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You searched for +publisher:"University of Michigan" +contributor:("Gamba, Mirko"). Showing records 1 – 21 of 21 total matches.

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University of Michigan

1. Hassanaly, Malik. Extreme Events in Turbulent Combustion.

Degree: PhD, Aerospace Engineering, 2019, University of Michigan

 The design of reliable combustors is a crucial aspect of propulsion and energy production applications: a faulty engine could cost human lives and millions (if… (more)

Subjects/Keywords: Extreme events; Lyapunov analysis; Turbulent combustion; Rare events; Aerospace Engineering; Engineering

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APA (6th Edition):

Hassanaly, M. (2019). Extreme Events in Turbulent Combustion. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/151504

Chicago Manual of Style (16th Edition):

Hassanaly, Malik. “Extreme Events in Turbulent Combustion.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/151504.

MLA Handbook (7th Edition):

Hassanaly, Malik. “Extreme Events in Turbulent Combustion.” 2019. Web. 14 Apr 2021.

Vancouver:

Hassanaly M. Extreme Events in Turbulent Combustion. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/151504.

Council of Science Editors:

Hassanaly M. Extreme Events in Turbulent Combustion. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/151504

2. Wagnon, Scott William. Chemical Kinetics for Advanced Combustion Strategies.

Degree: PhD, Mechanical Engineering, 2014, University of Michigan

 This dissertation presents new understanding of the role of fuel chemistry on reaction pathways important to fuel oxidation and ignition at conditions relevant to advanced… (more)

Subjects/Keywords: Alternative Fuels; Experimental Chemical Kinetics; Low Temperature Combustion; Rapid Compression Facility; Shock Tube; Mechanical Engineering; Engineering

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APA (6th Edition):

Wagnon, S. W. (2014). Chemical Kinetics for Advanced Combustion Strategies. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/108943

Chicago Manual of Style (16th Edition):

Wagnon, Scott William. “Chemical Kinetics for Advanced Combustion Strategies.” 2014. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/108943.

MLA Handbook (7th Edition):

Wagnon, Scott William. “Chemical Kinetics for Advanced Combustion Strategies.” 2014. Web. 14 Apr 2021.

Vancouver:

Wagnon SW. Chemical Kinetics for Advanced Combustion Strategies. [Internet] [Doctoral dissertation]. University of Michigan; 2014. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/108943.

Council of Science Editors:

Wagnon SW. Chemical Kinetics for Advanced Combustion Strategies. [Doctoral Dissertation]. University of Michigan; 2014. Available from: http://hdl.handle.net/2027.42/108943


University of Michigan

3. France, Jacob. High Temperature and Pressure Measurements from TDLAS Through the Application of 2nd Derivative Fitting and the Aggregate Boltzmann Method.

Degree: PhD, Aerospace Engineering, 2019, University of Michigan

 This work expands Tunable Diode Laser Absorption Spectroscopy (TDLAS) measurement and data processing techniques. Specifically, it introduces new data acquisition and data reduction techniques that… (more)

Subjects/Keywords: Tunable Diode Laser Absorption Spectroscopy; Planar Tunable Diode Laser Absorption Spectroscopy; Linear Array Camera; Second Derivative Fitting; Aggregate Boltzmann Plot; Aerospace Engineering; Engineering

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APA (6th Edition):

France, J. (2019). High Temperature and Pressure Measurements from TDLAS Through the Application of 2nd Derivative Fitting and the Aggregate Boltzmann Method. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/149901

Chicago Manual of Style (16th Edition):

France, Jacob. “High Temperature and Pressure Measurements from TDLAS Through the Application of 2nd Derivative Fitting and the Aggregate Boltzmann Method.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/149901.

MLA Handbook (7th Edition):

France, Jacob. “High Temperature and Pressure Measurements from TDLAS Through the Application of 2nd Derivative Fitting and the Aggregate Boltzmann Method.” 2019. Web. 14 Apr 2021.

Vancouver:

France J. High Temperature and Pressure Measurements from TDLAS Through the Application of 2nd Derivative Fitting and the Aggregate Boltzmann Method. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/149901.

