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You searched for subject:(supersonic). Showing records 1 – 30 of 514 total matches.

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Texas A&M University

1. Sheffield, Les. Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams.

Degree: PhD, Physics, 2015, Texas A&M University

 In this thesis I describe the second generation of a rotating supersonic beam source. The purpose of this device is to produce velocity augmented molecular… (more)

Subjects/Keywords: Supersonic Velocity

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APA (6th Edition):

Sheffield, L. (2015). Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154986

Chicago Manual of Style (16th Edition):

Sheffield, Les. “Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams.” 2015. Doctoral Dissertation, Texas A&M University. Accessed January 18, 2021. http://hdl.handle.net/1969.1/154986.

MLA Handbook (7th Edition):

Sheffield, Les. “Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams.” 2015. Web. 18 Jan 2021.

Vancouver:

Sheffield L. Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams. [Internet] [Doctoral dissertation]. Texas A&M University; 2015. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1969.1/154986.

Council of Science Editors:

Sheffield L. Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams. [Doctoral Dissertation]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/154986


Rutgers University

2. Pizzaia, Adam R., 1989-. Side view and end view mixing measurements of a sonic transverse jet in a supersonic crossflow.

Degree: MS, Mechanical and Aerospace Engineering, 2014, Rutgers University

 The primary investigation was to determine if mixing of a sonic transverse jet in the side-view plane was correlated to or equal to the mixing… (more)

Subjects/Keywords: Airplanes – Scramjet engines; Aerodynamics, Supersonic; Supersonic planes

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APA (6th Edition):

Pizzaia, Adam R., 1. (2014). Side view and end view mixing measurements of a sonic transverse jet in a supersonic crossflow. (Masters Thesis). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/44199/

Chicago Manual of Style (16th Edition):

Pizzaia, Adam R., 1989-. “Side view and end view mixing measurements of a sonic transverse jet in a supersonic crossflow.” 2014. Masters Thesis, Rutgers University. Accessed January 18, 2021. https://rucore.libraries.rutgers.edu/rutgers-lib/44199/.

MLA Handbook (7th Edition):

Pizzaia, Adam R., 1989-. “Side view and end view mixing measurements of a sonic transverse jet in a supersonic crossflow.” 2014. Web. 18 Jan 2021.

Vancouver:

Pizzaia, Adam R. 1. Side view and end view mixing measurements of a sonic transverse jet in a supersonic crossflow. [Internet] [Masters thesis]. Rutgers University; 2014. [cited 2021 Jan 18]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/44199/.

Council of Science Editors:

Pizzaia, Adam R. 1. Side view and end view mixing measurements of a sonic transverse jet in a supersonic crossflow. [Masters Thesis]. Rutgers University; 2014. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/44199/


Georgia Tech

3. Blette, David Joseph. Supersonic descent staging aerodynamic and performance analysis.

Degree: PhD, Aerospace Engineering, 2020, Georgia Tech

Supersonic Retropropulsion (SRP) is one potential enabling technology to extend Mars entry, descent, and landing (EDL) capability beyond current Viking-era technological landed mass upper limits… (more)

Subjects/Keywords: Supersonic retropropulsion; Supersonic descent vehicle staging; Supersonic descent vehicle reconfigurations; Human Mars; Supersonic vehicle reconfiguration

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APA (6th Edition):

Blette, D. J. (2020). Supersonic descent staging aerodynamic and performance analysis. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62713

Chicago Manual of Style (16th Edition):

Blette, David Joseph. “Supersonic descent staging aerodynamic and performance analysis.” 2020. Doctoral Dissertation, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/62713.

MLA Handbook (7th Edition):

Blette, David Joseph. “Supersonic descent staging aerodynamic and performance analysis.” 2020. Web. 18 Jan 2021.

Vancouver:

Blette DJ. Supersonic descent staging aerodynamic and performance analysis. [Internet] [Doctoral dissertation]. Georgia Tech; 2020. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/62713.

Council of Science Editors:

Blette DJ. Supersonic descent staging aerodynamic and performance analysis. [Doctoral Dissertation]. Georgia Tech; 2020. Available from: http://hdl.handle.net/1853/62713


University of New South Wales

4. Sridhar, Vikram. Computational and Experimental Investigation of Supersonic Two-dimensional and Axi-symmetric Shallow Open Cavities.

Degree: Engineering & Information Technology Canberra, 2014, University of New South Wales

 Time-accurate numerical simulations and experiments were carried out on two-dimensional/planar and axi-symmetric open cavities with length-to-depth ratios of 3, 5, 6 and 8 in a… (more)

Subjects/Keywords: turbulent; Supersonic; Cavity

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APA (6th Edition):

Sridhar, V. (2014). Computational and Experimental Investigation of Supersonic Two-dimensional and Axi-symmetric Shallow Open Cavities. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/53981 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12692/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Sridhar, Vikram. “Computational and Experimental Investigation of Supersonic Two-dimensional and Axi-symmetric Shallow Open Cavities.” 2014. Doctoral Dissertation, University of New South Wales. Accessed January 18, 2021. http://handle.unsw.edu.au/1959.4/53981 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12692/SOURCE02?view=true.

MLA Handbook (7th Edition):

Sridhar, Vikram. “Computational and Experimental Investigation of Supersonic Two-dimensional and Axi-symmetric Shallow Open Cavities.” 2014. Web. 18 Jan 2021.

