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You searched for subject:(Scramjet). Showing records 1 – 30 of 97 total matches.

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Virginia Tech

1. Burger, Scott Kuhlman. Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow.

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

 This study examines the effect of varying injectant molecular weight on the penetration of transverse injection jets into a supersonic crossflow. The injectants considered here… (more)

Subjects/Keywords: molecular weight; mixing; injection; scramjet

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APA (6th Edition):

Burger, S. K. (2010). Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31981

Chicago Manual of Style (16th Edition):

Burger, Scott Kuhlman. “Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow.” 2010. Masters Thesis, Virginia Tech. Accessed June 18, 2019. http://hdl.handle.net/10919/31981.

MLA Handbook (7th Edition):

Burger, Scott Kuhlman. “Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow.” 2010. Web. 18 Jun 2019.

Vancouver:

Burger SK. Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/10919/31981.

Council of Science Editors:

Burger SK. Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/31981


University of Minnesota

2. Tylczak, Erik. Computational Study of Shock/Plume Interactions Between Multiple Jets in Supersonic Crossflow.

Degree: PhD, Aerospace Engineering and Mechanics, 2016, University of Minnesota

 The interaction of multiple jets in supersonic crossflow is simulated using hybrid Reynolds- Averaged Navier Stokes and Large Eddy Simulation turbulence models. The blockage of… (more)

Subjects/Keywords: CFD; Crossflow; Injection; Mixing; Scramjet

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APA (6th Edition):

Tylczak, E. (2016). Computational Study of Shock/Plume Interactions Between Multiple Jets in Supersonic Crossflow. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/182745

Chicago Manual of Style (16th Edition):

Tylczak, Erik. “Computational Study of Shock/Plume Interactions Between Multiple Jets in Supersonic Crossflow.” 2016. Doctoral Dissertation, University of Minnesota. Accessed June 18, 2019. http://hdl.handle.net/11299/182745.

MLA Handbook (7th Edition):

Tylczak, Erik. “Computational Study of Shock/Plume Interactions Between Multiple Jets in Supersonic Crossflow.” 2016. Web. 18 Jun 2019.

Vancouver:

Tylczak E. Computational Study of Shock/Plume Interactions Between Multiple Jets in Supersonic Crossflow. [Internet] [Doctoral dissertation]. University of Minnesota; 2016. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/11299/182745.

Council of Science Editors:

Tylczak E. Computational Study of Shock/Plume Interactions Between Multiple Jets in Supersonic Crossflow. [Doctoral Dissertation]. University of Minnesota; 2016. Available from: http://hdl.handle.net/11299/182745


University of Notre Dame

3. Brock E. Hedlund. Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>.

Degree: MSin Aerospace Engineering, Aerospace and Mechanical Engineering, 2018, University of Notre Dame

  This thesis documents the efforts to characterize the Mach 4.5 flow over a flat plate model with a 30° compression ramp over a range… (more)

Subjects/Keywords: Flow Measurement; Scramjet; Hypersonic

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APA (6th Edition):

Hedlund, B. E. (2018). Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/d791sf2933j

Chicago Manual of Style (16th Edition):

Hedlund, Brock E.. “Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>.” 2018. Masters Thesis, University of Notre Dame. Accessed June 18, 2019. https://curate.nd.edu/show/d791sf2933j.

MLA Handbook (7th Edition):

Hedlund, Brock E.. “Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>.” 2018. Web. 18 Jun 2019.

Vancouver:

Hedlund BE. Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2018. [cited 2019 Jun 18]. Available from: https://curate.nd.edu/show/d791sf2933j.

Council of Science Editors:

Hedlund BE. Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>. [Masters Thesis]. University of Notre Dame; 2018. Available from: https://curate.nd.edu/show/d791sf2933j


Penn State University

4. Li, Jian. IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING.

Degree: PhD, Mechanical Engineering, 2008, Penn State University

 This research focuses on the modeling and simulation of ignition transient and subsequent combustion dynamics in an ethylene fueled supersonic combustion ramjet (scramjet) engine. The… (more)

Subjects/Keywords: supersonic combustion; Scramjet; CFD; air throttling

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APA (6th Edition):

Li, J. (2008). IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9560

Chicago Manual of Style (16th Edition):

Li, Jian. “IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING.” 2008. Doctoral Dissertation, Penn State University. Accessed June 18, 2019. https://etda.libraries.psu.edu/catalog/9560.

MLA Handbook (7th Edition):

Li, Jian. “IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING.” 2008. Web. 18 Jun 2019.

Vancouver:

Li J. IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING. [Internet] [Doctoral dissertation]. Penn State University; 2008. [cited 2019 Jun 18]. Available from: https://etda.libraries.psu.edu/catalog/9560.

Council of Science Editors:

Li J. IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING. [Doctoral Dissertation]. Penn State University; 2008. Available from: https://etda.libraries.psu.edu/catalog/9560


University of Toronto

5. Chan, Jonathan. Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11.

Degree: 2010, University of Toronto

This study investigates the design and aeropropulsive performance of a complete, hydrogen powered, shock-induced combustion ramjet (shcramjet) at a flight Mach number of 11 and… (more)

Subjects/Keywords: hypersonic; propulsion; scramjet; shcramjet; performance; simulation; 0538

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APA (6th Edition):

Chan, J. (2010). Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/25446

Chicago Manual of Style (16th Edition):

Chan, Jonathan. “Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11.” 2010. Masters Thesis, University of Toronto. Accessed June 18, 2019. http://hdl.handle.net/1807/25446.