Council of Science Editors:

France J. High Temperature and Pressure Measurements from TDLAS Through the Application of 2nd Derivative Fitting and the Aggregate Boltzmann Method. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/149901


University of Michigan

4. Medina, Mario. Experimental Studies of High-pressure Gasoline Fuel Sprays for Advanced Internal Combustion Engines.

Degree: PhD, Mechanical Engineering, 2020, University of Michigan

 While much has been learned about gasoline direct injection sprays, there are still large gaps in the fundamental knowledge of the effects of high-pressure (over… (more)

Subjects/Keywords: Fuel sprays; High pressure injection; Gasoline fuel; Mechanical Engineering; Transportation; Engineering

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APA (6th Edition):

Medina, M. (2020). Experimental Studies of High-pressure Gasoline Fuel Sprays for Advanced Internal Combustion Engines. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/155095

Chicago Manual of Style (16th Edition):

Medina, Mario. “Experimental Studies of High-pressure Gasoline Fuel Sprays for Advanced Internal Combustion Engines.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/155095.

MLA Handbook (7th Edition):

Medina, Mario. “Experimental Studies of High-pressure Gasoline Fuel Sprays for Advanced Internal Combustion Engines.” 2020. Web. 14 Apr 2021.

Vancouver:

Medina M. Experimental Studies of High-pressure Gasoline Fuel Sprays for Advanced Internal Combustion Engines. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/155095.

Council of Science Editors:

Medina M. Experimental Studies of High-pressure Gasoline Fuel Sprays for Advanced Internal Combustion Engines. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/155095


University of Michigan

5. Fievet, Romain. Impact of Vibrational Nonequilibrium on the Simulation and Modeling of Dual-Mode Scramjets.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 The practical realization of supersonic flight relies on the development of a robust propulsion system. These air-breathing scramjet engines process fuel and high-speed air to… (more)

Subjects/Keywords: Hypersonics; Computational fluid dynamics; Vibrational nonequilibrium; Aerospace Engineering; Engineering; Science

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APA (6th Edition):

Fievet, R. (2018). Impact of Vibrational Nonequilibrium on the Simulation and Modeling of Dual-Mode Scramjets. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/143909

Chicago Manual of Style (16th Edition):

Fievet, Romain. “Impact of Vibrational Nonequilibrium on the Simulation and Modeling of Dual-Mode Scramjets.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/143909.

MLA Handbook (7th Edition):

Fievet, Romain. “Impact of Vibrational Nonequilibrium on the Simulation and Modeling of Dual-Mode Scramjets.” 2018. Web. 14 Apr 2021.

Vancouver:

Fievet R. Impact of Vibrational Nonequilibrium on the Simulation and Modeling of Dual-Mode Scramjets. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/143909.

Council of Science Editors:

Fievet R. Impact of Vibrational Nonequilibrium on the Simulation and Modeling of Dual-Mode Scramjets. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/143909


University of Michigan

6. Tibavinsky, Ivan. Thermal Emission of Strontium Products for Scalar Diagnostics in Internal Combustion Engines.

Degree: PhD, Mechanical Engineering, 2019, University of Michigan

 Developments in optical diagnostics for combustion systems have been essential to the recent improvements in efficiency and abatement of emissions that internal combustion engines have… (more)

Subjects/Keywords: Engine optical diagnostics; Strontium spectral emission; strontium monohydroxide; internal combustion engines; Mechanical Engineering; Engineering

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APA (6th Edition):

Tibavinsky, I. (2019). Thermal Emission of Strontium Products for Scalar Diagnostics in Internal Combustion Engines. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/153368

Chicago Manual of Style (16th Edition):

Tibavinsky, Ivan. “Thermal Emission of Strontium Products for Scalar Diagnostics in Internal Combustion Engines.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/153368.

MLA Handbook (7th Edition):

Tibavinsky, Ivan. “Thermal Emission of Strontium Products for Scalar Diagnostics in Internal Combustion Engines.” 2019. Web. 14 Apr 2021.

Vancouver:

Tibavinsky I. Thermal Emission of Strontium Products for Scalar Diagnostics in Internal Combustion Engines. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/153368.

