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You searched for +publisher:"The Ohio State University" +contributor:("Gaitonde, Datta"). Showing records 1 – 14 of 14 total matches.

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The Ohio State University

1. Sasidharan Nair, Unnikrishnan. Jet noise source localization and identification.

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

 The exact mechanism by which turbulent fluctuations in jets areconverted into acoustic energy remains unexplained. The current workaims to improve our understanding of this problem… (more)

Subjects/Keywords: Aerospace Engineering; Mechanical Engineering; Jet noise, Aeroacoustics, Large-eddy simulation, Acoustic wavepacket

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APA (6th Edition):

Sasidharan Nair, U. (2017). Jet noise source localization and identification. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1482412964456451

Chicago Manual of Style (16th Edition):

Sasidharan Nair, Unnikrishnan. “Jet noise source localization and identification.” 2017. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1482412964456451.

MLA Handbook (7th Edition):

Sasidharan Nair, Unnikrishnan. “Jet noise source localization and identification.” 2017. Web. 23 Oct 2019.

Vancouver:

Sasidharan Nair U. Jet noise source localization and identification. [Internet] [Doctoral dissertation]. The Ohio State University; 2017. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1482412964456451.

Council of Science Editors:

Sasidharan Nair U. Jet noise source localization and identification. [Doctoral Dissertation]. The Ohio State University; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1482412964456451


The Ohio State University

2. Yentsch, Robert J. Three-Dimensional Shock-Boundary Layer Interactions in Simulations of HIFiRE-1 and HIFiRE-2.

Degree: PhD, Mechanical Engineering, 2013, The Ohio State University

 A series of high-fidelity, three-dimensional simulations has been performed to investigate hypersonic phenomena encountered in the HIFiRE Flight 1 and Flight 2 experiments. The investigation… (more)

Subjects/Keywords: Aerospace Engineering; HIFiRE; mode-transition; mode transition; scramjet, hypersonic airbreathing propulsion; shock boundary layer interactions; computational fluid dynamics; CFD; RANS; dual-mode; scramjet-mode

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APA (6th Edition):

Yentsch, R. J. (2013). Three-Dimensional Shock-Boundary Layer Interactions in Simulations of HIFiRE-1 and HIFiRE-2. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1384195671

Chicago Manual of Style (16th Edition):

Yentsch, Robert J. “Three-Dimensional Shock-Boundary Layer Interactions in Simulations of HIFiRE-1 and HIFiRE-2.” 2013. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1384195671.

MLA Handbook (7th Edition):

Yentsch, Robert J. “Three-Dimensional Shock-Boundary Layer Interactions in Simulations of HIFiRE-1 and HIFiRE-2.” 2013. Web. 23 Oct 2019.

Vancouver:

Yentsch RJ. Three-Dimensional Shock-Boundary Layer Interactions in Simulations of HIFiRE-1 and HIFiRE-2. [Internet] [Doctoral dissertation]. The Ohio State University; 2013. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1384195671.

Council of Science Editors:

Yentsch RJ. Three-Dimensional Shock-Boundary Layer Interactions in Simulations of HIFiRE-1 and HIFiRE-2. [Doctoral Dissertation]. The Ohio State University; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1384195671


The Ohio State University

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Goparaju, Kalyan. “Flow and Acoustic Characteristics of Complex Supersonic Jets.” 2017. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1510933315034965.

MLA Handbook (7th Edition):

Goparaju, Kalyan. “Flow and Acoustic Characteristics of Complex Supersonic Jets.” 2017. Web. 23 Oct 2019.

Vancouver:

Goparaju K. Flow and Acoustic Characteristics of Complex Supersonic Jets. [Internet] [Doctoral dissertation]. The Ohio State University; 2017. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1510933315034965.