Vancouver:

Sridhar V. Computational and Experimental Investigation of Supersonic Two-dimensional and Axi-symmetric Shallow Open Cavities. [Internet] [Doctoral dissertation]. University of New South Wales; 2014. [cited 2021 Jan 18]. Available from: http://handle.unsw.edu.au/1959.4/53981 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12692/SOURCE02?view=true.

Council of Science Editors:

Sridhar V. Computational and Experimental Investigation of Supersonic Two-dimensional and Axi-symmetric Shallow Open Cavities. [Doctoral Dissertation]. University of New South Wales; 2014. Available from: http://handle.unsw.edu.au/1959.4/53981 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12692/SOURCE02?view=true


Indian Institute of Science

5. Srisha Rao, M V. Experimental Investigations on Supersonic Ejectors.

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

 A supersonic ejector is used to pump a secondary gas using a supersonic primary gas flow by augmentation of momentum and energy in a variable… (more)

Subjects/Keywords: Supersonic Aerodynamics; Supersonic Ejector; Supersonic Ejector Test Rig; Supersonic Nozzles; Two-dimensional Supersonic Ejectors; Axisymmetric Supersonic Ejectors; Supersonic Ejector Flow; Supersonic Ejectors - Flow Dynamics; Flow Visualization; Nozzles - Flow Dynamics; Shock Oscillations; Supersonic Gaseous Ejector; Supersonic Hydrogen Ejector; Aerospace Engineering

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APA (6th Edition):

Srisha Rao, M. V. (2018). Experimental Investigations on Supersonic Ejectors. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3402

Chicago Manual of Style (16th Edition):

Srisha Rao, M V. “Experimental Investigations on Supersonic Ejectors.” 2018. Doctoral Dissertation, Indian Institute of Science. Accessed January 18, 2021. http://etd.iisc.ac.in/handle/2005/3402.

MLA Handbook (7th Edition):

Srisha Rao, M V. “Experimental Investigations on Supersonic Ejectors.” 2018. Web. 18 Jan 2021.

Vancouver:

Srisha Rao MV. Experimental Investigations on Supersonic Ejectors. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2018. [cited 2021 Jan 18]. Available from: http://etd.iisc.ac.in/handle/2005/3402.

Council of Science Editors:

Srisha Rao MV. Experimental Investigations on Supersonic Ejectors. [Doctoral Dissertation]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3402


Mississippi State University

6. Ratliff, West Cardman. REVITALIZATION AND INITIAL TESTING OF A BLOWDOWN SUPERSONIC WIND TUNNEL.

Degree: MS, Aerospace Engineering, 2008, Mississippi State University

 The Supersonic tunnel located in Patterson Labs at Mississippi State University has been thoroughly documented for future reference purposes. Data acquisition, physical components, shutdown devices,… (more)

Subjects/Keywords: supersonic tunnel

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APA (6th Edition):

Ratliff, W. C. (2008). REVITALIZATION AND INITIAL TESTING OF A BLOWDOWN SUPERSONIC WIND TUNNEL. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-07312008-093307/ ;

Chicago Manual of Style (16th Edition):

Ratliff, West Cardman. “REVITALIZATION AND INITIAL TESTING OF A BLOWDOWN SUPERSONIC WIND TUNNEL.” 2008. Masters Thesis, Mississippi State University. Accessed January 18, 2021. http://sun.library.msstate.edu/ETD-db/theses/available/etd-07312008-093307/ ;.

MLA Handbook (7th Edition):

Ratliff, West Cardman. “REVITALIZATION AND INITIAL TESTING OF A BLOWDOWN SUPERSONIC WIND TUNNEL.” 2008. Web. 18 Jan 2021.

Vancouver:

Ratliff WC. REVITALIZATION AND INITIAL TESTING OF A BLOWDOWN SUPERSONIC WIND TUNNEL. [Internet] [Masters thesis]. Mississippi State University; 2008. [cited 2021 Jan 18]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-07312008-093307/ ;.

Council of Science Editors:

Ratliff WC. REVITALIZATION AND INITIAL TESTING OF A BLOWDOWN SUPERSONIC WIND TUNNEL. [Masters Thesis]. Mississippi State University; 2008. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-07312008-093307/ ;


Texas A&M University

7. Ellis, Dean William. Thermochemistry Measurements in Non-Isobaric Flows.

Degree: PhD, Aerospace Engineering, 2017, Texas A&M University

 The primary research objective of this study is to advance our understanding of flame suppression in supersonic flows by improving a technique capable of measuring… (more)

Subjects/Keywords: thermochemistry; supersonic; laser diagnostic; raman

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APA (6th Edition):

Ellis, D. W. (2017). Thermochemistry Measurements in Non-Isobaric Flows. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/165968

Chicago Manual of Style (16th Edition):

Ellis, Dean William. “Thermochemistry Measurements in Non-Isobaric Flows.” 2017. Doctoral Dissertation, Texas A&M University. Accessed January 18, 2021. http://hdl.handle.net/1969.1/165968.

MLA Handbook (7th Edition):

Ellis, Dean William. “Thermochemistry Measurements in Non-Isobaric Flows.” 2017. Web. 18 Jan 2021.

Vancouver:

Ellis DW. Thermochemistry Measurements in Non-Isobaric Flows. [Internet] [Doctoral dissertation]. Texas A&M University; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1969.1/165968.

