational; Fluid dynamics; Mixing; Optimization; Supersonic ejector; Supersonic nozzle; Applied Mechanics; Mechanical Engineering

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APA (6th Edition):

Opgenorth, M. J. (2010). Computational Fluid Dynamic Optimization and Design for the Airborne Laser System. (Doctoral Dissertation). U of Denver. Retrieved from https://digitalcommons.du.edu/etd/1386

Chicago Manual of Style (16th Edition):

Opgenorth, Matthew James. “Computational Fluid Dynamic Optimization and Design for the Airborne Laser System.” 2010. Doctoral Dissertation, U of Denver. Accessed March 02, 2021. https://digitalcommons.du.edu/etd/1386.

MLA Handbook (7th Edition):

Opgenorth, Matthew James. “Computational Fluid Dynamic Optimization and Design for the Airborne Laser System.” 2010. Web. 02 Mar 2021.

Vancouver:

Opgenorth MJ. Computational Fluid Dynamic Optimization and Design for the Airborne Laser System. [Internet] [Doctoral dissertation]. U of Denver; 2010. [cited 2021 Mar 02]. Available from: https://digitalcommons.du.edu/etd/1386.

Council of Science Editors:

Opgenorth MJ. Computational Fluid Dynamic Optimization and Design for the Airborne Laser System. [Doctoral Dissertation]. U of Denver; 2010. Available from: https://digitalcommons.du.edu/etd/1386


Cal Poly

14. Montre, Trevor Allen. Experimental Investigation of a 2-D Air Augmented Rocket: Effects of Nozzle Lip Thickness on Rocket Mixing and Entrainment.

Degree: MS, Aerospace Engineering, 2011, Cal Poly

  Cold-flow tests were performed using a simulated Air Augmented Rocket (AAR) operating as a mixer-ejector in order to investigate the effects of varied primary… (more)

Subjects/Keywords: Supersonic Air Ejector; Nozzle Lip Thickness; Entrainment; Variable Geometry Ejector; Ejector Mixing Duct; Propulsion and Power

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APA (6th Edition):

Montre, T. A. (2011). Experimental Investigation of a 2-D Air Augmented Rocket: Effects of Nozzle Lip Thickness on Rocket Mixing and Entrainment. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/662 ; 10.15368/theses.2011.217

Chicago Manual of Style (16th Edition):

Montre, Trevor Allen. “Experimental Investigation of a 2-D Air Augmented Rocket: Effects of Nozzle Lip Thickness on Rocket Mixing and Entrainment.” 2011. Masters Thesis, Cal Poly. Accessed March 02, 2021. https://digitalcommons.calpoly.edu/theses/662 ; 10.15368/theses.2011.217.

MLA Handbook (7th Edition):

Montre, Trevor Allen. “Experimental Investigation of a 2-D Air Augmented Rocket: Effects of Nozzle Lip Thickness on Rocket Mixing and Entrainment.” 2011. Web. 02 Mar 2021.

Vancouver:

Montre TA. Experimental Investigation of a 2-D Air Augmented Rocket: Effects of Nozzle Lip Thickness on Rocket Mixing and Entrainment. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2021 Mar 02]. Available from: https://digitalcommons.calpoly.edu/theses/662 ; 10.15368/theses.2011.217.

Council of Science Editors:

Montre TA. Experimental Investigation of a 2-D Air Augmented Rocket: Effects of Nozzle Lip Thickness on Rocket Mixing and Entrainment. [Masters Thesis]. Cal Poly; 2011. Available from: https://digitalcommons.calpoly.edu/theses/662 ; 10.15368/theses.2011.217


University of Maryland

15. Tempel, Travis. Investigation of Supersonic Mixing Using Laser-Induced Breakdown Spectroscopy.

Degree: Mechanical Engineering, 2004, University of Maryland

Supersonic mixing enhancement techniques are of considerable interest; typically qualitative observations of shear layer growth rate are used to compare these techniques. A more accurate… (more)

Subjects/Keywords: Engineering, Mechanical; laser induced breakdown spectroscopy; supersonic mixing

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APA (6th Edition):

Tempel, T. (2004). Investigation of Supersonic Mixing Using Laser-Induced Breakdown Spectroscopy. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/1391

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):

Tempel, Travis. “Investigation of Supersonic Mixing Using Laser-Induced Breakdown Spectroscopy.” 2004. Thesis, University of Maryland. Accessed March 02, 2021. http://hdl.handle.net/1903/1391.