MLA Handbook (7th Edition):

Chan, Jonathan. “Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11.” 2010. Web. 18 Jun 2019.

Vancouver:

Chan J. Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11. [Internet] [Masters thesis]. University of Toronto; 2010. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/1807/25446.

Council of Science Editors:

Chan J. Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11. [Masters Thesis]. University of Toronto; 2010. Available from: http://hdl.handle.net/1807/25446


Clemson University

6. Quinones, Matthew. Numerical Analysis of Scramjet Cavity Flameholders at Varying Flight Mach Numbers.

Degree: MS, Mechanical Engineering, 2018, Clemson University

 Various types of air breathing engines are used as propulsion devices in aviation. At high flight velocities, the use of a ramjet or supersonic combustion… (more)

Subjects/Keywords: Flame holder; Flame stability; Ramjet; Scramjet

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APA (6th Edition):

Quinones, M. (2018). Numerical Analysis of Scramjet Cavity Flameholders at Varying Flight Mach Numbers. (Masters Thesis). Clemson University. Retrieved from https://tigerprints.clemson.edu/all_theses/3010

Chicago Manual of Style (16th Edition):

Quinones, Matthew. “Numerical Analysis of Scramjet Cavity Flameholders at Varying Flight Mach Numbers.” 2018. Masters Thesis, Clemson University. Accessed June 18, 2019. https://tigerprints.clemson.edu/all_theses/3010.

MLA Handbook (7th Edition):

Quinones, Matthew. “Numerical Analysis of Scramjet Cavity Flameholders at Varying Flight Mach Numbers.” 2018. Web. 18 Jun 2019.

Vancouver:

Quinones M. Numerical Analysis of Scramjet Cavity Flameholders at Varying Flight Mach Numbers. [Internet] [Masters thesis]. Clemson University; 2018. [cited 2019 Jun 18]. Available from: https://tigerprints.clemson.edu/all_theses/3010.

Council of Science Editors:

Quinones M. Numerical Analysis of Scramjet Cavity Flameholders at Varying Flight Mach Numbers. [Masters Thesis]. Clemson University; 2018. Available from: https://tigerprints.clemson.edu/all_theses/3010


North Carolina State University

7. Keistler, Patrick G. A Variable Turbulent Prandtl and Schmidt Number Model Study for Scramjet Applications.

Degree: PhD, Aerospace Engineering, 2009, North Carolina State University

 A turbulence model that allows for the calculation of the variable turbulent Prandtl (Prt) and Schmidt (Sct) numbers as part of the solution is presented.… (more)

Subjects/Keywords: scramjet; schmidt; prandtl; turbulence modeling; cfd

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APA (6th Edition):

Keistler, P. G. (2009). A Variable Turbulent Prandtl and Schmidt Number Model Study for Scramjet Applications. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/3373

Chicago Manual of Style (16th Edition):

Keistler, Patrick G. “A Variable Turbulent Prandtl and Schmidt Number Model Study for Scramjet Applications.” 2009. Doctoral Dissertation, North Carolina State University. Accessed June 18, 2019. http://www.lib.ncsu.edu/resolver/1840.16/3373.

MLA Handbook (7th Edition):

Keistler, Patrick G. “A Variable Turbulent Prandtl and Schmidt Number Model Study for Scramjet Applications.” 2009. Web. 18 Jun 2019.

Vancouver:

Keistler PG. A Variable Turbulent Prandtl and Schmidt Number Model Study for Scramjet Applications. [Internet] [Doctoral dissertation]. North Carolina State University; 2009. [cited 2019 Jun 18]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/3373.

Council of Science Editors:

Keistler PG. A Variable Turbulent Prandtl and Schmidt Number Model Study for Scramjet Applications. [Doctoral Dissertation]. North Carolina State University; 2009. Available from: http://www.lib.ncsu.edu/resolver/1840.16/3373


University of New South Wales

8. Van Pelt, Hilbert. Shock Vector Control applied to a Converging-Diverging Nozzle and a Hypersonic Vehicle.

Degree: Aerospace & Mechanical Engineering, 2018, University of New South Wales

 Shock vector control (SVC) is a technique to control airplanes and spaceplanes by means of fluidinjection into the nozzle flow. SVC is part of fluidic… (more)

Subjects/Keywords: Scramjet; Thrust vectoring; Shock vector control

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APA (6th Edition):

Van Pelt, H. (2018). Shock Vector Control applied to a Converging-Diverging Nozzle and a Hypersonic Vehicle. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/60744 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:53083/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Van Pelt, Hilbert. “Shock Vector Control applied to a Converging-Diverging Nozzle and a Hypersonic Vehicle.” 2018. Doctoral Dissertation, University of New South Wales. Accessed June 18, 2019. http://handle.unsw.edu.au/1959.4/60744 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:53083/SOURCE02?view=true.