Council of Science Editors:

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


The Ohio State University

4. Waindim, Mbu. On Unsteadiness in 2-D and 3-D Shock Wave/Turbulent Boundary Layer Interactions.

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

 Shock-boundary layer interactions (SBLIs) are ubiquitous occurrences in supersonic andhypersonic vehicles and have the tendency to inhibit their structural and aerodynamic performance.For example, in the… (more)

Subjects/Keywords: Aerospace Engineering; Fluid Dynamics; shock waves; fluid dynamics; turbulence; boundary layers; computational fluid dynamics; CFD; unsteadiness; SBLI; dynamic mode decomposition; DMD; empirical mode decomposition; EMD; stability analysis

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APA (6th Edition):

Waindim, M. (2017). On Unsteadiness in 2-D and 3-D Shock Wave/Turbulent Boundary Layer Interactions. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1511734224701396

Chicago Manual of Style (16th Edition):

Waindim, Mbu. “On Unsteadiness in 2-D and 3-D Shock Wave/Turbulent Boundary Layer Interactions.” 2017. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1511734224701396.

MLA Handbook (7th Edition):

Waindim, Mbu. “On Unsteadiness in 2-D and 3-D Shock Wave/Turbulent Boundary Layer Interactions.” 2017. Web. 23 Oct 2019.

Vancouver:

Waindim M. On Unsteadiness in 2-D and 3-D Shock Wave/Turbulent Boundary Layer Interactions. [Internet] [Doctoral dissertation]. The Ohio State University; 2017. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1511734224701396.

Council of Science Editors:

Waindim M. On Unsteadiness in 2-D and 3-D Shock Wave/Turbulent Boundary Layer Interactions. [Doctoral Dissertation]. The Ohio State University; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1511734224701396


The Ohio State University

5. Mohan, Arvind Thanam. Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations.

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

 Numerical methods and computational approaches for studying fluid flow have become increasingly popular and more mature in their capabilities since the 1960s, when the prohibitive… (more)

Subjects/Keywords: Aerospace Engineering; CFD; aerodynamics; turbulence; DMD; EMD; Multivariate EMD; Matching Pursuits; Statistics; Wavelets; MAV; UAV

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APA (6th Edition):

Mohan, A. T. (2017). Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368

Chicago Manual of Style (16th Edition):

Mohan, Arvind Thanam. “Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations.” 2017. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368.

MLA Handbook (7th Edition):

Mohan, Arvind Thanam. “Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations.” 2017. Web. 23 Oct 2019.

Vancouver:

Mohan AT. Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations. [Internet] [Doctoral dissertation]. The Ohio State University; 2017. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368.

Council of Science Editors:

Mohan AT. Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations. [Doctoral Dissertation]. The Ohio State University; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368


The Ohio State University

6. Speth, Rachelle Lea. Controlling The Development of Coherent Structures in High Speed Jets and The Resultant Near Field.

Degree: PhD, Aero/Astro Engineering, 2015, The Ohio State University

 This work uses Large-Eddy Simulations to examine the effect of actuator parameters and jet exit properties on the evolution of coherent structures and their impact… (more)

Subjects/Keywords: Acoustics; Aerospace Engineering; acoustics; large eddy simulation; jets; plasma control

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APA (6th Edition):

Speth, R. L. (2015). Controlling The Development of Coherent Structures in High Speed Jets and The Resultant Near Field. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1447419083

Chicago Manual of Style (16th Edition):

Speth, Rachelle Lea. “Controlling The Development of Coherent Structures in High Speed Jets and The Resultant Near Field.” 2015. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1447419083.

MLA Handbook (7th Edition):

Speth, Rachelle Lea. “Controlling The Development of Coherent Structures in High Speed Jets and The Resultant Near Field.” 2015. Web. 23 Oct 2019.

Vancouver:

Speth RL. Controlling The Development of Coherent Structures in High Speed Jets and The Resultant Near Field. [Internet] [Doctoral dissertation]. The Ohio State University; 2015. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1447419083.

Council of Science Editors:

Speth RL. Controlling The Development of Coherent Structures in High Speed Jets and The Resultant Near Field. [Doctoral Dissertation]. The Ohio State University; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1447419083


The Ohio State University

7. Gonzalez, David R. Development of a Semi-Lagrangian Methodology for Jet Aeroacoustics Analysis.

Degree: PhD, Aero/Astro Engineering, 2016, The Ohio State University

 A novel analysis technique is developed for the time-accurate analysis of noise sources in compressible jet flows. By adopting a Lagrangian point of view, the… (more)

Subjects/Keywords: Aerospace Engineering; Jet noise, finite-time Lypaunov exponents, Lagrangian dynamics, computational fluid dynamics

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APA (6th Edition):

Gonzalez, D. R. (2016). Development of a Semi-Lagrangian Methodology for Jet Aeroacoustics Analysis. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1467201142

Chicago Manual of Style (16th Edition):

Gonzalez, David R. “Development of a Semi-Lagrangian Methodology for Jet Aeroacoustics Analysis.” 2016. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1467201142.

