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You searched for subject:(Ramjet). Showing records 1 – 23 of 23 total matches.

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Clemson University

1. 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 January 18, 2021. 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 Jan 2021.

Vancouver:

Quinones M. Numerical Analysis of Scramjet Cavity Flameholders at Varying Flight Mach Numbers. [Internet] [Masters thesis]. Clemson University; 2018. [cited 2021 Jan 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


Delft University of Technology

2. van Wijk, Erwin (author). Submerged Ramjet Intake Modeling.

Degree: 2017, Delft University of Technology

 To evaluate the performance of proposed submerged intakes in an early design phase, a performance analysis model able to evaluate a range of intake geometries… (more)

Subjects/Keywords: Ramjet; Intake; Shock wave boundary layer interaction; Modeling; intake performance

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APA (6th Edition):

van Wijk, E. (. (2017). Submerged Ramjet Intake Modeling. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1203a4cc-adae-45ef-abe2-afc7f735ca7a

Chicago Manual of Style (16th Edition):

van Wijk, Erwin (author). “Submerged Ramjet Intake Modeling.” 2017. Masters Thesis, Delft University of Technology. Accessed January 18, 2021. http://resolver.tudelft.nl/uuid:1203a4cc-adae-45ef-abe2-afc7f735ca7a.

MLA Handbook (7th Edition):

van Wijk, Erwin (author). “Submerged Ramjet Intake Modeling.” 2017. Web. 18 Jan 2021.

Vancouver:

van Wijk E(. Submerged Ramjet Intake Modeling. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:1203a4cc-adae-45ef-abe2-afc7f735ca7a.

Council of Science Editors:

van Wijk E(. Submerged Ramjet Intake Modeling. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:1203a4cc-adae-45ef-abe2-afc7f735ca7a


Delft University of Technology

3. Kwakman, Koen (author). Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance.

Degree: 2019, Delft University of Technology

 Since ramjet propulsion eliminates the need for oxidizers, it provides an alternative to classic rocket engines for missiles and projectiles. However, to capture free-stream air,… (more)

Subjects/Keywords: Submerged; Supersonic; Intake; Inlet; Flush; Ramjet; Propulsion; Missile; Airbreathing

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APA (6th Edition):

Kwakman, K. (. (2019). Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:671fa0bd-d6e5-4159-b29d-6f09dda6dcce

Chicago Manual of Style (16th Edition):

Kwakman, Koen (author). “Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance.” 2019. Masters Thesis, Delft University of Technology. Accessed January 18, 2021. http://resolver.tudelft.nl/uuid:671fa0bd-d6e5-4159-b29d-6f09dda6dcce.

MLA Handbook (7th Edition):

Kwakman, Koen (author). “Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance.” 2019. Web. 18 Jan 2021.

Vancouver:

Kwakman K(. Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:671fa0bd-d6e5-4159-b29d-6f09dda6dcce.

Council of Science Editors:

Kwakman K(. Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:671fa0bd-d6e5-4159-b29d-6f09dda6dcce

4. Choi, Jongseong. Parametric Scramjet Analysis.

Degree: M.S. in Engineering Science, Mechanical Engineering, 2014, University of Mississippi

 The performance of a hypersonic flight vehicle will depend on existing materials and fuels; this work presents the performance of the ideal scramjet engine for… (more)

Subjects/Keywords: Efficiency; Heat Transfer; Mass Flow Rate; Parametric; Ramjet; Scramjet; Aerospace Engineering

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APA (6th Edition):

Choi, J. (2014). Parametric Scramjet Analysis. (Thesis). University of Mississippi. Retrieved from https://egrove.olemiss.edu/etd/535

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):

Choi, Jongseong. “Parametric Scramjet Analysis.” 2014. Thesis, University of Mississippi. Accessed January 18, 2021. https://egrove.olemiss.edu/etd/535.

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

MLA Handbook (7th Edition):

Choi, Jongseong. “Parametric Scramjet Analysis.” 2014. Web. 18 Jan 2021.