MLA Handbook (7th Edition):

Van Pelt, Hilbert. “Shock Vector Control applied to a Converging-Diverging Nozzle and a Hypersonic Vehicle.” 2018. Web. 18 Jun 2019.

Vancouver:

Van Pelt H. Shock Vector Control applied to a Converging-Diverging Nozzle and a Hypersonic Vehicle. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2019 Jun 18]. Available from: http://handle.unsw.edu.au/1959.4/60744 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:53083/SOURCE02?view=true.

Council of Science Editors:

Van Pelt H. Shock Vector Control applied to a Converging-Diverging Nozzle and a Hypersonic Vehicle. [Doctoral Dissertation]. University of New South Wales; 2018. Available from: http://handle.unsw.edu.au/1959.4/60744 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:53083/SOURCE02?view=true


University of New South Wales

9. Brieschenk, Stefan. Laser-Induced Plasma Ignition Studies for Scramjet Propulsion.

Degree: Engineering & Information Technology, 2012, University of New South Wales

 An experimental investigation of the characteristics of laser-induced plasma (LIP)ignition for scramjet propulsion is presented. This work demonstrates for the first time, that LIP can… (more)

Subjects/Keywords: Scramjet propulsion; Laser-induced plasma ignition

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APA (6th Edition):

Brieschenk, S. (2012). Laser-Induced Plasma Ignition Studies for Scramjet Propulsion. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/52252 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10922/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Brieschenk, Stefan. “Laser-Induced Plasma Ignition Studies for Scramjet Propulsion.” 2012. Doctoral Dissertation, University of New South Wales. Accessed June 18, 2019. http://handle.unsw.edu.au/1959.4/52252 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10922/SOURCE02?view=true.

MLA Handbook (7th Edition):

Brieschenk, Stefan. “Laser-Induced Plasma Ignition Studies for Scramjet Propulsion.” 2012. Web. 18 Jun 2019.

Vancouver:

Brieschenk S. Laser-Induced Plasma Ignition Studies for Scramjet Propulsion. [Internet] [Doctoral dissertation]. University of New South Wales; 2012. [cited 2019 Jun 18]. Available from: http://handle.unsw.edu.au/1959.4/52252 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10922/SOURCE02?view=true.

Council of Science Editors:

Brieschenk S. Laser-Induced Plasma Ignition Studies for Scramjet Propulsion. [Doctoral Dissertation]. University of New South Wales; 2012. Available from: http://handle.unsw.edu.au/1959.4/52252 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10922/SOURCE02?view=true


Vanderbilt University

10. Grady, Nathan Ryan. Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut.

Degree: MS, Mechanical Engineering, 2010, Vanderbilt University

 Supersonic air flow over a wall cavity with a rear ramp both with and without an upstream strut was studied with Hydroxyl Tagging Velocimetry (HTV).… (more)

Subjects/Keywords: strut; cavity; laser; HTV; supersonic; scramjet

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APA (6th Edition):

Grady, N. R. (2010). Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut. (Masters Thesis). Vanderbilt University. Retrieved from http://etd.library.vanderbilt.edu/available/etd-12102010-144923/ ;

Chicago Manual of Style (16th Edition):

Grady, Nathan Ryan. “Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut.” 2010. Masters Thesis, Vanderbilt University. Accessed June 18, 2019. http://etd.library.vanderbilt.edu/available/etd-12102010-144923/ ;.

MLA Handbook (7th Edition):

Grady, Nathan Ryan. “Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut.” 2010. Web. 18 Jun 2019.

Vancouver:

Grady NR. Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut. [Internet] [Masters thesis]. Vanderbilt University; 2010. [cited 2019 Jun 18]. Available from: http://etd.library.vanderbilt.edu/available/etd-12102010-144923/ ;.

Council of Science Editors:

Grady NR. Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut. [Masters Thesis]. Vanderbilt University; 2010. Available from: http://etd.library.vanderbilt.edu/available/etd-12102010-144923/ ;


Georgia Tech

11. Miki, Kenji. Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 The main objective of this thesis is to develop a comprehensive model with the capability of modeling both a high Reynolds number and high magnetic… (more)

Subjects/Keywords: Scramjet; MHD; Turbulence; Supersonic flow; Plasma; Magnetohydrodynamics; Airplanes Scramjet engines; Reynolds number; Aerodynamics

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APA (6th Edition):

Miki, K. (2009). Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/26605

Chicago Manual of Style (16th Edition):

Miki, Kenji. “Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion.” 2009. Doctoral Dissertation, Georgia Tech. Accessed June 18, 2019. http://hdl.handle.net/1853/26605.

MLA Handbook (7th Edition):

Miki, Kenji. “Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion.” 2009. Web. 18 Jun 2019.

Vancouver:

Miki K. Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/1853/26605.

Council of Science Editors:

Miki K. Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/26605

12. Rodrigues, Luís. Thermodynamic analysis and optimization of a scramjet engine with thermal management system.

Degree: 2010, RCAAP

 Thermal management of the scramjet engine is one of the key issues of the challenges brought by the development of hypersonic airbreathing vehicles. A Closed… (more)

Subjects/Keywords: Scramjet (motor) - Veículos hipersónicos; Arrefecimento regenerativo - Motor - Veículo hipersónico; Arrefecimento regenerativo - Veículo hipersónico; Gestão térmica - Scramjet (motor) - Veículos hipersónicos

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APA (6th Edition):

Rodrigues, L. (2010). Thermodynamic analysis and optimization of a scramjet engine with thermal management system. (Thesis). RCAAP. Retrieved from https://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3686

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):

Rodrigues, Luís. “Thermodynamic analysis and optimization of a scramjet engine with thermal management system.” 2010. Thesis, RCAAP. Accessed June 18, 2019. https://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3686.