Council of Science Editors:

Ellis DW. Thermochemistry Measurements in Non-Isobaric Flows. [Doctoral Dissertation]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/165968


Penn State University

8. Karns, Alex Mitchell. Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements.

Degree: 2014, Penn State University

 The study of military style exhaust nozzles to further understand their acoustic characteristics has been the recent focus of the Pennsylvania State University high-speed jet… (more)

Subjects/Keywords: LDV; Laser; Velocimetry; Supersonic Jet

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APA (6th Edition):

Karns, A. M. (2014). Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/22749

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):

Karns, Alex Mitchell. “Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements.” 2014. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/22749.

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

MLA Handbook (7th Edition):

Karns, Alex Mitchell. “Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements.” 2014. Web. 18 Jan 2021.

Vancouver:

Karns AM. Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/22749.

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

Council of Science Editors:

Karns AM. Development of a Laser Doppler Velocimetry System for Supersonic Jet Turbulence Measurements. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/22749

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


Purdue University

9. Fagin, Max Harrison. Payload Mass Improvements of Supersonic Retropropulsive Flight for Human Class Mission to Mars.

Degree: MSin Aeronautics and Astronautics, Aeronautics and Astronautics, 2015, Purdue University

Supersonic retropropulsion (SRP) is the use of retrorockets to decelerate during atmospheric flight while the vehicle is still traveling in the supersonic/hypersonic flight regime. In… (more)

Subjects/Keywords: EDL; Mars; Retropropulsion; Supersonic

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APA (6th Edition):

Fagin, M. H. (2015). Payload Mass Improvements of Supersonic Retropropulsive Flight for Human Class Mission to Mars. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/1199

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):

Fagin, Max Harrison. “Payload Mass Improvements of Supersonic Retropropulsive Flight for Human Class Mission to Mars.” 2015. Thesis, Purdue University. Accessed January 18, 2021. https://docs.lib.purdue.edu/open_access_theses/1199.

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

MLA Handbook (7th Edition):

Fagin, Max Harrison. “Payload Mass Improvements of Supersonic Retropropulsive Flight for Human Class Mission to Mars.” 2015. Web. 18 Jan 2021.

Vancouver:

Fagin MH. Payload Mass Improvements of Supersonic Retropropulsive Flight for Human Class Mission to Mars. [Internet] [Thesis]. Purdue University; 2015. [cited 2021 Jan 18]. Available from: https://docs.lib.purdue.edu/open_access_theses/1199.

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

Council of Science Editors:

Fagin MH. Payload Mass Improvements of Supersonic Retropropulsive Flight for Human Class Mission to Mars. [Thesis]. Purdue University; 2015. Available from: https://docs.lib.purdue.edu/open_access_theses/1199

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


University of Illinois – Urbana-Champaign

10. Su, Rui. Supersonic cooling of short-lived molecular states in a pulsed microcavity plasma jet.

Degree: MS, Electrical & Computer Engr, 2016, University of Illinois – Urbana-Champaign

 Electronic states of helium diners having potential energy > 24 eV and radiative lifetimes as short as 19 ns have been generated in a micro-plasma… (more)

Subjects/Keywords: microplasma; supersonic cooling; molecular spectroscopy

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APA (6th Edition):

Su, R. (2016). Supersonic cooling of short-lived molecular states in a pulsed microcavity plasma jet. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/90736

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):

Su, Rui. “Supersonic cooling of short-lived molecular states in a pulsed microcavity plasma jet.” 2016. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2021. http://hdl.handle.net/2142/90736.

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

MLA Handbook (7th Edition):

Su, Rui. “Supersonic cooling of short-lived molecular states in a pulsed microcavity plasma jet.” 2016. Web. 18 Jan 2021.

Vancouver:

Su R. Supersonic cooling of short-lived molecular states in a pulsed microcavity plasma jet. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2142/90736.

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

Council of Science Editors:

Su R. Supersonic cooling of short-lived molecular states in a pulsed microcavity plasma jet. [Thesis]. University of Illinois – Urbana-Champaign; 2016. Available from: http://hdl.handle.net/2142/90736

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


University of Windsor

11. Peirone, Chris. An Experimental Investigation of Tank Pressure Oscillations during Filling with a Bi-Stable Load Switched Supersonic Fluidic Oscillator.

Degree: MA, Mechanical, Automotive, and Materials Engineering, 2019, University of Windsor

 Preliminary testing shows that providing pressure pulsations during the super plastic forming process has proven to increase the total elongation of the material and is… (more)

Subjects/Keywords: Experiment; Fluidics; Oscillator; Supersonic

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APA (6th Edition):

Peirone, C. (2019). An Experimental Investigation of Tank Pressure Oscillations during Filling with a Bi-Stable Load Switched Supersonic Fluidic Oscillator. (Masters Thesis). University of Windsor. Retrieved from https://scholar.uwindsor.ca/etd/7833

Chicago Manual of Style (16th Edition):

Peirone, Chris. “An Experimental Investigation of Tank Pressure Oscillations during Filling with a Bi-Stable Load Switched Supersonic Fluidic Oscillator.” 2019. Masters Thesis, University of Windsor. Accessed January 18, 2021. https://scholar.uwindsor.ca/etd/7833.