Vancouver:

Choi J. Parametric Scramjet Analysis. [Internet] [Thesis]. University of Mississippi; 2014. [cited 2021 Jan 18]. Available from: https://egrove.olemiss.edu/etd/535.

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

Council of Science Editors:

Choi J. Parametric Scramjet Analysis. [Thesis]. University of Mississippi; 2014. Available from: https://egrove.olemiss.edu/etd/535

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


University of Florida

5. Barnes, Frank W IV. Fuel-Air Mixing in a Directly-Fueled Supersonic Cavity Flameholder.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2016, University of Florida

Subjects/Keywords: cavity; flameholding; hypersonics; ramjet

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APA (6th Edition):

Barnes, F. W. I. (2016). Fuel-Air Mixing in a Directly-Fueled Supersonic Cavity Flameholder. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0050304

Chicago Manual of Style (16th Edition):

Barnes, Frank W IV. “Fuel-Air Mixing in a Directly-Fueled Supersonic Cavity Flameholder.” 2016. Doctoral Dissertation, University of Florida. Accessed January 18, 2021. https://ufdc.ufl.edu/UFE0050304.

MLA Handbook (7th Edition):

Barnes, Frank W IV. “Fuel-Air Mixing in a Directly-Fueled Supersonic Cavity Flameholder.” 2016. Web. 18 Jan 2021.

Vancouver:

Barnes FWI. Fuel-Air Mixing in a Directly-Fueled Supersonic Cavity Flameholder. [Internet] [Doctoral dissertation]. University of Florida; 2016. [cited 2021 Jan 18]. Available from: https://ufdc.ufl.edu/UFE0050304.

Council of Science Editors:

Barnes FWI. Fuel-Air Mixing in a Directly-Fueled Supersonic Cavity Flameholder. [Doctoral Dissertation]. University of Florida; 2016. Available from: https://ufdc.ufl.edu/UFE0050304


Cal Poly

6. Sykes, Harrison G. COLD FLOW PERFORMANCE OF A RAMJET ENGINE.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  The design process and construction of the initial modular ramjet attachment to the Cal Poly supersonic wind tunnel is presented. The design of a… (more)

Subjects/Keywords: Propulsion; Supersonic; Ramjet; Performance; Aerodynamics and Fluid Mechanics; Propulsion and Power

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APA (6th Edition):

Sykes, H. G. (2014). COLD FLOW PERFORMANCE OF A RAMJET ENGINE. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182

Chicago Manual of Style (16th Edition):

Sykes, Harrison G. “COLD FLOW PERFORMANCE OF A RAMJET ENGINE.” 2014. Masters Thesis, Cal Poly. Accessed January 18, 2021. https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182.

MLA Handbook (7th Edition):

Sykes, Harrison G. “COLD FLOW PERFORMANCE OF A RAMJET ENGINE.” 2014. Web. 18 Jan 2021.

Vancouver:

Sykes HG. COLD FLOW PERFORMANCE OF A RAMJET ENGINE. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2021 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182.

Council of Science Editors:

Sykes HG. COLD FLOW PERFORMANCE OF A RAMJET ENGINE. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182

7. Dupont, Benoît. Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine.

Degree: M. Sc. A., Génie mécanique, 2016, Université de Sherbrooke

 La demande pour les ressources énergétiques est en hausse alors que leur disponibilité est en baisse. Dans ce contexte, l’industrie du transport et de l’énergie… (more)

Subjects/Keywords: Cascade supersonique; Compresseurs supersoniques; Méthode de visualisation; Fluide compressible; Moteur Ramjet; Régime transitoire

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APA (6th Edition):

Dupont, B. (2016). Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine. (Masters Thesis). Université de Sherbrooke. Retrieved from http://www.collectionscanada.gc.ca/obj/thesescanada/vol2/QSHERU/TC-QSHERU-11143_8823.pdf ; http://savoirs.usherbrooke.ca/bitstream/11143/8823/3/Dupont_Benoit_MScA_2016.pdf

Chicago Manual of Style (16th Edition):

Dupont, Benoît. “Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine.” 2016. Masters Thesis, Université de Sherbrooke. Accessed January 18, 2021. http://www.collectionscanada.gc.ca/obj/thesescanada/vol2/QSHERU/TC-QSHERU-11143_8823.pdf ; http://savoirs.usherbrooke.ca/bitstream/11143/8823/3/Dupont_Benoit_MScA_2016.pdf.