MLA Handbook (7th Edition):

Gonzalez, David R. “Development of a Semi-Lagrangian Methodology for Jet Aeroacoustics Analysis.” 2016. Web. 23 Oct 2019.

Vancouver:

Gonzalez DR. Development of a Semi-Lagrangian Methodology for Jet Aeroacoustics Analysis. [Internet] [Doctoral dissertation]. The Ohio State University; 2016. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1467201142.

Council of Science Editors:

Gonzalez DR. Development of a Semi-Lagrangian Methodology for Jet Aeroacoustics Analysis. [Doctoral Dissertation]. The Ohio State University; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1467201142


The Ohio State University

8. Adler, Michael C. On the Advancement of Phenomenological and Mechanistic Descriptions of Unsteadiness in Shock-Wave/Turbulent-Boundary-Layer Interactions.

Degree: PhD, Aero/Astro Engineering, 2019, The Ohio State University

 Recent experimental and computational investigations have provided a comprehensive phenomenological description of unsteadiness in nominally two-dimensional (2-D), spanwise homogeneous shock-wave/turbulent-boundary-layer interactions (STBLIs), including both the… (more)

Subjects/Keywords: Aerospace Engineering; shock; shock wave; turbulence; turbulent boundary layer; SBLI; shock unsteadiness; flow separation; compressible flow; unsteady aerodynamics; Lyapunov exponent; linear stability; absolute instability; convective instability; large-eddy simulation; LES

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APA (6th Edition):

Adler, M. C. (2019). On the Advancement of Phenomenological and Mechanistic Descriptions of Unsteadiness in Shock-Wave/Turbulent-Boundary-Layer Interactions. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1553543774661509

Chicago Manual of Style (16th Edition):

Adler, Michael C. “On the Advancement of Phenomenological and Mechanistic Descriptions of Unsteadiness in Shock-Wave/Turbulent-Boundary-Layer Interactions.” 2019. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1553543774661509.

MLA Handbook (7th Edition):

Adler, Michael C. “On the Advancement of Phenomenological and Mechanistic Descriptions of Unsteadiness in Shock-Wave/Turbulent-Boundary-Layer Interactions.” 2019. Web. 23 Oct 2019.

Vancouver:

Adler MC. On the Advancement of Phenomenological and Mechanistic Descriptions of Unsteadiness in Shock-Wave/Turbulent-Boundary-Layer Interactions. [Internet] [Doctoral dissertation]. The Ohio State University; 2019. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1553543774661509.

Council of Science Editors:

Adler MC. On the Advancement of Phenomenological and Mechanistic Descriptions of Unsteadiness in Shock-Wave/Turbulent-Boundary-Layer Interactions. [Doctoral Dissertation]. The Ohio State University; 2019. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1553543774661509


The Ohio State University

9. Stack, Cory M. Turbulence Mechanisms in a Supersonic Rectangular Multistream Jet with an Aft-Deck.

Degree: PhD, Aero/Astro Engineering, 2019, The Ohio State University

 Over the last 80 years, high-performance military aircraft have relied on increasingly sophisticated jet engine technologies to enable performance and fulfill mission requirements. To satisfy… (more)

Subjects/Keywords: Aerospace Engineering; supersonic, multistream, airframe-integrated, jet, nozzle, aft-deck, rectangular, unsteady, Large-Eddy Simulations

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APA (6th Edition):

Stack, C. M. (2019). Turbulence Mechanisms in a Supersonic Rectangular Multistream Jet with an Aft-Deck. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1560352886647369

Chicago Manual of Style (16th Edition):

Stack, Cory M. “Turbulence Mechanisms in a Supersonic Rectangular Multistream Jet with an Aft-Deck.” 2019. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1560352886647369.