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

MLA Handbook (7th Edition):

Rodrigues, Luís. “Thermodynamic analysis and optimization of a scramjet engine with thermal management system.” 2010. Web. 18 Jun 2019.

Vancouver:

Rodrigues L. Thermodynamic analysis and optimization of a scramjet engine with thermal management system. [Internet] [Thesis]. RCAAP; 2010. [cited 2019 Jun 18]. Available from: https://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3686.

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

Council of Science Editors:

Rodrigues L. Thermodynamic analysis and optimization of a scramjet engine with thermal management system. [Thesis]. RCAAP; 2010. Available from: https://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3686

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


Virginia Tech

13. Prebola, John L. Jr. Performance of a Plasma Torch with Hydrocarbon Feedstocks for Use in Scramjet Combustion.

Degree: MS, Aerospace and Ocean Engineering, 1998, Virginia Tech

 Research was conducted at Virginia Tech on a high-pressure uncooled plasma torch to study torch operational characteristics with hydrocarbon feedstocks and to determine the feasibility… (more)

Subjects/Keywords: plasma torch; hydrocarbon feedstocks; scramjet; scramjet combustion

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APA (6th Edition):

Prebola, J. L. J. (1998). Performance of a Plasma Torch with Hydrocarbon Feedstocks for Use in Scramjet Combustion. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36941

Chicago Manual of Style (16th Edition):

Prebola, John L Jr. “Performance of a Plasma Torch with Hydrocarbon Feedstocks for Use in Scramjet Combustion.” 1998. Masters Thesis, Virginia Tech. Accessed June 18, 2019. http://hdl.handle.net/10919/36941.

MLA Handbook (7th Edition):

Prebola, John L Jr. “Performance of a Plasma Torch with Hydrocarbon Feedstocks for Use in Scramjet Combustion.” 1998. Web. 18 Jun 2019.

Vancouver:

Prebola JLJ. Performance of a Plasma Torch with Hydrocarbon Feedstocks for Use in Scramjet Combustion. [Internet] [Masters thesis]. Virginia Tech; 1998. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/10919/36941.

Council of Science Editors:

Prebola JLJ. Performance of a Plasma Torch with Hydrocarbon Feedstocks for Use in Scramjet Combustion. [Masters Thesis]. Virginia Tech; 1998. Available from: http://hdl.handle.net/10919/36941


University of Kansas

14. Tourani, Chandraprakash Chandra. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.

Degree: MS, Aerospace Engineering, 2011, University of Kansas

 1-D simulations based on the quasi-one-dimensional equations of fluid motion plus an ignition delay model and 2-D numerical simulations based on Reynolds-Averaged Navier-Stokes (RANS) equations… (more)

Subjects/Keywords: Aerospace engineering; Air-breathing propulsion; Combustor; Hypersonic; Quasi one-dimensional; Scramjet

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APA (6th Edition):

Tourani, C. C. (2011). COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7635

Chicago Manual of Style (16th Edition):

Tourani, Chandraprakash Chandra. “COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.” 2011. Masters Thesis, University of Kansas. Accessed June 18, 2019. http://hdl.handle.net/1808/7635.

MLA Handbook (7th Edition):

Tourani, Chandraprakash Chandra. “COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.” 2011. Web. 18 Jun 2019.

Vancouver:

Tourani CC. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/1808/7635.

Council of Science Editors:

Tourani CC. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7635


University of Kansas

15. Hwang, Seung-Jae. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.

Degree: PhD, Aerospace Engineering, 2011, University of Kansas

 Numerical simulations of the scramjet combustor by using the commercial CFD code Fluent with the coupled implicit method with second-order accurate discretization have been obtained… (more)

Subjects/Keywords: Aerospace engineering; Combustor; Enhanced; Mixing; Scramjet; Suction collar; Tabs

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

APA (6th Edition):

Hwang, S. (2011). Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/8080

Chicago Manual of Style (16th Edition):

Hwang, Seung-Jae. “Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.” 2011. Doctoral Dissertation, University of Kansas. Accessed June 18, 2019. http://hdl.handle.net/1808/8080.

MLA Handbook (7th Edition):

Hwang, Seung-Jae. “Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.” 2011. Web. 18 Jun 2019.

Vancouver:

Hwang S. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. [Internet] [Doctoral dissertation]. University of Kansas; 2011. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/1808/8080.

Council of Science Editors:

Hwang S. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. [Doctoral Dissertation]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/8080


University of Kansas

16. Smith, Leslie Ann. The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber.

Degree: PhD, Aerospace Engineering, 2015, University of Kansas

 One of the greatest problems that scramjet research faces is fuel air mixing. The residence time for a scramjet engine, or the time it takes… (more)

Subjects/Keywords: Aerospace engineering; Injector; Micro-mixing; Pulsed Injection; Scramjet; Shear Layer

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APA (6th Edition):

Smith, L. A. (2015). The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19415

Chicago Manual of Style (16th Edition):

Smith, Leslie Ann. “The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber.” 2015. Doctoral Dissertation, University of Kansas. Accessed June 18, 2019. http://hdl.handle.net/1808/19415.