MLA Handbook (7th Edition):

Dupont, Benoît. “Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine.” 2016. Web. 18 Jan 2021.

Vancouver:

Dupont B. Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine. [Internet] [Masters thesis]. Université de Sherbrooke; 2016. [cited 2021 Jan 18]. Available from: http://www.collectionscanada.gc.ca/obj/thesescanada/vol2/QSHERU/TC-QSHERU-11143_8823.pdf ; http://savoirs.usherbrooke.ca/bitstream/11143/8823/3/Dupont_Benoit_MScA_2016.pdf.

Council of Science Editors:

Dupont B. Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine. [Masters Thesis]. Université de Sherbrooke; 2016. Available from: http://www.collectionscanada.gc.ca/obj/thesescanada/vol2/QSHERU/TC-QSHERU-11143_8823.pdf ; http://savoirs.usherbrooke.ca/bitstream/11143/8823/3/Dupont_Benoit_MScA_2016.pdf


Université de Sherbrooke

8. Dupont, Benoît. Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine.

Degree: 2016, Université de Sherbrooke

 La demande pour les ressources énergétiques est en hausse alors que leur disponibilité est en baisse. Dans ce contexte, l’industrie du transport et de l’énergie… (more)

Subjects/Keywords: Cascade supersonique; Compresseurs supersoniques; Méthode de visualisation; Fluide compressible; Moteur Ramjet; Régime transitoire

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APA (6th Edition):

Dupont, B. (2016). Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine. (Masters Thesis). Université de Sherbrooke. Retrieved from http://hdl.handle.net/11143/8823

Chicago Manual of Style (16th Edition):

Dupont, Benoît. “Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine.” 2016. Masters Thesis, Université de Sherbrooke. Accessed January 18, 2021. http://hdl.handle.net/11143/8823.

MLA Handbook (7th Edition):

Dupont, Benoît. “Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine.” 2016. Web. 18 Jan 2021.

Vancouver:

Dupont B. Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine. [Internet] [Masters thesis]. Université de Sherbrooke; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11143/8823.

Council of Science Editors:

Dupont B. Conception du compresseur supersonique du Rim Rotor Rotary Ramjet Engine. [Masters Thesis]. Université de Sherbrooke; 2016. Available from: http://hdl.handle.net/11143/8823


University of Tennessee – Knoxville

9. Holst, Kevin Raymond. A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors.

Degree: MS, Aerospace Engineering, 2012, University of Tennessee – Knoxville

Ramjet and scramjet engines are being developed to provide a more fuel efficient means of propulsion at high Mach numbers. Part of the development… (more)

Subjects/Keywords: Ramjet; Engine Performance; Uncertainty; Free-jet; Ground Test; Other Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Holst, K. R. (2012). A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/1163

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):

Holst, Kevin Raymond. “A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors.” 2012. Thesis, University of Tennessee – Knoxville. Accessed January 18, 2021. https://trace.tennessee.edu/utk_gradthes/1163.

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

MLA Handbook (7th Edition):

Holst, Kevin Raymond. “A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors.” 2012. Web. 18 Jan 2021.

Vancouver:

Holst KR. A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors. [Internet] [Thesis]. University of Tennessee – Knoxville; 2012. [cited 2021 Jan 18]. Available from: https://trace.tennessee.edu/utk_gradthes/1163.