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

MLA Handbook (7th Edition):

Tempel, Travis. “Investigation of Supersonic Mixing Using Laser-Induced Breakdown Spectroscopy.” 2004. Web. 02 Mar 2021.

Vancouver:

Tempel T. Investigation of Supersonic Mixing Using Laser-Induced Breakdown Spectroscopy. [Internet] [Thesis]. University of Maryland; 2004. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/1903/1391.

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

Council of Science Editors:

Tempel T. Investigation of Supersonic Mixing Using Laser-Induced Breakdown Spectroscopy. [Thesis]. University of Maryland; 2004. Available from: http://hdl.handle.net/1903/1391

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


Virginia Tech

16. Rock, Christopher. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors.

Degree: PhD, Aerospace and Ocean Engineering, 2010, Virginia Tech

 A flush-wall injector model and a strut injector model representative of state of the art scramjet engine combustion chambers were experimentally studied in a cold-flow… (more)

Subjects/Keywords: Fuel Injection; Mixing; Hypersonic Propulsion; Supersonic Combustion; Scramjet

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

APA (6th Edition):

Rock, C. (2010). Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77208

Chicago Manual of Style (16th Edition):

Rock, Christopher. “Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors.” 2010. Doctoral Dissertation, Virginia Tech. Accessed March 02, 2021. http://hdl.handle.net/10919/77208.

MLA Handbook (7th Edition):

Rock, Christopher. “Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors.” 2010. Web. 02 Mar 2021.

Vancouver:

Rock C. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/10919/77208.

Council of Science Editors:

Rock C. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/77208


Virginia Tech

17. Grossman, Peter Michael. Experimental Investigation of a Flush-Walled, Diamond-Shaped Fuel Injector for High Mach Number Scramjets.

Degree: MS, Aerospace and Ocean Engineering, 2007, Virginia Tech

 An experimental investigation of a flush-wall, diamond-shaped injector was conducted in the Virginia Tech supersonic wind tunnel. The diamond injector was elongated in the streamwise… (more)

Subjects/Keywords: Scramjets; Hypersonic; Supersonic; Mixing; Penetration; Helium Injection

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APA (6th Edition):

Grossman, P. M. (2007). Experimental Investigation of a Flush-Walled, Diamond-Shaped Fuel Injector for High Mach Number Scramjets. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30974

Chicago Manual of Style (16th Edition):

Grossman, Peter Michael. “Experimental Investigation of a Flush-Walled, Diamond-Shaped Fuel Injector for High Mach Number Scramjets.” 2007. Masters Thesis, Virginia Tech. Accessed March 02, 2021. http://hdl.handle.net/10919/30974.

MLA Handbook (7th Edition):

Grossman, Peter Michael. “Experimental Investigation of a Flush-Walled, Diamond-Shaped Fuel Injector for High Mach Number Scramjets.” 2007. Web. 02 Mar 2021.

Vancouver:

Grossman PM. Experimental Investigation of a Flush-Walled, Diamond-Shaped Fuel Injector for High Mach Number Scramjets. [Internet] [Masters thesis]. Virginia Tech; 2007. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/10919/30974.