MLA Handbook (7th Edition):

Smith, Leslie Ann. “The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber.” 2015. Web. 18 Jun 2019.

Vancouver:

Smith LA. The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/1808/19415.

Council of Science Editors:

Smith LA. The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber. [Doctoral Dissertation]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19415


University of Kansas

17. Flesberg, Sonja. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.

Degree: PhD, Aerospace Engineering, 2015, University of Kansas

 The scramjet engine has proven to be a viable means of powering a hypersonic vehicle, especially after successful flights of the X-51 WaveRider and various… (more)

Subjects/Keywords: Aerospace engineering; fuel jet injection swirl; mixing enhancement; scramjet combustion

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APA (6th Edition):

Flesberg, S. (2015). Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19380

Chicago Manual of Style (16th Edition):

Flesberg, Sonja. “Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.” 2015. Doctoral Dissertation, University of Kansas. Accessed June 18, 2019. http://hdl.handle.net/1808/19380.

MLA Handbook (7th Edition):

Flesberg, Sonja. “Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.” 2015. Web. 18 Jun 2019.

Vancouver:

Flesberg S. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/1808/19380.

Council of Science Editors:

Flesberg S. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl. [Doctoral Dissertation]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19380


University of Cincinnati

18. Barone, Dominic L. Investigation of TDLAS Measurements in a Scramjet Engine.

Degree: MS, Engineering : Aerospace Engineering, 2010, University of Cincinnati

  An investigation of the viability of tunable diode laser absorption spectroscopy for use as a flow measurement device in a scramjet engine was completed.… (more)

Subjects/Keywords: Aerospace Materials; Tunable Diode Laser; Absorption; Spectroscopy; TDLAS; Scramjet

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

APA (6th Edition):

Barone, D. L. (2010). Investigation of TDLAS Measurements in a Scramjet Engine. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1277130335

Chicago Manual of Style (16th Edition):

Barone, Dominic L. “Investigation of TDLAS Measurements in a Scramjet Engine.” 2010. Masters Thesis, University of Cincinnati. Accessed June 18, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1277130335.

MLA Handbook (7th Edition):

Barone, Dominic L. “Investigation of TDLAS Measurements in a Scramjet Engine.” 2010. Web. 18 Jun 2019.

Vancouver:

Barone DL. Investigation of TDLAS Measurements in a Scramjet Engine. [Internet] [Masters thesis]. University of Cincinnati; 2010. [cited 2019 Jun 18]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1277130335.

Council of Science Editors:

Barone DL. Investigation of TDLAS Measurements in a Scramjet Engine. [Masters Thesis]. University of Cincinnati; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1277130335


Purdue University

19. Williams, Joseph. Trajectory optimization using indirect methods and parametric scramjet cycle analysis.

Degree: MSin Aeronautics and Astronautics, Aeronautics and Astronautics, 2016, Purdue University

  This study investigates the solution of time sensitive regional strike trajectories for hypersonic missiles. This minimum time trajectory is suspected to be best performed… (more)

Subjects/Keywords: Applied sciences; Indirect; Optimization; Powered; Regularization; Scramjet; Trajectory; Aerospace Engineering

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APA (6th Edition):

Williams, J. (2016). Trajectory optimization using indirect methods and parametric scramjet cycle analysis. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/908

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):

Williams, Joseph. “Trajectory optimization using indirect methods and parametric scramjet cycle analysis.” 2016. Thesis, Purdue University. Accessed June 18, 2019. https://docs.lib.purdue.edu/open_access_theses/908.

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

MLA Handbook (7th Edition):

Williams, Joseph. “Trajectory optimization using indirect methods and parametric scramjet cycle analysis.” 2016. Web. 18 Jun 2019.

Vancouver:

Williams J. Trajectory optimization using indirect methods and parametric scramjet cycle analysis. [Internet] [Thesis]. Purdue University; 2016. [cited 2019 Jun 18]. Available from: https://docs.lib.purdue.edu/open_access_theses/908.

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

Council of Science Editors:

Williams J. Trajectory optimization using indirect methods and parametric scramjet cycle analysis. [Thesis]. Purdue University; 2016. Available from: https://docs.lib.purdue.edu/open_access_theses/908

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


University of Toronto

20. West, Jonathan Philip. Numerical Analysis of Ethylene Injection in the Inlet of a Mach Six Scramjet.

Degree: 2011, University of Toronto

A scramjet inlet was designed for use on a small scale, Mach six, ethylene-fuelled vehicle. The inlet used strut-based cantilevered fuel injectors and a well-defined… (more)

Subjects/Keywords: scramjet; ethylene; hypersonic; fuel injection; fuel mixing; computational fluid dynamics; 0538

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APA (6th Edition):

West, J. P. (2011). Numerical Analysis of Ethylene Injection in the Inlet of a Mach Six Scramjet. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/29643

Chicago Manual of Style (16th Edition):

West, Jonathan Philip. “Numerical Analysis of Ethylene Injection in the Inlet of a Mach Six Scramjet.” 2011. Masters Thesis, University of Toronto. Accessed June 18, 2019. http://hdl.handle.net/1807/29643.