Council of Science Editors:

Tibavinsky I. Thermal Emission of Strontium Products for Scalar Diagnostics in Internal Combustion Engines. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/153368


University of Michigan

7. Skiba, Aaron. On the Structure of Premixed Flames Subjected to Extreme Levels of Turbulence.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 Developing next-generation propulsion and energy production devices that are efficient, cost-effective, and generate little to no harmful emissions will require highly-accurate, robust, yet computationally tractable… (more)

Subjects/Keywords: Turbulent Premixed Combustion; Regime Diagram; Extreme Turbulence; Hi-Pilot Burner; Aerospace Engineering; Engineering

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APA (6th Edition):

Skiba, A. (2017). On the Structure of Premixed Flames Subjected to Extreme Levels of Turbulence. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/138725

Chicago Manual of Style (16th Edition):

Skiba, Aaron. “On the Structure of Premixed Flames Subjected to Extreme Levels of Turbulence.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/138725.

MLA Handbook (7th Edition):

Skiba, Aaron. “On the Structure of Premixed Flames Subjected to Extreme Levels of Turbulence.” 2017. Web. 14 Apr 2021.

Vancouver:

Skiba A. On the Structure of Premixed Flames Subjected to Extreme Levels of Turbulence. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/138725.

Council of Science Editors:

Skiba A. On the Structure of Premixed Flames Subjected to Extreme Levels of Turbulence. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/138725


University of Michigan

8. Chong, Shao Teng. Modeling of Turbulent Sooting Flames.

Degree: PhD, Mechanical Engineering, 2018, University of Michigan

 Modeling multiphase particles in turbulent fluid environment is a challenging task. To accurately describe the size distribution, a large number of scalars need to be… (more)

Subjects/Keywords: soot modeling; turbulent sooting flames; method of moments; partially-stirred reactor; aircraft combustor; Aerospace Engineering; Mechanical Engineering; Engineering

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APA (6th Edition):

Chong, S. T. (2018). Modeling of Turbulent Sooting Flames. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/147513

Chicago Manual of Style (16th Edition):

Chong, Shao Teng. “Modeling of Turbulent Sooting Flames.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/147513.

MLA Handbook (7th Edition):

Chong, Shao Teng. “Modeling of Turbulent Sooting Flames.” 2018. Web. 14 Apr 2021.

Vancouver:

Chong ST. Modeling of Turbulent Sooting Flames. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/147513.

Council of Science Editors:

Chong ST. Modeling of Turbulent Sooting Flames. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/147513


University of Michigan

9. Sato, Takuma. High-fidelity Simulations for Rotating Detonation Engines.

Degree: PhD, Aerospace Engineering, 2020, University of Michigan

 RDEs have drawn increased attention throughout the world as a viable technique for pressure gain combustion. An annular cylindrical combustor is used to drive a… (more)

Subjects/Keywords: Non-premixed detonations; Rotating detonation engines; Detailed kinetics; Aerospace Engineering; Engineering

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APA (6th Edition):

Sato, T. (2020). High-fidelity Simulations for Rotating Detonation Engines. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/163166

Chicago Manual of Style (16th Edition):

Sato, Takuma. “High-fidelity Simulations for Rotating Detonation Engines.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/163166.

MLA Handbook (7th Edition):

Sato, Takuma. “High-fidelity Simulations for Rotating Detonation Engines.” 2020. Web. 14 Apr 2021.

Vancouver:

Sato T. High-fidelity Simulations for Rotating Detonation Engines. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/163166.

Council of Science Editors:

Sato T. High-fidelity Simulations for Rotating Detonation Engines. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/163166


University of Michigan

10. Triantopoulos, Vasileios. Experimental and Computational Investigation of Spark Assisted Compression Ignition Combustion Under Boosted, Ultra EGR-Dilute Conditions.