Council of Science Editors:

Grossman PM. Experimental Investigation of a Flush-Walled, Diamond-Shaped Fuel Injector for High Mach Number Scramjets. [Masters Thesis]. Virginia Tech; 2007. Available from: http://hdl.handle.net/10919/30974

18. Abdel-Salam, Tarek M. Numerical Studies on Supersonic Mixing and Combustion Phenomena.

Degree: PhD, Mechanical Engineering, 2003, Old Dominion University

  A numerical study is conducted to investigate the mixing, combustion, and flow characteristics of different scramjet-combustor configurations. Three-dimensional models for the combustors have been… (more)

Subjects/Keywords: Combustion; Mixing; Scramjet; Supersonic; Heat Transfer, Combustion; Mechanical Engineering

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APA (6th Edition):

Abdel-Salam, T. M. (2003). Numerical Studies on Supersonic Mixing and Combustion Phenomena. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/105

Chicago Manual of Style (16th Edition):

Abdel-Salam, Tarek M. “Numerical Studies on Supersonic Mixing and Combustion Phenomena.” 2003. Doctoral Dissertation, Old Dominion University. Accessed March 02, 2021. https://digitalcommons.odu.edu/mae_etds/105.

MLA Handbook (7th Edition):

Abdel-Salam, Tarek M. “Numerical Studies on Supersonic Mixing and Combustion Phenomena.” 2003. Web. 02 Mar 2021.

Vancouver:

Abdel-Salam TM. Numerical Studies on Supersonic Mixing and Combustion Phenomena. [Internet] [Doctoral dissertation]. Old Dominion University; 2003. [cited 2021 Mar 02]. Available from: https://digitalcommons.odu.edu/mae_etds/105.

Council of Science Editors:

Abdel-Salam TM. Numerical Studies on Supersonic Mixing and Combustion Phenomena. [Doctoral Dissertation]. Old Dominion University; 2003. Available from: https://digitalcommons.odu.edu/mae_etds/105


University of Cincinnati

19. MURUGAPPAN, SHANMUGAM. INNOVATIVE TECHNIQUES TO IMPROVE MIXING AND PENETRATION IN SCRAMJET COMBUSTORS.

Degree: PhD, Engineering : Aerospace Engineering, 2005, University of Cincinnati

 Scramjet combustors are characterized by an extremely short residence time for the completion of fuel atomization, mixing and combustion. It is therefore desired to develop… (more)

Subjects/Keywords: Engineering, Aerospace; Supersonic; Mixing; Scramjets; Fuel Injection

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APA (6th Edition):

MURUGAPPAN, S. (2005). INNOVATIVE TECHNIQUES TO IMPROVE MIXING AND PENETRATION IN SCRAMJET COMBUSTORS. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1109697512

Chicago Manual of Style (16th Edition):

MURUGAPPAN, SHANMUGAM. “INNOVATIVE TECHNIQUES TO IMPROVE MIXING AND PENETRATION IN SCRAMJET COMBUSTORS.” 2005. Doctoral Dissertation, University of Cincinnati. Accessed March 02, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1109697512.

MLA Handbook (7th Edition):

MURUGAPPAN, SHANMUGAM. “INNOVATIVE TECHNIQUES TO IMPROVE MIXING AND PENETRATION IN SCRAMJET COMBUSTORS.” 2005. Web. 02 Mar 2021.

Vancouver:

MURUGAPPAN S. INNOVATIVE TECHNIQUES TO IMPROVE MIXING AND PENETRATION IN SCRAMJET COMBUSTORS. [Internet] [Doctoral dissertation]. University of Cincinnati; 2005. [cited 2021 Mar 02]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1109697512.

Council of Science Editors:

MURUGAPPAN S. INNOVATIVE TECHNIQUES TO IMPROVE MIXING AND PENETRATION IN SCRAMJET COMBUSTORS. [Doctoral Dissertation]. University of Cincinnati; 2005. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1109697512


University of Michigan

20. Nakagawa, Masaki. Experimental study of compressibility effects on entrainment and mixing in supersonic planar turbulent bluff -body wakes.