MLA Handbook (7th Edition):

Stack, Cory M. “Turbulence Mechanisms in a Supersonic Rectangular Multistream Jet with an Aft-Deck.” 2019. Web. 23 Oct 2019.

Vancouver:

Stack CM. Turbulence Mechanisms in a Supersonic Rectangular Multistream Jet with an Aft-Deck. [Internet] [Doctoral dissertation]. The Ohio State University; 2019. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1560352886647369.

Council of Science Editors:

Stack CM. Turbulence Mechanisms in a Supersonic Rectangular Multistream Jet with an Aft-Deck. [Doctoral Dissertation]. The Ohio State University; 2019. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1560352886647369

10. Sengupta, Soumyo, Sengupta. Investigation of Flow Dynamics of a SubsonicCircular to Rectangular Jet.

Degree: MS, Mechanical Engineering, 2016, The Ohio State University

 Large Eddy Simulation based investigation is performed on a circular to rectangular Mach 0.226 jet to understand the effect of the non-axisymmetric geometryon the jet… (more)

Subjects/Keywords: Mechanical Engineering; Rectangular Nozzle, Subsonic, LES, Jet Flow, entrainment

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APA (6th Edition):

Sengupta, Soumyo, S. (2016). Investigation of Flow Dynamics of a SubsonicCircular to Rectangular Jet. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1467990955

Chicago Manual of Style (16th Edition):

Sengupta, Soumyo, Sengupta. “Investigation of Flow Dynamics of a SubsonicCircular to Rectangular Jet.” 2016. Masters Thesis, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1467990955.

MLA Handbook (7th Edition):

Sengupta, Soumyo, Sengupta. “Investigation of Flow Dynamics of a SubsonicCircular to Rectangular Jet.” 2016. Web. 23 Oct 2019.

Vancouver:

Sengupta, Soumyo S. Investigation of Flow Dynamics of a SubsonicCircular to Rectangular Jet. [Internet] [Masters thesis]. The Ohio State University; 2016. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1467990955.

Council of Science Editors:

Sengupta, Soumyo S. Investigation of Flow Dynamics of a SubsonicCircular to Rectangular Jet. [Masters Thesis]. The Ohio State University; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1467990955

11. Mustafa, Mansoor. Investigation into Offset Streams for Jet Noise Reduction.

Degree: MS, Aero/Astro Engineering, 2015, The Ohio State University

 This effort investigates the near field behavior of two ideally-expanded subsonic dual-stream jets. One case implements a traditional symmetric, concentric dual-stream nozzle configuration while the… (more)

Subjects/Keywords: Aerospace Engineering; offset; noise reduction; jets; aerospace; aerodynamics; LES; computational simulation; jet noise; eccentric; concentric; dual-stream; nozzle

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APA (6th Edition):

Mustafa, M. (2015). Investigation into Offset Streams for Jet Noise Reduction. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1437477139

Chicago Manual of Style (16th Edition):

Mustafa, Mansoor. “Investigation into Offset Streams for Jet Noise Reduction.” 2015. Masters Thesis, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1437477139.

MLA Handbook (7th Edition):

Mustafa, Mansoor. “Investigation into Offset Streams for Jet Noise Reduction.” 2015. Web. 23 Oct 2019.

Vancouver:

Mustafa M. Investigation into Offset Streams for Jet Noise Reduction. [Internet] [Masters thesis]. The Ohio State University; 2015. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1437477139.

Council of Science Editors:

Mustafa M. Investigation into Offset Streams for Jet Noise Reduction. [Masters Thesis]. The Ohio State University; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1437477139

12. Speth, Rachelle Lea. Parametric Study of the Effects of the Flapping Mode Excitation on the Near Field Structures of a Mach 1.3 Cold Jet.

Degree: MS, Aero/Astro Engineering, 2012, The Ohio State University

 This effort investigates numerical and physical parameters influencing an ideally-expanded Mach 1.3 jet excited by the m=+/-1 flapping mode. The excitation is imposed by eight… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; Mechanical Engineering; supersonic jets; Large Eddy Simulation; plasma actuators

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APA (6th Edition):

Speth, R. L. (2012). Parametric Study of the Effects of the Flapping Mode Excitation on the Near Field Structures of a Mach 1.3 Cold Jet. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1338049511

Chicago Manual of Style (16th Edition):

Speth, Rachelle Lea. “Parametric Study of the Effects of the Flapping Mode Excitation on the Near Field Structures of a Mach 1.3 Cold Jet.” 2012. Masters Thesis, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1338049511.