MLA Handbook (7th Edition):

West, Jonathan Philip. “Numerical Analysis of Ethylene Injection in the Inlet of a Mach Six Scramjet.” 2011. Web. 18 Jun 2019.

Vancouver:

West JP. Numerical Analysis of Ethylene Injection in the Inlet of a Mach Six Scramjet. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/1807/29643.

Council of Science Editors:

West JP. Numerical Analysis of Ethylene Injection in the Inlet of a Mach Six Scramjet. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/29643


University of California – San Diego

21. Sexton, Scott Michael. Progress Toward Analytic Predictions of Supersonic Hydrocarbon-Air Combustion: Computation of Ignition Times and Supersonic Mixing Layers.

Degree: Engineering Sciences (Mechanical Engineering), 2017, University of California – San Diego

 Combustion in scramjet engines is faced with the limitation of brief residence time in the combustion chamber, requiring fuel and preheated air streams to mix… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; analytic; combustion; hydrocarbon; ignition; scramjet; supersonic

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APA (6th Edition):

Sexton, S. M. (2017). Progress Toward Analytic Predictions of Supersonic Hydrocarbon-Air Combustion: Computation of Ignition Times and Supersonic Mixing Layers. (Thesis). University of California – San Diego. Retrieved from http://www.escholarship.org/uc/item/70799141

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):

Sexton, Scott Michael. “Progress Toward Analytic Predictions of Supersonic Hydrocarbon-Air Combustion: Computation of Ignition Times and Supersonic Mixing Layers.” 2017. Thesis, University of California – San Diego. Accessed June 18, 2019. http://www.escholarship.org/uc/item/70799141.

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

MLA Handbook (7th Edition):

Sexton, Scott Michael. “Progress Toward Analytic Predictions of Supersonic Hydrocarbon-Air Combustion: Computation of Ignition Times and Supersonic Mixing Layers.” 2017. Web. 18 Jun 2019.

Vancouver:

Sexton SM. Progress Toward Analytic Predictions of Supersonic Hydrocarbon-Air Combustion: Computation of Ignition Times and Supersonic Mixing Layers. [Internet] [Thesis]. University of California – San Diego; 2017. [cited 2019 Jun 18]. Available from: http://www.escholarship.org/uc/item/70799141.

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

Council of Science Editors:

Sexton SM. Progress Toward Analytic Predictions of Supersonic Hydrocarbon-Air Combustion: Computation of Ignition Times and Supersonic Mixing Layers. [Thesis]. University of California – San Diego; 2017. Available from: http://www.escholarship.org/uc/item/70799141

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


Oregon State University

22. Nahorniak, Matthew T. Feasibility of Lorentz mixing to enhance combustion in supersonic diffusion flames.

Degree: MS, Mechanical Engineering, 1996, Oregon State University

 The purpose of this research was to determine if it is feasible to apply Lorentz mixing to supersonic diffusion flames, such as those found in… (more)

Subjects/Keywords: Airplanes  – Scramjet engines  – Mathematical models

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APA (6th Edition):

Nahorniak, M. T. (1996). Feasibility of Lorentz mixing to enhance combustion in supersonic diffusion flames. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/34208

Chicago Manual of Style (16th Edition):

Nahorniak, Matthew T. “Feasibility of Lorentz mixing to enhance combustion in supersonic diffusion flames.” 1996. Masters Thesis, Oregon State University. Accessed June 18, 2019. http://hdl.handle.net/1957/34208.

MLA Handbook (7th Edition):

Nahorniak, Matthew T. “Feasibility of Lorentz mixing to enhance combustion in supersonic diffusion flames.” 1996. Web. 18 Jun 2019.

Vancouver:

Nahorniak MT. Feasibility of Lorentz mixing to enhance combustion in supersonic diffusion flames. [Internet] [Masters thesis]. Oregon State University; 1996. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/1957/34208.

Council of Science Editors:

Nahorniak MT. Feasibility of Lorentz mixing to enhance combustion in supersonic diffusion flames. [Masters Thesis]. Oregon State University; 1996. Available from: http://hdl.handle.net/1957/34208


Virginia Tech

23. Markell, Kyle Charles. Exergy Methods for the Generic Analysis and Optimization of Hypersonic Vehicle Concepts.

Degree: MS, Mechanical Engineering, 2005, Virginia Tech

 This thesis work presents detailed results of the application of exergy-based methods to highly dynamic, integrated aerospace systems such as hypersonic vehicle concepts. In particular,… (more)

Subjects/Keywords: scramjet; exergy; optimization; hypersonic's

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APA (6th Edition):

Markell, K. C. (2005). Exergy Methods for the Generic Analysis and Optimization of Hypersonic Vehicle Concepts. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31256

Chicago Manual of Style (16th Edition):

Markell, Kyle Charles. “Exergy Methods for the Generic Analysis and Optimization of Hypersonic Vehicle Concepts.” 2005. Masters Thesis, Virginia Tech. Accessed June 18, 2019. http://hdl.handle.net/10919/31256.