Degree: PhD, Pure Sciences, 2001, University of Michigan

 Understanding effects of compressibility on the entrainment and mixing properties of supersonic turbulent shear flows is a key to successful development of the next generation… (more)

Subjects/Keywords: Bluff-body Wakes; Compressibility; Effects; Entrainment; Experimental; Mixing; Planar; Study; Supersonic; Turbulent

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APA (6th Edition):

Nakagawa, M. (2001). Experimental study of compressibility effects on entrainment and mixing in supersonic planar turbulent bluff -body wakes. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/123713

Chicago Manual of Style (16th Edition):

Nakagawa, Masaki. “Experimental study of compressibility effects on entrainment and mixing in supersonic planar turbulent bluff -body wakes.” 2001. Doctoral Dissertation, University of Michigan. Accessed March 02, 2021. http://hdl.handle.net/2027.42/123713.

MLA Handbook (7th Edition):

Nakagawa, Masaki. “Experimental study of compressibility effects on entrainment and mixing in supersonic planar turbulent bluff -body wakes.” 2001. Web. 02 Mar 2021.

Vancouver:

Nakagawa M. Experimental study of compressibility effects on entrainment and mixing in supersonic planar turbulent bluff -body wakes. [Internet] [Doctoral dissertation]. University of Michigan; 2001. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/2027.42/123713.

Council of Science Editors:

Nakagawa M. Experimental study of compressibility effects on entrainment and mixing in supersonic planar turbulent bluff -body wakes. [Doctoral Dissertation]. University of Michigan; 2001. Available from: http://hdl.handle.net/2027.42/123713


University of Florida

21. Tu, Qiuya. Effects of Fuel Injection on Mixing And Upstream Interactions in Supersonic Flow.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 Scramjet engine performance has been studied experimentally and computationally almost under steady-state conditions. Transients of the airflow and fueling in the scramjet’s isolator or combustor… (more)

Subjects/Keywords: Boundary layers; Combustion; Combustion chambers; Internal combustion engines; Mach number; Plumes; Propulsion; Pylons; Supersonic combustion ramjet engines; Supersonics; backpressure  – fluent  – mixing  – penetration  – pylon  – schlieren  – scramjet  – spreading

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APA (6th Edition):

Tu, Q. (2013). Effects of Fuel Injection on Mixing And Upstream Interactions in Supersonic Flow. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0046076

Chicago Manual of Style (16th Edition):

Tu, Qiuya. “Effects of Fuel Injection on Mixing And Upstream Interactions in Supersonic Flow.” 2013. Doctoral Dissertation, University of Florida. Accessed March 02, 2021. https://ufdc.ufl.edu/UFE0046076.

MLA Handbook (7th Edition):

Tu, Qiuya. “Effects of Fuel Injection on Mixing And Upstream Interactions in Supersonic Flow.” 2013. Web. 02 Mar 2021.

Vancouver:

Tu Q. Effects of Fuel Injection on Mixing And Upstream Interactions in Supersonic Flow. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2021 Mar 02]. Available from: https://ufdc.ufl.edu/UFE0046076.

Council of Science Editors:

Tu Q. Effects of Fuel Injection on Mixing And Upstream Interactions in Supersonic Flow. [Doctoral Dissertation]. University of Florida; 2013. Available from: https://ufdc.ufl.edu/UFE0046076


Virginia Tech

22. Bonanos, Aristides Michael. Scramjet Operability Range Studies of an Integrated Aerodynamic-Ramp-Injector/Plasma-Torch Igniter with Hydrogen and Hydrocarbon Fuels.

Degree: PhD, Aerospace and Ocean Engineering, 2005, Virginia Tech

 An integrated aerodynamic-ramp-injector/plasma-torch-igniter of original design was tested in a Mâ = 2, unvitiated, heated flow facility arranged as a diverging duct scramjet combustor. The… (more)

Subjects/Keywords: aeroramp mixing and injection; hypersonic propulsion; plasma torch; supersonic combustion; scramjets

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APA (6th Edition):

Bonanos, A. M. (2005). Scramjet Operability Range Studies of an Integrated Aerodynamic-Ramp-Injector/Plasma-Torch Igniter with Hydrogen and Hydrocarbon Fuels. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28847

Chicago Manual of Style (16th Edition):

Bonanos, Aristides Michael. “Scramjet Operability Range Studies of an Integrated Aerodynamic-Ramp-Injector/Plasma-Torch Igniter with Hydrogen and Hydrocarbon Fuels.” 2005. Doctoral Dissertation, Virginia Tech. Accessed March 02, 2021. http://hdl.handle.net/10919/28847.