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

Council of Science Editors:

Holst KR. A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors. [Thesis]. University of Tennessee – Knoxville; 2012. Available from: https://trace.tennessee.edu/utk_gradthes/1163

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


INP Toulouse

10. Roux, Anthony. Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets.

Degree: Docteur es, Dynamique des fluides, 2009, INP Toulouse

La conception d'un statoréacteur bénificie aujourd'hui des progrès divers des outils numériques permettant par la même occasion d'alléger les différentes étapes préliminaires de tests en… (more)

Subjects/Keywords: Simulations aux Grandes Echelles; Statoréacteur; Turbulence; Instabilitiés de combustion; Ecoulement Diphasique; Large-Eddy Simulation; Ramjet; Turbulence; Combustion instabilities; Two-Phase Flows

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APA (6th Edition):

Roux, A. (2009). Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2009INPT025H

Chicago Manual of Style (16th Edition):

Roux, Anthony. “Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets.” 2009. Doctoral Dissertation, INP Toulouse. Accessed January 18, 2021. http://www.theses.fr/2009INPT025H.

MLA Handbook (7th Edition):

Roux, Anthony. “Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets.” 2009. Web. 18 Jan 2021.

Vancouver:

Roux A. Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets. [Internet] [Doctoral dissertation]. INP Toulouse; 2009. [cited 2021 Jan 18]. Available from: http://www.theses.fr/2009INPT025H.

Council of Science Editors:

Roux A. Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets. [Doctoral Dissertation]. INP Toulouse; 2009. Available from: http://www.theses.fr/2009INPT025H


University of Kansas

11. Bramlette, Richard. Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine.

Degree: PhD, Mechanical Engineering, 2016, University of Kansas

 In the 1950s, Eugene Gluhareff built the first working “pressure jet” engine, a variation on the classical ramjet engine with a pressurized inlet system relying… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Chemistry; Chemical Kinetics; Computational Fluid Dynamics; Jet Propulsion; Pressure Jet; Propane Oxidation; Ramjet

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APA (6th Edition):

Bramlette, R. (2016). Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/23515

Chicago Manual of Style (16th Edition):

Bramlette, Richard. “Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine.” 2016. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/23515.

MLA Handbook (7th Edition):

Bramlette, Richard. “Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine.” 2016. Web. 18 Jan 2021.

Vancouver:

Bramlette R. Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/23515.

Council of Science Editors:

Bramlette R. Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine. [Doctoral Dissertation]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/23515


Virginia Tech

12. Hewitt, Patrick. Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation.

Degree: PhD, Aerospace and Ocean Engineering, 2008, Virginia Tech

 The present work was conducted with the intent of developing a high-fidelity numerical model of a unique combustion flow problem combining multi-phase fuel injection with… (more)

Subjects/Keywords: Soot; Boron; Combustion; Ducted Rocket; Ramjet; Gas Generator

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APA (6th Edition):

Hewitt, P. (2008). Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28928

Chicago Manual of Style (16th Edition):

Hewitt, Patrick. “Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation.” 2008. Doctoral Dissertation, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/28928.

MLA Handbook (7th Edition):

Hewitt, Patrick. “Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation.” 2008. Web. 18 Jan 2021.

Vancouver:

Hewitt P. Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation. [Internet] [Doctoral dissertation]. Virginia Tech; 2008. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/28928.

Council of Science Editors:

Hewitt P. Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation. [Doctoral Dissertation]. Virginia Tech; 2008. Available from: http://hdl.handle.net/10919/28928

13. Torrez, Sean Michael. Design Refinement and Modeling Methods for Highly-Integrated Hypersonic Vehicles.

Degree: PhD, Aerospace Engineering, 2012, University of Michigan

 A method for early-stage design of high-speed airplanes is presented based on analysis of vehicle performance, including internal flow in the engine and external flows… (more)

Subjects/Keywords: Hypersonic; Optimization; Ramjet; Scramjet; Integrated; Control; Aerospace Engineering; Engineering