Degree: PhD, Mechanical Engineering, 2018, University of Michigan

 Low temperature combustion (LTC) engines that employ high levels of dilution have received increased research interest due to the demonstrated thermal efficiency improvements compared to… (more)

Subjects/Keywords: engines; thermodynamics; energy; efficiency; automotive; power; Mechanical Engineering; Engineering

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APA (6th Edition):

Triantopoulos, V. (2018). Experimental and Computational Investigation of Spark Assisted Compression Ignition Combustion Under Boosted, Ultra EGR-Dilute Conditions. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/147508

Chicago Manual of Style (16th Edition):

Triantopoulos, Vasileios. “Experimental and Computational Investigation of Spark Assisted Compression Ignition Combustion Under Boosted, Ultra EGR-Dilute Conditions.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/147508.

MLA Handbook (7th Edition):

Triantopoulos, Vasileios. “Experimental and Computational Investigation of Spark Assisted Compression Ignition Combustion Under Boosted, Ultra EGR-Dilute Conditions.” 2018. Web. 14 Apr 2021.

Vancouver:

Triantopoulos V. Experimental and Computational Investigation of Spark Assisted Compression Ignition Combustion Under Boosted, Ultra EGR-Dilute Conditions. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/147508.

Council of Science Editors:

Triantopoulos V. Experimental and Computational Investigation of Spark Assisted Compression Ignition Combustion Under Boosted, Ultra EGR-Dilute Conditions. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/147508

11. Singh, Ripudaman. Enabling Ethanol Use as a Renewable Transportation Fuel: A Micro- and Macro-scale Perspective.

Degree: PhD, Mechanical Engineering, 2019, University of Michigan

 The transportation sector remains the most challenging area to reduce greenhouse gas emissions from the combustion of fossil fuels. A successful transition away from fossil… (more)

Subjects/Keywords: spark ignition engine; gasoline direct injection; cellulosic ethanol; thermodynamic efficiency; particulate emissions; Ghana; Mechanical Engineering; Engineering

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APA (6th Edition):

Singh, R. (2019). Enabling Ethanol Use as a Renewable Transportation Fuel: A Micro- and Macro-scale Perspective. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/149831

Chicago Manual of Style (16th Edition):

Singh, Ripudaman. “Enabling Ethanol Use as a Renewable Transportation Fuel: A Micro- and Macro-scale Perspective.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/149831.

MLA Handbook (7th Edition):

Singh, Ripudaman. “Enabling Ethanol Use as a Renewable Transportation Fuel: A Micro- and Macro-scale Perspective.” 2019. Web. 14 Apr 2021.

Vancouver:

Singh R. Enabling Ethanol Use as a Renewable Transportation Fuel: A Micro- and Macro-scale Perspective. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/149831.

Council of Science Editors:

Singh R. Enabling Ethanol Use as a Renewable Transportation Fuel: A Micro- and Macro-scale Perspective. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/149831

12. Neitzel, Kevin. Thermochemical Modeling of Nonequilibrium Oxygen Flows.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 The development of hypersonic vehicles leans heavily on computational simulation due to the high enthalpy flow conditions that are expensive and technically challenging to replicate… (more)

Subjects/Keywords: Hypersonics; Nonequilibrium; Oxygen; CFD; Aerospace Engineering; Engineering

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APA (6th Edition):

Neitzel, K. (2017). Thermochemical Modeling of Nonequilibrium Oxygen Flows. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/137049

Chicago Manual of Style (16th Edition):

Neitzel, Kevin. “Thermochemical Modeling of Nonequilibrium Oxygen Flows.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/137049.

MLA Handbook (7th Edition):

Neitzel, Kevin. “Thermochemical Modeling of Nonequilibrium Oxygen Flows.” 2017. Web. 14 Apr 2021.

Vancouver:

Neitzel K. Thermochemical Modeling of Nonequilibrium Oxygen Flows. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/137049.

Council of Science Editors:

Neitzel K. Thermochemical Modeling of Nonequilibrium Oxygen Flows. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/137049

13. Chen, YunTao. Investigation of Partially Premixed Combustion Instabilities through Experimental, Theoretical, and Computational Methods.