MLA Handbook (7th Edition):

Markell, Kyle Charles. “Exergy Methods for the Generic Analysis and Optimization of Hypersonic Vehicle Concepts.” 2005. Web. 18 Jun 2019.

Vancouver:

Markell KC. Exergy Methods for the Generic Analysis and Optimization of Hypersonic Vehicle Concepts. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/10919/31256.

Council of Science Editors:

Markell KC. Exergy Methods for the Generic Analysis and Optimization of Hypersonic Vehicle Concepts. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/31256


Virginia Tech

24. 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 June 18, 2019. http://hdl.handle.net/10919/77208.

MLA Handbook (7th Edition):

Rock, Christopher. “Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors.” 2010. Web. 18 Jun 2019.

Vancouver:

Rock C. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Jun 18]. 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

25. Cox-Stouffer, Susan K. Jr. Numerical Simulation of Injection and Mixing in Supersonic Flow.

Degree: PhD, Aerospace and Ocean Engineering, 1997, Virginia Tech

 A numerical investigation of the performance of two candidate designs for injection into supersonic flow, including a comparison of two renormalized group theory (RNG) based… (more)

Subjects/Keywords: scramjet; RNG; CFD; ramp injector

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APA (6th Edition):

Cox-Stouffer, S. K. J. (1997). Numerical Simulation of Injection and Mixing in Supersonic Flow. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/29628

Chicago Manual of Style (16th Edition):

Cox-Stouffer, Susan K Jr. “Numerical Simulation of Injection and Mixing in Supersonic Flow.” 1997. Doctoral Dissertation, Virginia Tech. Accessed June 18, 2019. http://hdl.handle.net/10919/29628.

MLA Handbook (7th Edition):

Cox-Stouffer, Susan K Jr. “Numerical Simulation of Injection and Mixing in Supersonic Flow.” 1997. Web. 18 Jun 2019.

Vancouver:

Cox-Stouffer SKJ. Numerical Simulation of Injection and Mixing in Supersonic Flow. [Internet] [Doctoral dissertation]. Virginia Tech; 1997. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/10919/29628.

Council of Science Editors:

Cox-Stouffer SKJ. Numerical Simulation of Injection and Mixing in Supersonic Flow. [Doctoral Dissertation]. Virginia Tech; 1997. Available from: http://hdl.handle.net/10919/29628


Virginia Tech

26. Brewer, Keith Merritt. Exergy Methods for the Mission-Level Analysis and Optimization of Generic Hypersonic Vehicles.

Degree: MS, Mechanical Engineering, 2006, Virginia Tech

 Though the field of hypersonic vehicle design is thriving again, few studies to date demonstrate the technology through a mission in which multiple flight conditions… (more)

Subjects/Keywords: exergy hypersonic optimization scramjet

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APA (6th Edition):

Brewer, K. M. (2006). Exergy Methods for the Mission-Level Analysis and Optimization of Generic Hypersonic Vehicles. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32007

Chicago Manual of Style (16th Edition):

Brewer, Keith Merritt. “Exergy Methods for the Mission-Level Analysis and Optimization of Generic Hypersonic Vehicles.” 2006. Masters Thesis, Virginia Tech. Accessed June 18, 2019. http://hdl.handle.net/10919/32007.

MLA Handbook (7th Edition):

Brewer, Keith Merritt. “Exergy Methods for the Mission-Level Analysis and Optimization of Generic Hypersonic Vehicles.” 2006. Web. 18 Jun 2019.

Vancouver:

Brewer KM. Exergy Methods for the Mission-Level Analysis and Optimization of Generic Hypersonic Vehicles. [Internet] [Masters thesis]. Virginia Tech; 2006. [cited 2019 Jun 18]. Available from: http://hdl.handle.net/10919/32007.

Council of Science Editors:

Brewer KM. Exergy Methods for the Mission-Level Analysis and Optimization of Generic Hypersonic Vehicles. [Masters Thesis]. Virginia Tech; 2006. Available from: http://hdl.handle.net/10919/32007


University of Cambridge

27. Cocks, Peter. Large eddy simulation of supersonic combustion with application to scramjet engines.

Degree: PhD, 2011, University of Cambridge

 This work evaluates the capabilities of the RANS and LES techniques for the simulation of high speed reacting flows. These methods are used to gain… (more)

Subjects/Keywords: 620; Scramjet; Supersonic combustion; Assumed pdf combustion model; Large eddy simulation

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APA (6th Edition):

Cocks, P. (2011). Large eddy simulation of supersonic combustion with application to scramjet engines. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/239344 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.541905

Chicago Manual of Style (16th Edition):

Cocks, Peter. “Large eddy simulation of supersonic combustion with application to scramjet engines.” 2011. Doctoral Dissertation, University of Cambridge. Accessed June 18, 2019. https://www.repository.cam.ac.uk/handle/1810/239344 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.541905.

MLA Handbook (7th Edition):

Cocks, Peter. “Large eddy simulation of supersonic combustion with application to scramjet engines.” 2011. Web. 18 Jun 2019.