MLA Handbook (7th Edition):

Bonanos, Aristides Michael. “Scramjet Operability Range Studies of an Integrated Aerodynamic-Ramp-Injector/Plasma-Torch Igniter with Hydrogen and Hydrocarbon Fuels.” 2005. Web. 02 Mar 2021.

Vancouver:

Bonanos AM. Scramjet Operability Range Studies of an Integrated Aerodynamic-Ramp-Injector/Plasma-Torch Igniter with Hydrogen and Hydrocarbon Fuels. [Internet] [Doctoral dissertation]. Virginia Tech; 2005. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/10919/28847.

Council of Science Editors:

Bonanos AM. Scramjet Operability Range Studies of an Integrated Aerodynamic-Ramp-Injector/Plasma-Torch Igniter with Hydrogen and Hydrocarbon Fuels. [Doctoral Dissertation]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/28847

23. Haimovitch, Yaacov. Investigation of Wall Injectors for Supersonic Mixing Enhancement.

Degree: PhD, Mechanical Engineering, 1994, Old Dominion University

  A comparative study of the interaction between wall mounted swept-ramp injectors and injector nozzle shape has been conducted in a constant area duct to… (more)

Subjects/Keywords: Wall injectors; Supersonic mixing; Scramjet combustors; Aerospace Engineering; Mechanical Engineering; Structures and Materials

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APA (6th Edition):

Haimovitch, Y. (1994). Investigation of Wall Injectors for Supersonic Mixing Enhancement. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/135

Chicago Manual of Style (16th Edition):

Haimovitch, Yaacov. “Investigation of Wall Injectors for Supersonic Mixing Enhancement.” 1994. Doctoral Dissertation, Old Dominion University. Accessed March 02, 2021. https://digitalcommons.odu.edu/mae_etds/135.

MLA Handbook (7th Edition):

Haimovitch, Yaacov. “Investigation of Wall Injectors for Supersonic Mixing Enhancement.” 1994. Web. 02 Mar 2021.

Vancouver:

Haimovitch Y. Investigation of Wall Injectors for Supersonic Mixing Enhancement. [Internet] [Doctoral dissertation]. Old Dominion University; 1994. [cited 2021 Mar 02]. Available from: https://digitalcommons.odu.edu/mae_etds/135.

Council of Science Editors:

Haimovitch Y. Investigation of Wall Injectors for Supersonic Mixing Enhancement. [Doctoral Dissertation]. Old Dominion University; 1994. Available from: https://digitalcommons.odu.edu/mae_etds/135


Virginia Tech

24. Fuller, Raymond Preston. Fuel-vortex interactions for enhanced mixing in supersonic flow.

Degree: PhD, Aerospace Engineering, 1996, Virginia Tech

 An experimental investigation was conducted to compare the supersonic mixing performance between a novel aerodynamic ramp injector and a physical ramp injector. The aerodynamic ramp… (more)

Subjects/Keywords: supersonic; injection; vortex; mixing; aerodynamic; ramp; LD5655.V856 1996.F855

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APA (6th Edition):

Fuller, R. P. (1996). Fuel-vortex interactions for enhanced mixing in supersonic flow. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/38092

Chicago Manual of Style (16th Edition):

Fuller, Raymond Preston. “Fuel-vortex interactions for enhanced mixing in supersonic flow.” 1996. Doctoral Dissertation, Virginia Tech. Accessed March 02, 2021. http://hdl.handle.net/10919/38092.

MLA Handbook (7th Edition):

Fuller, Raymond Preston. “Fuel-vortex interactions for enhanced mixing in supersonic flow.” 1996. Web. 02 Mar 2021.

Vancouver:

Fuller RP. Fuel-vortex interactions for enhanced mixing in supersonic flow. [Internet] [Doctoral dissertation]. Virginia Tech; 1996. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/10919/38092.