MLA Handbook (7th Edition):

Peirone, Chris. “An Experimental Investigation of Tank Pressure Oscillations during Filling with a Bi-Stable Load Switched Supersonic Fluidic Oscillator.” 2019. Web. 18 Jan 2021.

Vancouver:

Peirone C. An Experimental Investigation of Tank Pressure Oscillations during Filling with a Bi-Stable Load Switched Supersonic Fluidic Oscillator. [Internet] [Masters thesis]. University of Windsor; 2019. [cited 2021 Jan 18]. Available from: https://scholar.uwindsor.ca/etd/7833.

Council of Science Editors:

Peirone C. An Experimental Investigation of Tank Pressure Oscillations during Filling with a Bi-Stable Load Switched Supersonic Fluidic Oscillator. [Masters Thesis]. University of Windsor; 2019. Available from: https://scholar.uwindsor.ca/etd/7833


University of Arizona

12. Bailey, Vincent Patrick, 1928-. Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics .

Degree: 1962, University of Arizona

Subjects/Keywords: Supersonic nozzles.

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APA (6th Edition):

Bailey, Vincent Patrick, 1. (1962). Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/551615

Chicago Manual of Style (16th Edition):

Bailey, Vincent Patrick, 1928-. “Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics .” 1962. Masters Thesis, University of Arizona. Accessed January 18, 2021. http://hdl.handle.net/10150/551615.

MLA Handbook (7th Edition):

Bailey, Vincent Patrick, 1928-. “Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics .” 1962. Web. 18 Jan 2021.

Vancouver:

Bailey, Vincent Patrick 1. Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics . [Internet] [Masters thesis]. University of Arizona; 1962. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10150/551615.

Council of Science Editors:

Bailey, Vincent Patrick 1. Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics . [Masters Thesis]. University of Arizona; 1962. Available from: http://hdl.handle.net/10150/551615


Georgia Tech

13. McCauley, William DeForest. Investigation of the effects of precondensation sections in two-dimensional supersonic flow.

Degree: MS, Aeronautical Engineering, 1951, Georgia Tech

Subjects/Keywords: Aerodynamics; Supersonic

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APA (6th Edition):

McCauley, W. D. (1951). Investigation of the effects of precondensation sections in two-dimensional supersonic flow. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12162

Chicago Manual of Style (16th Edition):

McCauley, William DeForest. “Investigation of the effects of precondensation sections in two-dimensional supersonic flow.” 1951. Masters Thesis, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/12162.

MLA Handbook (7th Edition):

McCauley, William DeForest. “Investigation of the effects of precondensation sections in two-dimensional supersonic flow.” 1951. Web. 18 Jan 2021.

Vancouver:

McCauley WD. Investigation of the effects of precondensation sections in two-dimensional supersonic flow. [Internet] [Masters thesis]. Georgia Tech; 1951. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/12162.

Council of Science Editors:

McCauley WD. Investigation of the effects of precondensation sections in two-dimensional supersonic flow. [Masters Thesis]. Georgia Tech; 1951. Available from: http://hdl.handle.net/1853/12162


Rutgers University

14. Todd, Nathan, 1992-. Technopolitics of commercial supersonic flight.

Degree: MA, History, 2020, Rutgers University

 The study of technological development and technopolitics is complex. The history of the three supersonic commercial transports, or SST, developed and built in the 1960s… (more)

Subjects/Keywords: Supersonic transport planes  – Political aspects

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APA (6th Edition):

Todd, Nathan, 1. (2020). Technopolitics of commercial supersonic flight. (Masters Thesis). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/63336/

Chicago Manual of Style (16th Edition):

Todd, Nathan, 1992-. “Technopolitics of commercial supersonic flight.” 2020. Masters Thesis, Rutgers University. Accessed January 18, 2021. https://rucore.libraries.rutgers.edu/rutgers-lib/63336/.

MLA Handbook (7th Edition):

Todd, Nathan, 1992-. “Technopolitics of commercial supersonic flight.” 2020. Web. 18 Jan 2021.

Vancouver:

Todd, Nathan 1. Technopolitics of commercial supersonic flight. [Internet] [Masters thesis]. Rutgers University; 2020. [cited 2021 Jan 18]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/63336/.

Council of Science Editors:

Todd, Nathan 1. Technopolitics of commercial supersonic flight. [Masters Thesis]. Rutgers University; 2020. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/63336/


Georgia Tech

15. Ochs, Bradley Alan. Ignition, topology, and growth of turbulent premixed flames in supersonic flows.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

Supersonic combustion ramjets (scramjets) are currently the most efficient combustor technology for air breathing hypersonic flight, however, lack of fundamental understanding and numerous engineering challenges… (more)

Subjects/Keywords: Hypersonics; Supersonic flows; Supersonic combustion; Laser ignition; Turbulent flames; Premixed flames

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APA (6th Edition):

Ochs, B. A. (2019). Ignition, topology, and growth of turbulent premixed flames in supersonic flows. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62313

Chicago Manual of Style (16th Edition):

Ochs, Bradley Alan. “Ignition, topology, and growth of turbulent premixed flames in supersonic flows.” 2019. Doctoral Dissertation, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/62313.

MLA Handbook (7th Edition):

Ochs, Bradley Alan. “Ignition, topology, and growth of turbulent premixed flames in supersonic flows.” 2019. Web. 18 Jan 2021.