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

 Partially premixed combustion has the merits of lower emission as well as higher efficiency. However, its practical application has been hindered by its inherent instabilities.… (more)

Subjects/Keywords: Partially Premixed Combustion; Combustion Instability; Gas Turbine Engine; Planar Laser Induced Fluorescence; Flamelet/Progress Variable Model; Aerospace Engineering; Engineering

…introduced. Then previous measurements conducted both at DLR and at the University of Michigan are… 

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APA (6th Edition):

Chen, Y. (2015). Investigation of Partially Premixed Combustion Instabilities through Experimental, Theoretical, and Computational Methods. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/111342

Chicago Manual of Style (16th Edition):

Chen, YunTao. “Investigation of Partially Premixed Combustion Instabilities through Experimental, Theoretical, and Computational Methods.” 2015. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/111342.

MLA Handbook (7th Edition):

Chen, YunTao. “Investigation of Partially Premixed Combustion Instabilities through Experimental, Theoretical, and Computational Methods.” 2015. Web. 14 Apr 2021.

Vancouver:

Chen Y. Investigation of Partially Premixed Combustion Instabilities through Experimental, Theoretical, and Computational Methods. [Internet] [Doctoral dissertation]. University of Michigan; 2015. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/111342.

Council of Science Editors:

Chen Y. Investigation of Partially Premixed Combustion Instabilities through Experimental, Theoretical, and Computational Methods. [Doctoral Dissertation]. University of Michigan; 2015. Available from: http://hdl.handle.net/2027.42/111342

14. Allison, Patton Manuel. Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor.

Degree: PhD, Aerospace Engineering, 2013, University of Michigan

 Partially-premixed, swirl combustion is applied in gas turbine combustors to achieve flame stabilization and reduced emission production. However, this method is also inherently sensitive to… (more)

Subjects/Keywords: Combustion Instabilities; Laser Diagnostics; Aerospace Engineering; Engineering

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APA (6th Edition):

Allison, P. M. (2013). Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/102385

Chicago Manual of Style (16th Edition):

Allison, Patton Manuel. “Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor.” 2013. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/102385.

MLA Handbook (7th Edition):

Allison, Patton Manuel. “Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor.” 2013. Web. 14 Apr 2021.

Vancouver:

Allison PM. Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/102385.

Council of Science Editors:

Allison PM. Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/102385

15. Wabel, Timothy. An Experimental Investigation of Premixed Combustion in Extreme Turbulence.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 This work has explored various aspects of high Reynolds number combustion that have received much previous speculation. A new high-Reynolds number premixed Bunsen burner, called… (more)

Subjects/Keywords: Turbulent Combustion; Turbulent Flows; Aerospace Engineering; Mechanical Engineering; Chemistry; Physics; Science (General); Engineering; Science

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APA (6th Edition):

Wabel, T. (2017). An Experimental Investigation of Premixed Combustion in Extreme Turbulence. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/137086

Chicago Manual of Style (16th Edition):

Wabel, Timothy. “An Experimental Investigation of Premixed Combustion in Extreme Turbulence.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/137086.

MLA Handbook (7th Edition):

Wabel, Timothy. “An Experimental Investigation of Premixed Combustion in Extreme Turbulence.” 2017. Web. 14 Apr 2021.

Vancouver:

Wabel T. An Experimental Investigation of Premixed Combustion in Extreme Turbulence. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/137086.

Council of Science Editors:

Wabel T. An Experimental Investigation of Premixed Combustion in Extreme Turbulence. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/137086

16. Rosenberg, David Ari. A Method to Measure Flame Index in Turbulent Partially-Premixed Flames.

Degree: PhD, Aerospace Engineering, 2014, University of Michigan

 This dissertation describes the development of a diagnostic technique and data processing routine to measure the flame index in partially-premixed flames, called the Flame Index… (more)

Subjects/Keywords: Flame Index; PLIF; Turbulent Combustion; Gas Turbine; Partially-Premixed Combustion; Planar Laser-induced Fluorescence; Aerospace Engineering; Engineering

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APA (6th Edition):

Rosenberg, D. A. (2014). A Method to Measure Flame Index in Turbulent Partially-Premixed Flames. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/107298

Chicago Manual of Style (16th Edition):

Rosenberg, David Ari. “A Method to Measure Flame Index in Turbulent Partially-Premixed Flames.” 2014. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/107298.