…surfaces of aftbody and cowl. 6, 8, 9, 16, 19, 21, 47, 52, 65, 87, 101 ramjet a jet engine that… …16, 23, 101, 103 rocket-ramjet an engine with a rocket engine and a ramjet flowpath… …integrated into a single unit. 2 scramjet a supersonic-combustion ramjet. 2, 12, 13, 16, 23, 26, 41… …49–61, 80–84, 86, 87, 92–96, 98–100, 102–107 turbo-ramjet an engine with a gas turbine and… …a ramjet flowpath integrated into a single unit. 2 unstart a condition in which shocks… 

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APA (6th Edition):

Torrez, S. M. (2012). Design Refinement and Modeling Methods for Highly-Integrated Hypersonic Vehicles. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/93832

Chicago Manual of Style (16th Edition):

Torrez, Sean Michael. “Design Refinement and Modeling Methods for Highly-Integrated Hypersonic Vehicles.” 2012. Doctoral Dissertation, University of Michigan. Accessed January 18, 2021. http://hdl.handle.net/2027.42/93832.

MLA Handbook (7th Edition):

Torrez, Sean Michael. “Design Refinement and Modeling Methods for Highly-Integrated Hypersonic Vehicles.” 2012. Web. 18 Jan 2021.

Vancouver:

Torrez SM. Design Refinement and Modeling Methods for Highly-Integrated Hypersonic Vehicles. [Internet] [Doctoral dissertation]. University of Michigan; 2012. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2027.42/93832.

Council of Science Editors:

Torrez SM. Design Refinement and Modeling Methods for Highly-Integrated Hypersonic Vehicles. [Doctoral Dissertation]. University of Michigan; 2012. Available from: http://hdl.handle.net/2027.42/93832


University of Florida

14. 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 January 18, 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. 18 Jan 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 Jan 18]. 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

15. Gallimore, Scott D. Jr. Operation of a High-Pressure Uncooled Plasma Torch with Hydrocarbon Feedstocks.

Degree: MS, Mechanical Engineering, 1998, Virginia Tech

 The main scope of this project was to determine if a plasma torch could operate on pure hydrocarbon feedstocks and, if so, to catalogue the… (more)

Subjects/Keywords: Plasma; torch; hydrocarbons; combustion; supersonic; scramjet; ramjet; arc; ignitor; generator

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

APA (6th Edition):

Gallimore, S. D. J. (1998). Operation of a High-Pressure Uncooled Plasma Torch with Hydrocarbon Feedstocks. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36917

Chicago Manual of Style (16th Edition):

Gallimore, Scott D Jr. “Operation of a High-Pressure Uncooled Plasma Torch with Hydrocarbon Feedstocks.” 1998. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/36917.

MLA Handbook (7th Edition):

Gallimore, Scott D Jr. “Operation of a High-Pressure Uncooled Plasma Torch with Hydrocarbon Feedstocks.” 1998. Web. 18 Jan 2021.

Vancouver:

Gallimore SDJ. Operation of a High-Pressure Uncooled Plasma Torch with Hydrocarbon Feedstocks. [Internet] [Masters thesis]. Virginia Tech; 1998. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/36917.

Council of Science Editors:

Gallimore SDJ. Operation of a High-Pressure Uncooled Plasma Torch with Hydrocarbon Feedstocks. [Masters Thesis]. Virginia Tech; 1998. Available from: http://hdl.handle.net/10919/36917


Virginia Tech

16. Ogg, John Chappell. Investigation of liquid fuel jet injection into a simulated subsonic "dump" combustor.

Degree: MS, Aerospace Engineering, 1979, Virginia Tech

Subjects/Keywords: LD5655.V855 1979.O33; Liquid propellant rockets; Rockets (Aeronautics)  – Ramjet engines

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APA (6th Edition):

Ogg, J. C. (1979). Investigation of liquid fuel jet injection into a simulated subsonic "dump" combustor. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/101411

Chicago Manual of Style (16th Edition):

Ogg, John Chappell. “Investigation of liquid fuel jet injection into a simulated subsonic "dump" combustor.” 1979. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/101411.