Vancouver:

Ochs BA. Ignition, topology, and growth of turbulent premixed flames in supersonic flows. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/62313.

Council of Science Editors:

Ochs BA. Ignition, topology, and growth of turbulent premixed flames in supersonic flows. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/62313


University of Cambridge

16. Sabnis, Kshitij. Supersonic Corner Flows in Rectangular Channels.

Degree: PhD, 2020, University of Cambridge

 Rectangular channel geometries are widely encountered in supersonic flows, such as in wind tunnels and in aircraft inlets. Shock-boundary-layer interactions in these flows are known… (more)

Subjects/Keywords: Supersonic; Compressible flow; Supersonic wind tunnels; Corner flows; Rectangular channel flow

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

APA (6th Edition):

Sabnis, K. (2020). Supersonic Corner Flows in Rectangular Channels. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/312706

Chicago Manual of Style (16th Edition):

Sabnis, Kshitij. “Supersonic Corner Flows in Rectangular Channels.” 2020. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2021. https://www.repository.cam.ac.uk/handle/1810/312706.

MLA Handbook (7th Edition):

Sabnis, Kshitij. “Supersonic Corner Flows in Rectangular Channels.” 2020. Web. 18 Jan 2021.

Vancouver:

Sabnis K. Supersonic Corner Flows in Rectangular Channels. [Internet] [Doctoral dissertation]. University of Cambridge; 2020. [cited 2021 Jan 18]. Available from: https://www.repository.cam.ac.uk/handle/1810/312706.

Council of Science Editors:

Sabnis K. Supersonic Corner Flows in Rectangular Channels. [Doctoral Dissertation]. University of Cambridge; 2020. Available from: https://www.repository.cam.ac.uk/handle/1810/312706


Arizona State University

17. Cleary, Spencer. The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets.

Degree: Aerospace Engineering, 2018, Arizona State University

 The objective of this study is to understand how to integrate conical spike external compression inlets with high bypass turbofan engines for application on future… (more)

Subjects/Keywords: Aerospace engineering; External Compression Inlets; High Bypass Turbofan Engines; Supersonic Aircraft Performance; Supersonic Airliners; Supersonic Propulsion Performance

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

APA (6th Edition):

Cleary, S. (2018). The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/49114

Chicago Manual of Style (16th Edition):

Cleary, Spencer. “The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets.” 2018. Masters Thesis, Arizona State University. Accessed January 18, 2021. http://repository.asu.edu/items/49114.

MLA Handbook (7th Edition):

Cleary, Spencer. “The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets.” 2018. Web. 18 Jan 2021.

Vancouver:

Cleary S. The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets. [Internet] [Masters thesis]. Arizona State University; 2018. [cited 2021 Jan 18]. Available from: http://repository.asu.edu/items/49114.

Council of Science Editors:

Cleary S. The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets. [Masters Thesis]. Arizona State University; 2018. Available from: http://repository.asu.edu/items/49114


University of Maryland

18. Adamson, Colin Sawyer. Heat Transfer Measurements in a Supersonic Film Flow.

Degree: Aerospace Engineering, 2016, University of Maryland

 This thesis presents measurements of wall heat flux and flow structure in a canonical film cooling configuration with Mach 2.3 core flow in which the… (more)

Subjects/Keywords: Aerospace engineering; Film Cooling; Heat Flux Measurements; Heat Transfer; Supersonic Film Cooling; Supersonic Flow; Supersonic Heat Transfer

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

APA (6th Edition):

Adamson, C. S. (2016). Heat Transfer Measurements in a Supersonic Film Flow. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/18424

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):

Adamson, Colin Sawyer. “Heat Transfer Measurements in a Supersonic Film Flow.” 2016. Thesis, University of Maryland. Accessed January 18, 2021. http://hdl.handle.net/1903/18424.

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

MLA Handbook (7th Edition):

Adamson, Colin Sawyer. “Heat Transfer Measurements in a Supersonic Film Flow.” 2016. Web. 18 Jan 2021.

Vancouver:

Adamson CS. Heat Transfer Measurements in a Supersonic Film Flow. [Internet] [Thesis]. University of Maryland; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1903/18424.

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

Council of Science Editors:

Adamson CS. Heat Transfer Measurements in a Supersonic Film Flow. [Thesis]. University of Maryland; 2016. Available from: http://hdl.handle.net/1903/18424

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

19. Vijayaraja K. Effect of rib on suddenly expanded supersonic flow;.

Degree: Effect of rib on suddenly expanded supersonic flow, 2014, Anna University

The base pressure field and the wall pressure distribution along the newlineenlarged duct for subsonic correctly underexpanded sonic and supersonic newlineflow at different expansion have… (more)

Subjects/Keywords: mechanical engineering; rib on suddenly; supersonic flow

Page 1

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APA (6th Edition):

K, V. (2014). Effect of rib on suddenly expanded supersonic flow;. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/30470

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):

K, Vijayaraja. “Effect of rib on suddenly expanded supersonic flow;.” 2014. Thesis, Anna University. Accessed January 18, 2021. http://shodhganga.inflibnet.ac.in/handle/10603/30470.

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

MLA Handbook (7th Edition):

K, Vijayaraja. “Effect of rib on suddenly expanded supersonic flow;.” 2014. Web. 18 Jan 2021.