Council of Science Editors:

Fuller RP. Fuel-vortex interactions for enhanced mixing in supersonic flow. [Doctoral Dissertation]. Virginia Tech; 1996. Available from: http://hdl.handle.net/10919/38092

25. Burns, Ross Andrew. Development of scalar and velocity imaging diagnostics for supersonic hypermixing strut injector flowfields.

Degree: PhD, Aerospace Engineering, 2014, University of Texas – Austin

 A new diagnostic technique for studying the turbulent mixing characteristics of supersonic mixing flowfields is developed and implemented in two Mach 3 mixing flowfields. The… (more)

Subjects/Keywords: Laser diagnostics; Supersonic; Mixing; Laser induced fluorescence; PIV

…110 Chapter 4: Application of Krypton PLIF to Supersonic Mixing Flowfields .......178 4.1… …Estimation of Thermodynamic Conditions in Supersonic Mixing Flowfields… …Illustration of the effect of averaging on a well-stirred mixing flowfield. a) Instantaneous… …Figure 2.2: Diagram of supersonic nozzle orientation within test cell with beam path and test… …220 Figure 4.2: Schematic of simultaneous PLIF/PIV laser setup used in mixing studies… 

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APA (6th Edition):

Burns, R. A. (2014). Development of scalar and velocity imaging diagnostics for supersonic hypermixing strut injector flowfields. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/28316

Chicago Manual of Style (16th Edition):

Burns, Ross Andrew. “Development of scalar and velocity imaging diagnostics for supersonic hypermixing strut injector flowfields.” 2014. Doctoral Dissertation, University of Texas – Austin. Accessed March 02, 2021. http://hdl.handle.net/2152/28316.

MLA Handbook (7th Edition):

Burns, Ross Andrew. “Development of scalar and velocity imaging diagnostics for supersonic hypermixing strut injector flowfields.” 2014. Web. 02 Mar 2021.

Vancouver:

Burns RA. Development of scalar and velocity imaging diagnostics for supersonic hypermixing strut injector flowfields. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2014. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/2152/28316.

Council of Science Editors:

Burns RA. Development of scalar and velocity imaging diagnostics for supersonic hypermixing strut injector flowfields. [Doctoral Dissertation]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/28316

26. Leonardo da Costa Salemi. Análise de estabilidade linear de camada de mistura compressível binária.

Degree: 2006, Instituto Nacional de Pesquisas Espaciais

 Os sistemas aeroespaciais em sua maioria, se utilizam da liberação de energia química para funcionar. Dentre as aplicações mais comuns estão os motores de aeronaves… (more)

Subjects/Keywords: Estabilidade de escoamento; Camadas cisalhantes; Camadas de mistura (fluidos); Mistura laminar; Misturas binárias; Escoamento compressivel; Flow stability shear layers; Mixing layers (fluids); Binary mixtures; Fluid flow; COMBUSTÃO E PROPULSÃO; Estato reatores de combustão supersônica; Escoamento de fluido; Efeitos de compressibilidade; COMBUSTION AND PROPULSION; Supersonic combustion ramjet engines; Laminar mixing; Compressibility effects

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APA (6th Edition):

Salemi, L. d. C. (2006). Análise de estabilidade linear de camada de mistura compressível binária. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2007/02.15.17.50

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):

Salemi, Leonardo da Costa. “Análise de estabilidade linear de camada de mistura compressível binária.” 2006. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed March 02, 2021. http://urlib.net/sid.inpe.br/[email protected]/2007/02.15.17.50.

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

MLA Handbook (7th Edition):

Salemi, Leonardo da Costa. “Análise de estabilidade linear de camada de mistura compressível binária.” 2006. Web. 02 Mar 2021.

Vancouver:

Salemi LdC. Análise de estabilidade linear de camada de mistura compressível binária. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2006. [cited 2021 Mar 02]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2007/02.15.17.50.