Vancouver:

Cocks P. Large eddy simulation of supersonic combustion with application to scramjet engines. [Internet] [Doctoral dissertation]. University of Cambridge; 2011. [cited 2019 Jun 18]. Available from: https://www.repository.cam.ac.uk/handle/1810/239344 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.541905.

Council of Science Editors:

Cocks P. Large eddy simulation of supersonic combustion with application to scramjet engines. [Doctoral Dissertation]. University of Cambridge; 2011. Available from: https://www.repository.cam.ac.uk/handle/1810/239344 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.541905


University of Cambridge

28. Cocks, Peter. Large eddy simulation of supersonic combustion with application to scramjet engines .

Degree: 2011, University of Cambridge

 This work evaluates the capabilities of the RANS and LES techniques for the simulation of high speed reacting flows. These methods are used to gain… (more)

Subjects/Keywords: Scramjet; Supersonic combustion; Assumed pdf combustion model; Large eddy simulation

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APA (6th Edition):

Cocks, P. (2011). Large eddy simulation of supersonic combustion with application to scramjet engines . (Thesis). University of Cambridge. Retrieved from http://www.dspace.cam.ac.uk/handle/1810/239344

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):

Cocks, Peter. “Large eddy simulation of supersonic combustion with application to scramjet engines .” 2011. Thesis, University of Cambridge. Accessed June 18, 2019. http://www.dspace.cam.ac.uk/handle/1810/239344.

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

MLA Handbook (7th Edition):

Cocks, Peter. “Large eddy simulation of supersonic combustion with application to scramjet engines .” 2011. Web. 18 Jun 2019.

Vancouver:

Cocks P. Large eddy simulation of supersonic combustion with application to scramjet engines . [Internet] [Thesis]. University of Cambridge; 2011. [cited 2019 Jun 18]. Available from: http://www.dspace.cam.ac.uk/handle/1810/239344.

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

Council of Science Editors:

Cocks P. Large eddy simulation of supersonic combustion with application to scramjet engines . [Thesis]. University of Cambridge; 2011. Available from: http://www.dspace.cam.ac.uk/handle/1810/239344

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


Iowa State University

29. Hagen, Wyatt. Numerical modeling of liquid jets in crossflow with applications to supersonic combustion ramjets.

Degree: 2017, Iowa State University

 Liquid jets in crossflow are used in a variety of fuel injection systems. Of particular interest in this work is the injection of liquid fuel… (more)

Subjects/Keywords: Atomization; Computational fluid dynamics; Liquid jet; Scramjet; Aerospace Engineering

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APA (6th Edition):

Hagen, W. (2017). Numerical modeling of liquid jets in crossflow with applications to supersonic combustion ramjets. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/16718

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):

Hagen, Wyatt. “Numerical modeling of liquid jets in crossflow with applications to supersonic combustion ramjets.” 2017. Thesis, Iowa State University. Accessed June 18, 2019. https://lib.dr.iastate.edu/etd/16718.

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

MLA Handbook (7th Edition):

Hagen, Wyatt. “Numerical modeling of liquid jets in crossflow with applications to supersonic combustion ramjets.” 2017. Web. 18 Jun 2019.

Vancouver:

Hagen W. Numerical modeling of liquid jets in crossflow with applications to supersonic combustion ramjets. [Internet] [Thesis]. Iowa State University; 2017. [cited 2019 Jun 18]. Available from: https://lib.dr.iastate.edu/etd/16718.

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

Council of Science Editors:

Hagen W. Numerical modeling of liquid jets in crossflow with applications to supersonic combustion ramjets. [Thesis]. Iowa State University; 2017. Available from: https://lib.dr.iastate.edu/etd/16718

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


Wright State University

30. McGillivray, Nathan T. Coupling Computational Fluid Dynamics Analysis and Optimization Techniques for Scramjet Engine Design.

Degree: MSME, Mechanical Engineering, 2018, Wright State University

 Various aspects of hypersonic vehicles are being rapidly explored for improved functionality. One of the main areas of consideration is the fueling of a Supersonic… (more)

Subjects/Keywords: Aerospace Engineering; Mechanical Engineering; CFD; optimization; scramjet; hypersonic; DAKOTA; optimization routine

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APA (6th Edition):

McGillivray, N. T. (2018). Coupling Computational Fluid Dynamics Analysis and Optimization Techniques for Scramjet Engine Design. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1536311445147862

Chicago Manual of Style (16th Edition):

McGillivray, Nathan T. “Coupling Computational Fluid Dynamics Analysis and Optimization Techniques for Scramjet Engine Design.” 2018. Masters Thesis, Wright State University. Accessed June 18, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright1536311445147862.

MLA Handbook (7th Edition):

McGillivray, Nathan T. “Coupling Computational Fluid Dynamics Analysis and Optimization Techniques for Scramjet Engine Design.” 2018. Web. 18 Jun 2019.

Vancouver:

McGillivray NT. Coupling Computational Fluid Dynamics Analysis and Optimization Techniques for Scramjet Engine Design. [Internet] [Masters thesis]. Wright State University; 2018. [cited 2019 Jun 18]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1536311445147862.

Council of Science Editors:

McGillivray NT. Coupling Computational Fluid Dynamics Analysis and Optimization Techniques for Scramjet Engine Design. [Masters Thesis]. Wright State University; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1536311445147862

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