Vancouver:

K V. Effect of rib on suddenly expanded supersonic flow;. [Internet] [Thesis]. Anna University; 2014. [cited 2021 Jan 18]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/30470.

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

Council of Science Editors:

K V. Effect of rib on suddenly expanded supersonic flow;. [Thesis]. Anna University; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/30470

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


Anna University

20. Senthilkumar C. Experimental and numerical studies on the flow characteristics of slanted entry cd nozzle in supersonic streams;.

Degree: Experimental and numerical studies on the flow characteristics of slanted entry cd nozzle in supersonic streams, 2014, Anna University

Flow characteristics of straight and slanted entry CD nozzle with a newlinedesign Mach number of 294 exposed to a Mach 2 free jet has been… (more)

Subjects/Keywords: cd nozzle; mechanical engineering; supersonic streams

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APA (6th Edition):

C, S. (2014). Experimental and numerical studies on the flow characteristics of slanted entry cd nozzle in supersonic streams;. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/31537

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):

C, Senthilkumar. “Experimental and numerical studies on the flow characteristics of slanted entry cd nozzle in supersonic streams;.” 2014. Thesis, Anna University. Accessed January 18, 2021. http://shodhganga.inflibnet.ac.in/handle/10603/31537.

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

MLA Handbook (7th Edition):

C, Senthilkumar. “Experimental and numerical studies on the flow characteristics of slanted entry cd nozzle in supersonic streams;.” 2014. Web. 18 Jan 2021.

Vancouver:

C S. Experimental and numerical studies on the flow characteristics of slanted entry cd nozzle in supersonic streams;. [Internet] [Thesis]. Anna University; 2014. [cited 2021 Jan 18]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/31537.

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

Council of Science Editors:

C S. Experimental and numerical studies on the flow characteristics of slanted entry cd nozzle in supersonic streams;. [Thesis]. Anna University; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/31537

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


Penn State University

21. Powers, Russell. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.

Degree: 2015, Penn State University

 The noise produced by the supersonic, high temperature jets that exhaust from military aircraft is becoming a hazard to naval personnel and a disturbance to… (more)

Subjects/Keywords: Jet Noise; Supersonic; Aeroacoustics; Noise Reduction

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APA (6th Edition):

Powers, R. (2015). Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/26397

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):

Powers, Russell. “Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.” 2015. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/26397.

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

MLA Handbook (7th Edition):

Powers, Russell. “Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.” 2015. Web. 18 Jan 2021.

Vancouver:

Powers R. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/26397.

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

Council of Science Editors:

Powers R. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. [Thesis]. Penn State University; 2015. Available from: https://submit-etda.libraries.psu.edu/catalog/26397

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


Penn State University

22. Morgan, Jessica. Development of the Fluid Insert Noise Reduction Method Investigating Azimuthal Asymmetry.

Degree: 2018, Penn State University

Supersonic tactical aircraft engines create a high amplitude noise environment that leads to hearing loss for military personnel working on aircraft carriers and noise complaints… (more)

Subjects/Keywords: Aeroacoustics; Supersonic; Noise Reduction; Jet Noise; PIV

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APA (6th Edition):

Morgan, J. (2018). Development of the Fluid Insert Noise Reduction Method Investigating Azimuthal Asymmetry. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15696jum360

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):

Morgan, Jessica. “Development of the Fluid Insert Noise Reduction Method Investigating Azimuthal Asymmetry.” 2018. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/15696jum360.

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

MLA Handbook (7th Edition):

Morgan, Jessica. “Development of the Fluid Insert Noise Reduction Method Investigating Azimuthal Asymmetry.” 2018. Web. 18 Jan 2021.

Vancouver:

Morgan J. Development of the Fluid Insert Noise Reduction Method Investigating Azimuthal Asymmetry. [Internet] [Thesis]. Penn State University; 2018. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/15696jum360.

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

Council of Science Editors:

Morgan J. Development of the Fluid Insert Noise Reduction Method Investigating Azimuthal Asymmetry. [Thesis]. Penn State University; 2018. Available from: https://submit-etda.libraries.psu.edu/catalog/15696jum360

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


University of Cambridge

23. Coles, Charlotte. The Impact of Surface Roughness on Transonic Inlet Lip-Flows at Incidence.

Degree: PhD, 2019, University of Cambridge

 At high angles of incidence, the flow-field around the lower inlet lip of a typical engine can accelerate to a supersonic value, creating a local… (more)

Subjects/Keywords: fluid dynamics; supersonic flow; shock wave

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

APA (6th Edition):

Coles, C. (2019). The Impact of Surface Roughness on Transonic Inlet Lip-Flows at Incidence. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/298263

Chicago Manual of Style (16th Edition):

Coles, Charlotte. “The Impact of Surface Roughness on Transonic Inlet Lip-Flows at Incidence.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2021. https://www.repository.cam.ac.uk/handle/1810/298263.

MLA Handbook (7th Edition):

Coles, Charlotte. “The Impact of Surface Roughness on Transonic Inlet Lip-Flows at Incidence.” 2019. Web. 18 Jan 2021.

Vancouver:

Coles C. The Impact of Surface Roughness on Transonic Inlet Lip-Flows at Incidence. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 18]. Available from: https://www.repository.cam.ac.uk/handle/1810/298263.