MLA Handbook (7th Edition):

Ogg, John Chappell. “Investigation of liquid fuel jet injection into a simulated subsonic "dump" combustor.” 1979. Web. 18 Jan 2021.

Vancouver:

Ogg JC. Investigation of liquid fuel jet injection into a simulated subsonic "dump" combustor. [Internet] [Masters thesis]. Virginia Tech; 1979. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/101411.

Council of Science Editors:

Ogg JC. Investigation of liquid fuel jet injection into a simulated subsonic "dump" combustor. [Masters Thesis]. Virginia Tech; 1979. Available from: http://hdl.handle.net/10919/101411

17. Gabriela Silva Moura. Análise teórica e experimental do desempenho de um estado-reator a combustível sólido utilizando polibutadieno hidroxilado.

Degree: 2007, Instituto Nacional de Pesquisas Espaciais

Solid fuel ramjets (SFR´s) constitute an important subject in the current stage of propulsion research. These systems can incorporate the high performance achieved by conventional… (more)

Subjects/Keywords: ENGENHARIA E TECNOLOGIA ESPACIAL Estato-reator; Polibutadieno hidroxilado; Gerador de ar viciado; Teoria de regressão; Impulsão específica; SPACE TECHNOLOGY AND ENGINEERING; Ramjet; Hidroxyl termineted; Viciated air generation; Teory of regression; Specific impulsion

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APA (6th Edition):

Moura, G. S. (2007). Análise teórica e experimental do desempenho de um estado-reator a combustível sólido utilizando polibutadieno hidroxilado. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2007/05.07.17.31

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):

Moura, Gabriela Silva. “Análise teórica e experimental do desempenho de um estado-reator a combustível sólido utilizando polibutadieno hidroxilado.” 2007. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed January 18, 2021. http://urlib.net/sid.inpe.br/[email protected]/2007/05.07.17.31.

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

MLA Handbook (7th Edition):

Moura, Gabriela Silva. “Análise teórica e experimental do desempenho de um estado-reator a combustível sólido utilizando polibutadieno hidroxilado.” 2007. Web. 18 Jan 2021.

Vancouver:

Moura GS. Análise teórica e experimental do desempenho de um estado-reator a combustível sólido utilizando polibutadieno hidroxilado. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2007. [cited 2021 Jan 18]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2007/05.07.17.31.

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

Council of Science Editors:

Moura GS. Análise teórica e experimental do desempenho de um estado-reator a combustível sólido utilizando polibutadieno hidroxilado. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2007. Available from: http://urlib.net/sid.inpe.br/[email protected]/2007/05.07.17.31

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


Indian Institute of Science

18. Sivaprakasam, M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.

Degree: MSc Engg, Faculty of Engineering, 2013, Indian Institute of Science

 In the present work, two phase reacting flow in a single cavity Trapped Vortex Combustor (TVC) is studied at atmospheric conditions. KIVA-3V, numerical program for… (more)

Subjects/Keywords: Trapped Vortex Combustor (TVC); Cavity Combustor; Trapped Vortex Combustor - Flow Modelling; Ramjet Engines; Trapped Vortex Combustor - Two Phase Reacting Flow; Cavity Combustor - Reacting Flow - Numerical Simulations; Taylor Analogy Breakup (TAB); Heat Engineering

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APA (6th Edition):

Sivaprakasam, M. (2013). Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2011

Chicago Manual of Style (16th Edition):

Sivaprakasam, M. “Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.” 2013. Masters Thesis, Indian Institute of Science. Accessed January 18, 2021. http://etd.iisc.ac.in/handle/2005/2011.

MLA Handbook (7th Edition):

Sivaprakasam, M. “Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.” 2013. Web. 18 Jan 2021.

Vancouver:

Sivaprakasam M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. [Internet] [Masters thesis]. Indian Institute of Science; 2013. [cited 2021 Jan 18]. Available from: http://etd.iisc.ac.in/handle/2005/2011.