MLA Handbook (7th Edition):

Speth, Rachelle Lea. “Parametric Study of the Effects of the Flapping Mode Excitation on the Near Field Structures of a Mach 1.3 Cold Jet.” 2012. Web. 23 Oct 2019.

Vancouver:

Speth RL. Parametric Study of the Effects of the Flapping Mode Excitation on the Near Field Structures of a Mach 1.3 Cold Jet. [Internet] [Masters thesis]. The Ohio State University; 2012. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1338049511.

Council of Science Editors:

Speth RL. Parametric Study of the Effects of the Flapping Mode Excitation on the Near Field Structures of a Mach 1.3 Cold Jet. [Masters Thesis]. The Ohio State University; 2012. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1338049511

13. Riley, Logan Patrick. Unstart Phenomenology of a Dual-Mode Scramjet Subject to Time-Varying Fuel Input.

Degree: PhD, Aeronautical and Astronautical Engineering, 2019, The Ohio State University

 Scramjet-based, air-breathing propulsion systems are poised to enable development of hypersonic defense, high speed transport, and access-to-space aerospace vehicles. A particular variant of scramjet engine,… (more)

Subjects/Keywords: Aerospace Engineering; scramjet; URANS; hypersonic; unstart; ethylene; SBLI; isolator; POD; DMD

…Fellowship from The Ohio State University Graduate School which provided support during my final… …Began Graduate studies, The Ohio State University Columbus, OH August 2014-February 2017… 

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APA (6th Edition):

Riley, L. P. (2019). Unstart Phenomenology of a Dual-Mode Scramjet Subject to Time-Varying Fuel Input. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1554740828968894

Chicago Manual of Style (16th Edition):

Riley, Logan Patrick. “Unstart Phenomenology of a Dual-Mode Scramjet Subject to Time-Varying Fuel Input.” 2019. Doctoral Dissertation, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1554740828968894.

MLA Handbook (7th Edition):

Riley, Logan Patrick. “Unstart Phenomenology of a Dual-Mode Scramjet Subject to Time-Varying Fuel Input.” 2019. Web. 23 Oct 2019.

Vancouver:

Riley LP. Unstart Phenomenology of a Dual-Mode Scramjet Subject to Time-Varying Fuel Input. [Internet] [Doctoral dissertation]. The Ohio State University; 2019. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1554740828968894.

Council of Science Editors:

Riley LP. Unstart Phenomenology of a Dual-Mode Scramjet Subject to Time-Varying Fuel Input. [Doctoral Dissertation]. The Ohio State University; 2019. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1554740828968894

14. Mohan, Arvind Thanam. Large Eddy Simulationof Separated Flows.

Degree: MS, Aero/Astro Engineering, 2013, The Ohio State University

 In the past few decades, Large eddy simulation has seen a surge in interest from theCFD community owing to its inherent advantages in terms of… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; Fluid Dynamics; Applied Mathematics; Mechanical Engineering; Statistics; CFD; LES; Turbulence Modeling; Statistics; Fluids

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APA (6th Edition):

Mohan, A. T. (2013). Large Eddy Simulationof Separated Flows. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1367493651

Chicago Manual of Style (16th Edition):

Mohan, Arvind Thanam. “Large Eddy Simulationof Separated Flows.” 2013. Masters Thesis, The Ohio State University. Accessed October 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1367493651.

MLA Handbook (7th Edition):

Mohan, Arvind Thanam. “Large Eddy Simulationof Separated Flows.” 2013. Web. 23 Oct 2019.

Vancouver:

Mohan AT. Large Eddy Simulationof Separated Flows. [Internet] [Masters thesis]. The Ohio State University; 2013. [cited 2019 Oct 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1367493651.

Council of Science Editors:

Mohan AT. Large Eddy Simulationof Separated Flows. [Masters Thesis]. The Ohio State University; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1367493651

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