Council of Science Editors:

Coles C. The Impact of Surface Roughness on Transonic Inlet Lip-Flows at Incidence. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/298263


Université Catholique de Louvain

24. Lamberts, Olivier. Choking and mixing phenomena in supersonic ejectors.

Degree: 2018, Université Catholique de Louvain

The purpose of a supersonic ejector consists in the mixing of two fluids with different stagnation pressures in order to obtain a fluid at an… (more)

Subjects/Keywords: Supersonic; Ejector; Choking; Fabri; Exergy; Compound-choking

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APA (6th Edition):

Lamberts, O. (2018). Choking and mixing phenomena in supersonic ejectors. (Thesis). Université Catholique de Louvain. Retrieved from http://hdl.handle.net/2078.1/203675

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):

Lamberts, Olivier. “Choking and mixing phenomena in supersonic ejectors.” 2018. Thesis, Université Catholique de Louvain. Accessed January 18, 2021. http://hdl.handle.net/2078.1/203675.

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

MLA Handbook (7th Edition):

Lamberts, Olivier. “Choking and mixing phenomena in supersonic ejectors.” 2018. Web. 18 Jan 2021.

Vancouver:

Lamberts O. Choking and mixing phenomena in supersonic ejectors. [Internet] [Thesis]. Université Catholique de Louvain; 2018. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2078.1/203675.

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

Council of Science Editors:

Lamberts O. Choking and mixing phenomena in supersonic ejectors. [Thesis]. Université Catholique de Louvain; 2018. Available from: http://hdl.handle.net/2078.1/203675

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


Georgia Tech

25. Crane, Nathan Thomas. A methodology to reduce dimensionality of a commercial supersonic transport design space using active subspaces.

Degree: MS, Aerospace Engineering, 2020, Georgia Tech

 As the commercial aviation industry continues to grow, the next technological leap is speed, and commercial supersonic transports are reappearing from multiple companies. Although this… (more)

Subjects/Keywords: Commercial supersonic; Active subspace; Aircraft design

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

APA (6th Edition):

Crane, N. T. (2020). A methodology to reduce dimensionality of a commercial supersonic transport design space using active subspaces. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62854

Chicago Manual of Style (16th Edition):

Crane, Nathan Thomas. “A methodology to reduce dimensionality of a commercial supersonic transport design space using active subspaces.” 2020. Masters Thesis, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/62854.

MLA Handbook (7th Edition):

Crane, Nathan Thomas. “A methodology to reduce dimensionality of a commercial supersonic transport design space using active subspaces.” 2020. Web. 18 Jan 2021.

Vancouver:

Crane NT. A methodology to reduce dimensionality of a commercial supersonic transport design space using active subspaces. [Internet] [Masters thesis]. Georgia Tech; 2020. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/62854.

Council of Science Editors:

Crane NT. A methodology to reduce dimensionality of a commercial supersonic transport design space using active subspaces. [Masters Thesis]. Georgia Tech; 2020. Available from: http://hdl.handle.net/1853/62854


Delft University of Technology

26. Voogt, Nick (author). Investigation on supersonic, large wall roughness elements using QIRT and PIV.

Degree: 2017, Delft University of Technology

In spaceflight, a launch vehicle is a rocket used to carry a payload from the Earth's surface into outer space. By traveling supersonically, launch vehicles… (more)

Subjects/Keywords: QIRT; supersonic; ribbed roughness; PIV; heat transfer

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APA (6th Edition):

Voogt, N. (. (2017). Investigation on supersonic, large wall roughness elements using QIRT and PIV. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:737e4a9d-75de-4699-88e2-b611f93a88b5

Chicago Manual of Style (16th Edition):

Voogt, Nick (author). “Investigation on supersonic, large wall roughness elements using QIRT and PIV.” 2017. Masters Thesis, Delft University of Technology. Accessed January 18, 2021. http://resolver.tudelft.nl/uuid:737e4a9d-75de-4699-88e2-b611f93a88b5.

MLA Handbook (7th Edition):

Voogt, Nick (author). “Investigation on supersonic, large wall roughness elements using QIRT and PIV.” 2017. Web. 18 Jan 2021.

Vancouver:

Voogt N(. Investigation on supersonic, large wall roughness elements using QIRT and PIV. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:737e4a9d-75de-4699-88e2-b611f93a88b5.

Council of Science Editors:

Voogt N(. Investigation on supersonic, large wall roughness elements using QIRT and PIV. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:737e4a9d-75de-4699-88e2-b611f93a88b5


Princeton University

27. Grube, Nathan Elias. Shock Wave – Turbulence Interactions .

Degree: PhD, 2020, Princeton University

 Canonical shock / isotropic turbulence interactions (SITIs) are studied using direct numerical simulation (DNS) and perturbation analysis. Flow parameters include unprecedentedly high turbulence Mach numbers… (more)

Subjects/Keywords: Hypersonic; Interaction; Shock; Shockwave; Supersonic; Turbulence

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APA (6th Edition):

Grube, N. E. (2020). Shock Wave – Turbulence Interactions . (Doctoral Dissertation). Princeton University. Retrieved from http://arks.princeton.edu/ark:/88435/dsp01j6731673z

Chicago Manual of Style (16th Edition):

Grube, Nathan Elias. “Shock Wave – Turbulence Interactions .” 2020. Doctoral Dissertation, Princeton University. Accessed January 18, 2021. http://arks.princeton.edu/ark:/88435/dsp01j6731673z.