Council of Science Editors:

Sivaprakasam M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. [Masters Thesis]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ac.in/handle/2005/2011


Pontifical Catholic University of Rio de Janeiro

19. HELIO DE MIRANDA CORDEIRO. [en] FLOW FIELD COMPUTATIONAL ANALYSIS IN A SOLID FUEL RAMJET COMBUSTOR.

Degree: 2003, Pontifical Catholic University of Rio de Janeiro

[pt] Essa dissertação realiza uma análise do escoamento reativo e turbulento no interior do combustor de um estato reator a combustível sólido. Investiga-se diferentes modelos… (more)

Subjects/Keywords: [pt] COMBUSTAO; [en] COMBUSTION; [pt] ANALISE COMPUTACIONAL; [en] COMPUTATIONAL ANALYSIS; [pt] COMBUSTIVEL SOLIDO; [en] SOLID FUEL; [pt] ESTATO REATOR; [en] RAMJET

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APA (6th Edition):

CORDEIRO, H. D. M. (2003). [en] FLOW FIELD COMPUTATIONAL ANALYSIS IN A SOLID FUEL RAMJET COMBUSTOR. (Thesis). Pontifical Catholic University of Rio de Janeiro. Retrieved from http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=3283

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):

CORDEIRO, HELIO DE MIRANDA. “[en] FLOW FIELD COMPUTATIONAL ANALYSIS IN A SOLID FUEL RAMJET COMBUSTOR.” 2003. Thesis, Pontifical Catholic University of Rio de Janeiro. Accessed January 18, 2021. http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=3283.

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

MLA Handbook (7th Edition):

CORDEIRO, HELIO DE MIRANDA. “[en] FLOW FIELD COMPUTATIONAL ANALYSIS IN A SOLID FUEL RAMJET COMBUSTOR.” 2003. Web. 18 Jan 2021.

Vancouver:

CORDEIRO HDM. [en] FLOW FIELD COMPUTATIONAL ANALYSIS IN A SOLID FUEL RAMJET COMBUSTOR. [Internet] [Thesis]. Pontifical Catholic University of Rio de Janeiro; 2003. [cited 2021 Jan 18]. Available from: http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=3283.

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

Council of Science Editors:

CORDEIRO HDM. [en] FLOW FIELD COMPUTATIONAL ANALYSIS IN A SOLID FUEL RAMJET COMBUSTOR. [Thesis]. Pontifical Catholic University of Rio de Janeiro; 2003. Available from: http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=3283

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


University of Florida

20. CUESTA, DANIEL F. ( Author, Primary ). Effects of Hydrogen and Ethylene Injection Schemes in a Supersonic Airstream.

Degree: University of Florida

Subjects/Keywords: Combustion; Combustion chambers; Combustion efficiency; Fuel injection; Hydrogen; Mach number; Propulsion; Stagnation pressure; Supersonic combustion ramjet engines; Supersonics

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APA (6th Edition):

CUESTA, DANIEL F. ( Author, P. ). (n.d.). Effects of Hydrogen and Ethylene Injection Schemes in a Supersonic Airstream. (Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0002725

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

Chicago Manual of Style (16th Edition):

CUESTA, DANIEL F. ( Author, Primary ). “Effects of Hydrogen and Ethylene Injection Schemes in a Supersonic Airstream.” Thesis, University of Florida. Accessed January 18, 2021. https://ufdc.ufl.edu/UFE0002725.

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

MLA Handbook (7th Edition):

CUESTA, DANIEL F. ( Author, Primary ). “Effects of Hydrogen and Ethylene Injection Schemes in a Supersonic Airstream.” Web. 18 Jan 2021.

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

Vancouver:

CUESTA, DANIEL F. ( Author P). Effects of Hydrogen and Ethylene Injection Schemes in a Supersonic Airstream. [Internet] [Thesis]. University of Florida; [cited 2021 Jan 18]. Available from: https://ufdc.ufl.edu/UFE0002725.