MLA Handbook (7th Edition):

Rosenberg, David Ari. “A Method to Measure Flame Index in Turbulent Partially-Premixed Flames.” 2014. Web. 14 Apr 2021.

Vancouver:

Rosenberg DA. A Method to Measure Flame Index in Turbulent Partially-Premixed Flames. [Internet] [Doctoral dissertation]. University of Michigan; 2014. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/107298.

Council of Science Editors:

Rosenberg DA. A Method to Measure Flame Index in Turbulent Partially-Premixed Flames. [Doctoral Dissertation]. University of Michigan; 2014. Available from: http://hdl.handle.net/2027.42/107298

17. Hunt, Robin. Shock Train Structure and Dynamics.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 The structure and dynamics of a shock train are studied experimentally using a direct-connect isolator model with a nominal inflow Mach number of 2.0. The… (more)

Subjects/Keywords: shock train; pseudoshock; unsteady shock dynamics; Aerospace Engineering; Engineering

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APA (6th Edition):

Hunt, R. (2018). Shock Train Structure and Dynamics. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/143988

Chicago Manual of Style (16th Edition):

Hunt, Robin. “Shock Train Structure and Dynamics.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/143988.

MLA Handbook (7th Edition):

Hunt, Robin. “Shock Train Structure and Dynamics.” 2018. Web. 14 Apr 2021.

Vancouver:

Hunt R. Shock Train Structure and Dynamics. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/143988.

Council of Science Editors:

Hunt R. Shock Train Structure and Dynamics. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/143988

18. Kwak, Kyoung Hyun. Fuel Sensitive Combustion Model Based On Quasi-Dimensional Multi-Zone Approach For Direct Injection Compression Ignition Engines.

Degree: PhD, Mechanical Engineering, 2014, University of Michigan

 This study describes a development of fuel sensitive quasi-dimensional multi-zone model for a direct injection compression ignition (DICI) engine. The objective is to develop fuel… (more)

Subjects/Keywords: Diesel Engine; Quasi-dimensional Multi-zone Simulation; Alternative Fuels; Ignition Delay; Multi-component Evaporation; Spray Model; Mechanical Engineering; Engineering

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

APA (6th Edition):

Kwak, K. H. (2014). Fuel Sensitive Combustion Model Based On Quasi-Dimensional Multi-Zone Approach For Direct Injection Compression Ignition Engines. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/108990

Chicago Manual of Style (16th Edition):

Kwak, Kyoung Hyun. “Fuel Sensitive Combustion Model Based On Quasi-Dimensional Multi-Zone Approach For Direct Injection Compression Ignition Engines.” 2014. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/108990.

MLA Handbook (7th Edition):

Kwak, Kyoung Hyun. “Fuel Sensitive Combustion Model Based On Quasi-Dimensional Multi-Zone Approach For Direct Injection Compression Ignition Engines.” 2014. Web. 14 Apr 2021.

Vancouver:

Kwak KH. Fuel Sensitive Combustion Model Based On Quasi-Dimensional Multi-Zone Approach For Direct Injection Compression Ignition Engines. [Internet] [Doctoral dissertation]. University of Michigan; 2014. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/108990.

Council of Science Editors:

Kwak KH. Fuel Sensitive Combustion Model Based On Quasi-Dimensional Multi-Zone Approach For Direct Injection Compression Ignition Engines. [Doctoral Dissertation]. University of Michigan; 2014. Available from: http://hdl.handle.net/2027.42/108990

19. Abul-Huda, Yasin. A Study of Combustion Augmentation in Supersonic Flows via a Pulsed-Detonation Device.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 Robust ignition and stable flame holding are challenging feats in scramjet combustors because of their susceptibility to large variations in flow, pressure, temperature, and composition.… (more)

Subjects/Keywords: supersonic combustion; detonation; expansion tube; combustion enhancement; scramjet; hypersonic supersonic; Aerospace Engineering; Engineering

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

APA (6th Edition):

Abul-Huda, Y. (2017). A Study of Combustion Augmentation in Supersonic Flows via a Pulsed-Detonation Device. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/140793

Chicago Manual of Style (16th Edition):

Abul-Huda, Yasin. “A Study of Combustion Augmentation in Supersonic Flows via a Pulsed-Detonation Device.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/140793.