MLA Handbook (7th Edition):

Grube, Nathan Elias. “Shock Wave – Turbulence Interactions .” 2020. Web. 18 Jan 2021.

Vancouver:

Grube NE. Shock Wave – Turbulence Interactions . [Internet] [Doctoral dissertation]. Princeton University; 2020. [cited 2021 Jan 18]. Available from: http://arks.princeton.edu/ark:/88435/dsp01j6731673z.

Council of Science Editors:

Grube NE. Shock Wave – Turbulence Interactions . [Doctoral Dissertation]. Princeton University; 2020. Available from: http://arks.princeton.edu/ark:/88435/dsp01j6731673z


University of New Mexico

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

Degree: Mechanical Engineering, 2016, University of New Mexico

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Olmstead, Dell. “Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column.” 2016. Doctoral Dissertation, University of New Mexico. Accessed January 18, 2021. http://hdl.handle.net/1928/31737.

MLA Handbook (7th Edition):

Olmstead, Dell. “Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column.” 2016. Web. 18 Jan 2021.

Vancouver:

Olmstead D. Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column. [Internet] [Doctoral dissertation]. University of New Mexico; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1928/31737.

Council of Science Editors:

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


University of Minnesota

29. Kreitzman, Jordan. Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet.

Degree: MS, Aerospace Engineering and Mechanics, 2015, University of Minnesota

 Source terms corresponding to Goldstein's generalized acoustic analogy are computed from a high-fidelity simulation of a supersonic jet issuing from a rectangular nozzle with chevrons.… (more)

Subjects/Keywords: acoustic; chevron; jet; rectangular; source; supersonic

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APA (6th Edition):

Kreitzman, J. (2015). Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet. (Masters Thesis). University of Minnesota. Retrieved from http://hdl.handle.net/11299/174797

Chicago Manual of Style (16th Edition):

Kreitzman, Jordan. “Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet.” 2015. Masters Thesis, University of Minnesota. Accessed January 18, 2021. http://hdl.handle.net/11299/174797.

MLA Handbook (7th Edition):

Kreitzman, Jordan. “Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet.” 2015. Web. 18 Jan 2021.

Vancouver:

Kreitzman J. Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet. [Internet] [Masters thesis]. University of Minnesota; 2015. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11299/174797.

Council of Science Editors:

Kreitzman J. Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet. [Masters Thesis]. University of Minnesota; 2015. Available from: http://hdl.handle.net/11299/174797


University of Cambridge

30. Michaux, Laurent. Supersonic Laser Deposition and LaserForge: Process Mechanism Coating Characteristics.

Degree: PhD, 2020, University of Cambridge

 LaserForge is a commercial coating process, that uses a pulsed laser to deposit flat sided wire onto a substrate with minimal heat input. Supersonic Laser… (more)

Subjects/Keywords: Supersonic Laser Deposition; WC-17Co; LaserForge; Coating

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APA (6th Edition):

Michaux, L. (2020). Supersonic Laser Deposition and LaserForge: Process Mechanism Coating Characteristics. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/304202https://www.repository.cam.ac.uk/bitstream/1810/304202/3/4c8c1208-1583-419b-af19-40078a9f209b_confirmations.txt ; https://www.repository.cam.ac.uk/bitstream/1810/304202/4/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/304202/5/4c8c1208-1583-419b-af19-40078a9f209b.zip

Chicago Manual of Style (16th Edition):

Michaux, Laurent. “Supersonic Laser Deposition and LaserForge: Process Mechanism Coating Characteristics.” 2020. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2021. https://www.repository.cam.ac.uk/handle/1810/304202https://www.repository.cam.ac.uk/bitstream/1810/304202/3/4c8c1208-1583-419b-af19-40078a9f209b_confirmations.txt ; https://www.repository.cam.ac.uk/bitstream/1810/304202/4/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/304202/5/4c8c1208-1583-419b-af19-40078a9f209b.zip.

MLA Handbook (7th Edition):

Michaux, Laurent. “Supersonic Laser Deposition and LaserForge: Process Mechanism Coating Characteristics.” 2020. Web. 18 Jan 2021.

Vancouver:

Michaux L. Supersonic Laser Deposition and LaserForge: Process Mechanism Coating Characteristics. [Internet] [Doctoral dissertation]. University of Cambridge; 2020. [cited 2021 Jan 18]. Available from: https://www.repository.cam.ac.uk/handle/1810/304202https://www.repository.cam.ac.uk/bitstream/1810/304202/3/4c8c1208-1583-419b-af19-40078a9f209b_confirmations.txt ; https://www.repository.cam.ac.uk/bitstream/1810/304202/4/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/304202/5/4c8c1208-1583-419b-af19-40078a9f209b.zip.

Council of Science Editors:

Michaux L. Supersonic Laser Deposition and LaserForge: Process Mechanism Coating Characteristics. [Doctoral Dissertation]. University of Cambridge; 2020. Available from: https://www.repository.cam.ac.uk/handle/1810/304202https://www.repository.cam.ac.uk/bitstream/1810/304202/3/4c8c1208-1583-419b-af19-40078a9f209b_confirmations.txt ; https://www.repository.cam.ac.uk/bitstream/1810/304202/4/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/304202/5/4c8c1208-1583-419b-af19-40078a9f209b.zip

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