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

Council of Science Editors:

Salemi LdC. Análise de estabilidade linear de camada de mistura compressível binária. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2006. Available from: http://urlib.net/sid.inpe.br/[email protected]/2007/02.15.17.50

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


University of Michigan

27. Bryant, Rodney Aldibonti. Planar laser-induced fluorescence images of fuel mixing and the reaction zone in a supersonic combustor.

Degree: PhD, Applied Sciences, 1998, University of Michigan

 The mixing of fuel and air and the structure of the chemical reaction zone were studied experimentally in a supersonic combustor. Planar images of laser… (more)

Subjects/Keywords: Combustor; Fluorescen; Fluorescence Imaging; Fuel; Images; Induced; Laser; Mixing; Planar Imaging; Reaction; Supersonic; Zone

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APA (6th Edition):

Bryant, R. A. (1998). Planar laser-induced fluorescence images of fuel mixing and the reaction zone in a supersonic combustor. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/130908

Chicago Manual of Style (16th Edition):

Bryant, Rodney Aldibonti. “Planar laser-induced fluorescence images of fuel mixing and the reaction zone in a supersonic combustor.” 1998. Doctoral Dissertation, University of Michigan. Accessed March 02, 2021. http://hdl.handle.net/2027.42/130908.

MLA Handbook (7th Edition):

Bryant, Rodney Aldibonti. “Planar laser-induced fluorescence images of fuel mixing and the reaction zone in a supersonic combustor.” 1998. Web. 02 Mar 2021.

Vancouver:

Bryant RA. Planar laser-induced fluorescence images of fuel mixing and the reaction zone in a supersonic combustor. [Internet] [Doctoral dissertation]. University of Michigan; 1998. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/2027.42/130908.

Council of Science Editors:

Bryant RA. Planar laser-induced fluorescence images of fuel mixing and the reaction zone in a supersonic combustor. [Doctoral Dissertation]. University of Michigan; 1998. Available from: http://hdl.handle.net/2027.42/130908

28. Lee, Gyu Sub S. Design and development of a wind tunnel for the investigation of turbulent compressible mixing layers.

Degree: MS, Aerospace Engineering, 2017, University of Illinois – Urbana-Champaign

 This thesis documents the design, fabrication, and characterization of a new intermittent-blowdown compressible shear layer wind tunnel built at the Gas Dynamics Laboratory (GDL) at… (more)

Subjects/Keywords: Wind tunnel; Compressible flow; Shear layer; Mixing layer; Experimental fluid mechanics; Supersonic flow

…early 1990s, accelerated by interest in the mixing flows in the supersonic combustors aboard… …tunnel is the production of a mixing region between two uniform streams: a sonic/supersonic… …DNS) models have been the primary focus of the CFD community with regard to the mixing… …unsurprisingly, DNS studies of the mixing layer (Sandham and Reynolds [1]; Vreman et al… …published data. More recently, a DNS study of the compressible mixing layer with convective Mach… 

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APA (6th Edition):

Lee, G. S. S. (2017). Design and development of a wind tunnel for the investigation of turbulent compressible mixing layers. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/98393

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):

Lee, Gyu Sub S. “Design and development of a wind tunnel for the investigation of turbulent compressible mixing layers.” 2017. Thesis, University of Illinois – Urbana-Champaign. Accessed March 02, 2021. http://hdl.handle.net/2142/98393.

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

MLA Handbook (7th Edition):

Lee, Gyu Sub S. “Design and development of a wind tunnel for the investigation of turbulent compressible mixing layers.” 2017. Web. 02 Mar 2021.

Vancouver:

Lee GSS. Design and development of a wind tunnel for the investigation of turbulent compressible mixing layers. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2017. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/2142/98393.