MLA Handbook (7th Edition):

Abul-Huda, Yasin. “A Study of Combustion Augmentation in Supersonic Flows via a Pulsed-Detonation Device.” 2017. Web. 14 Apr 2021.

Vancouver:

Abul-Huda Y. A Study of Combustion Augmentation in Supersonic Flows via a Pulsed-Detonation Device. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/140793.

Council of Science Editors:

Abul-Huda Y. A Study of Combustion Augmentation in Supersonic Flows via a Pulsed-Detonation Device. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/140793

20. Morajkar, Rohan. Role of Secondary Flows on Flow Separation Induced by Shock/boundary-layer Interaction in Supersonic Inlets.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 Flow separation in the scramjet air intakes is one of the reasons of failure of these engines which rely on shock waves to achieve flow… (more)

Subjects/Keywords: Shock wave Boundary Layer Interaction; Aerospace Engineering; Engineering (General); Science (General); Engineering; Science

…control of supersonic inlets. The study is conducted at the University of Michigan Glass… 

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

APA (6th Edition):

Morajkar, R. (2017). Role of Secondary Flows on Flow Separation Induced by Shock/boundary-layer Interaction in Supersonic Inlets. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/137080

Chicago Manual of Style (16th Edition):

Morajkar, Rohan. “Role of Secondary Flows on Flow Separation Induced by Shock/boundary-layer Interaction in Supersonic Inlets.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/137080.

MLA Handbook (7th Edition):

Morajkar, Rohan. “Role of Secondary Flows on Flow Separation Induced by Shock/boundary-layer Interaction in Supersonic Inlets.” 2017. Web. 14 Apr 2021.

Vancouver:

Morajkar R. Role of Secondary Flows on Flow Separation Induced by Shock/boundary-layer Interaction in Supersonic Inlets. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/137080.

Council of Science Editors:

Morajkar R. Role of Secondary Flows on Flow Separation Induced by Shock/boundary-layer Interaction in Supersonic Inlets. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/137080

21. Kim, Doohyun. Conventional and Alternative Jet Fuels for Diesel Combustion: Surrogate Development and Insights into the Effect of Fuel Properties on Ignition.

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

 The use of kerosene-based jet fuels for all military applications has been mandated by U.S. military’s single fuel forward concept. Recently, interest in non-petroleum-derived alternative… (more)

Subjects/Keywords: fuel surrogate development; diesel combustion; Mechanical Engineering; Engineering

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

APA (6th Edition):

Kim, D. (2016). Conventional and Alternative Jet Fuels for Diesel Combustion: Surrogate Development and Insights into the Effect of Fuel Properties on Ignition. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/120818

Chicago Manual of Style (16th Edition):

Kim, Doohyun. “Conventional and Alternative Jet Fuels for Diesel Combustion: Surrogate Development and Insights into the Effect of Fuel Properties on Ignition.” 2016. Doctoral Dissertation, University of Michigan. Accessed April 14, 2021. http://hdl.handle.net/2027.42/120818.

MLA Handbook (7th Edition):

Kim, Doohyun. “Conventional and Alternative Jet Fuels for Diesel Combustion: Surrogate Development and Insights into the Effect of Fuel Properties on Ignition.” 2016. Web. 14 Apr 2021.

Vancouver:

Kim D. Conventional and Alternative Jet Fuels for Diesel Combustion: Surrogate Development and Insights into the Effect of Fuel Properties on Ignition. [Internet] [Doctoral dissertation]. University of Michigan; 2016. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/2027.42/120818.

Council of Science Editors:

Kim D. Conventional and Alternative Jet Fuels for Diesel Combustion: Surrogate Development and Insights into the Effect of Fuel Properties on Ignition. [Doctoral Dissertation]. University of Michigan; 2016. Available from: http://hdl.handle.net/2027.42/120818

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