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

Council of Science Editors:

CUESTA, DANIEL F. ( Author P). Effects of Hydrogen and Ethylene Injection Schemes in a Supersonic Airstream. [Thesis]. University of Florida; Available from: https://ufdc.ufl.edu/UFE0002725

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


University of Florida

21. Stuthers, Stephen R. Measurements of Boundary Layers in a Direct-Connect Facility for Hypersonic Propulsion.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2016, University of Florida

 Presented in this study is the design and implementation of an experimental procedure which utilizes pitot tubes to measure and characterize compressible turbulent boundary layers.… (more)

Subjects/Keywords: Boundary layers; Contour lines; Mach number; Pitot tubes; Pressure sensors; Static pressure; Supersonic combustion ramjet engines; Velocity; Velocity distribution; Wind tunnels; boundary  – compressible  – duct  – flow  – hypersonic  – isolator  – layers  – measurements  – pitot  – propulsion  – scramjet  – supersonic  – turbulent; City of Gainesville ( local )

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APA (6th Edition):

Stuthers, S. R. (2016). Measurements of Boundary Layers in a Direct-Connect Facility for Hypersonic Propulsion. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0050813

Chicago Manual of Style (16th Edition):

Stuthers, Stephen R. “Measurements of Boundary Layers in a Direct-Connect Facility for Hypersonic Propulsion.” 2016. Masters Thesis, University of Florida. Accessed January 18, 2021. https://ufdc.ufl.edu/UFE0050813.

MLA Handbook (7th Edition):

Stuthers, Stephen R. “Measurements of Boundary Layers in a Direct-Connect Facility for Hypersonic Propulsion.” 2016. Web. 18 Jan 2021.

Vancouver:

Stuthers SR. Measurements of Boundary Layers in a Direct-Connect Facility for Hypersonic Propulsion. [Internet] [Masters thesis]. University of Florida; 2016. [cited 2021 Jan 18]. Available from: https://ufdc.ufl.edu/UFE0050813.

Council of Science Editors:

Stuthers SR. Measurements of Boundary Layers in a Direct-Connect Facility for Hypersonic Propulsion. [Masters Thesis]. University of Florida; 2016. Available from: https://ufdc.ufl.edu/UFE0050813

22. 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 January 18, 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. 18 Jan 2021.

Vancouver:

Salemi LdC. Análise de estabilidade linear de camada de mistura compressível binária. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2006. [cited 2021 Jan 18]. 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


Brno University of Technology

23. Bártek, Petr. Termodynamika proudových motorů: Thermodynamics of jet engines.

Degree: 2019, Brno University of Technology

 This research introduces the reader to a brief analysis of various types of aircraft engines, with particular focus upon jet engines. Amongst the types of… (more)

Subjects/Keywords: Termodynamika proudových motorů; termodynamický cyklus; letecký motor; historie leteckých motorů; turbovrtulový motor; turbokompresorový motor; turboventilátorový motor; náporový motor; propfan; pulzní motor; tah motoru; účinnost proudového motoru.; Thermodynamics of jet engines; thermodynamical cycle; aircraft engine; history of the jet engines; turboprop; turbojet; turbofan; ramjet; propfan; pulse engine; jet thrust; jet engine efficiency.

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APA (6th Edition):

Bártek, P. (2019). Termodynamika proudových motorů: Thermodynamics of jet engines. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/8130

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):

Bártek, Petr. “Termodynamika proudových motorů: Thermodynamics of jet engines.” 2019. Thesis, Brno University of Technology. Accessed January 18, 2021. http://hdl.handle.net/11012/8130.

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

MLA Handbook (7th Edition):

Bártek, Petr. “Termodynamika proudových motorů: Thermodynamics of jet engines.” 2019. Web. 18 Jan 2021.

Vancouver:

Bártek P. Termodynamika proudových motorů: Thermodynamics of jet engines. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11012/8130.

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

Council of Science Editors:

Bártek P. Termodynamika proudových motorů: Thermodynamics of jet engines. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/8130

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

.