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

Council of Science Editors:

Lee GSS. Design and development of a wind tunnel for the investigation of turbulent compressible mixing layers. [Thesis]. University of Illinois – Urbana-Champaign; 2017. Available from: http://hdl.handle.net/2142/98393

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

29. Johnson, Kyle Jacob. AXISYMMETRIC AIR AUGMENTED METHANOL/GOX ROCKET MIXING DUCT EXPERIMENTAL THRUST STUDY.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  A hot-flow axisymmetric Air Augmented Rocket (AAR) test apparatus was constructed to test various mixing duct configurations at static conditions. Primary flow for the… (more)

Subjects/Keywords: Air Augmented Rocket; Mixing Duct Thrust; Variable Mixture Ratio; Supersonic Ejector; Mixer-Ejector; Propulsion and Power

…9.1 Measured Mixing Duct Forces… …16 Figure 10: Attempt at SMORE mixing duct integration… …31 Figure 17: Mixing Duct Dimensions… …32 Figure 18: Mixing Duct Mounting… …33 Figure 19: Mixing Duct Placement Spacer… 

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

APA (6th Edition):

Johnson, K. J. (2013). AXISYMMETRIC AIR AUGMENTED METHANOL/GOX ROCKET MIXING DUCT EXPERIMENTAL THRUST STUDY. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/930 ; 10.15368/theses.2013.13

Chicago Manual of Style (16th Edition):

Johnson, Kyle Jacob. “AXISYMMETRIC AIR AUGMENTED METHANOL/GOX ROCKET MIXING DUCT EXPERIMENTAL THRUST STUDY.” 2013. Masters Thesis, Cal Poly. Accessed March 02, 2021. https://digitalcommons.calpoly.edu/theses/930 ; 10.15368/theses.2013.13.

MLA Handbook (7th Edition):

Johnson, Kyle Jacob. “AXISYMMETRIC AIR AUGMENTED METHANOL/GOX ROCKET MIXING DUCT EXPERIMENTAL THRUST STUDY.” 2013. Web. 02 Mar 2021.

Vancouver:

Johnson KJ. AXISYMMETRIC AIR AUGMENTED METHANOL/GOX ROCKET MIXING DUCT EXPERIMENTAL THRUST STUDY. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2021 Mar 02]. Available from: https://digitalcommons.calpoly.edu/theses/930 ; 10.15368/theses.2013.13.

Council of Science Editors:

Johnson KJ. AXISYMMETRIC AIR AUGMENTED METHANOL/GOX ROCKET MIXING DUCT EXPERIMENTAL THRUST STUDY. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/930 ; 10.15368/theses.2013.13


University of Maryland

30. Balar, Rama Ashok. Fin-Guided Fuel Injection Enhancements for Low Aspect Ratio Scramjet Combustors.

Degree: Aerospace Engineering, 2007, University of Maryland

 Characterization of a three-dimensional Mach 2 scramjet combustor with aspect ratio one has been conducted in order to provide baseline performance data. The maximum combustion… (more)

Subjects/Keywords: Engineering, Aerospace; Engineering, Aerospace; Fuel Injection; Supersonic fuel injection; Fin-guided; Low aspect ratio combustor; Mixing enhancement

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

APA (6th Edition):

Balar, R. A. (2007). Fin-Guided Fuel Injection Enhancements for Low Aspect Ratio Scramjet Combustors. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/6939

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):

Balar, Rama Ashok. “Fin-Guided Fuel Injection Enhancements for Low Aspect Ratio Scramjet Combustors.” 2007. Thesis, University of Maryland. Accessed March 02, 2021. http://hdl.handle.net/1903/6939.

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

MLA Handbook (7th Edition):

Balar, Rama Ashok. “Fin-Guided Fuel Injection Enhancements for Low Aspect Ratio Scramjet Combustors.” 2007. Web. 02 Mar 2021.

Vancouver:

Balar RA. Fin-Guided Fuel Injection Enhancements for Low Aspect Ratio Scramjet Combustors. [Internet] [Thesis]. University of Maryland; 2007. [cited 2021 Mar 02]. Available from: http://hdl.handle.net/1903/6939.

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

Council of Science Editors:

Balar RA. Fin-Guided Fuel Injection Enhancements for Low Aspect Ratio Scramjet Combustors. [Thesis]. University of Maryland; 2007. Available from: http://hdl.handle.net/1903/6939

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

.