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You searched for subject:(Supersonic). Showing records 1 – 30 of 447 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: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154986

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):

Sheffield, Les. “Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams.” 2015. Thesis, Texas A&M University. Accessed January 24, 2020. http://hdl.handle.net/1969.1/154986.

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

MLA Handbook (7th Edition):

Sheffield, Les. “Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams.” 2015. Web. 24 Jan 2020.

Vancouver:

Sheffield L. Velocity Augmentation of a Supersonic Source and The Production of Slow, Cold, Molecular Beams. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/1969.1/154986.

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

Council of Science Editors:

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

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


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 24, 2020. 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. 24 Jan 2020.

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 2020 Jan 24]. 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/


University of New South Wales

3. 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 24, 2020. 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. 24 Jan 2020.

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 2020 Jan 24]. 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

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

Degree: 2013, 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. (2013). Experimental Investigations on Supersonic Ejectors. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3402 ; http://etd.iisc.ernet.in/abstracts/4268/G25868-Abs.pdf

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):

Srisha Rao, M V. “Experimental Investigations on Supersonic Ejectors.” 2013. Thesis, Indian Institute of Science. Accessed January 24, 2020. http://etd.iisc.ernet.in/2005/3402 ; http://etd.iisc.ernet.in/abstracts/4268/G25868-Abs.pdf.

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

MLA Handbook (7th Edition):

Srisha Rao, M V. “Experimental Investigations on Supersonic Ejectors.” 2013. Web. 24 Jan 2020.

Vancouver:

Srisha Rao MV. Experimental Investigations on Supersonic Ejectors. [Internet] [Thesis]. Indian Institute of Science; 2013. [cited 2020 Jan 24]. Available from: http://etd.iisc.ernet.in/2005/3402 ; http://etd.iisc.ernet.in/abstracts/4268/G25868-Abs.pdf.

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

Council of Science Editors:

Srisha Rao MV. Experimental Investigations on Supersonic Ejectors. [Thesis]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ernet.in/2005/3402 ; http://etd.iisc.ernet.in/abstracts/4268/G25868-Abs.pdf

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


Purdue University

5. 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 24, 2020. 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. 24 Jan 2020.

Vancouver:

Fagin MH. Payload Mass Improvements of Supersonic Retropropulsive Flight for Human Class Mission to Mars. [Internet] [Thesis]. Purdue University; 2015. [cited 2020 Jan 24]. 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

6. 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 24, 2020. 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. 24 Jan 2020.

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 2020 Jan 24]. 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 Illinois – Urbana-Champaign

7. Yeong, Yong Han. Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft.

Degree: MS, 4048, 2010, University of Illinois – Urbana-Champaign

 Sonic boom attenuation is a considerable design challenge to enable civilian aircraft to operate at supersonic flight conditions. One technology proposed by Gulfstream Aerospace Corporation… (more)

Subjects/Keywords: Sonic Boom; Supersonic; Nacelle Bypass

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APA (6th Edition):

Yeong, Y. H. (2010). Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/14621

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):

Yeong, Yong Han. “Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft.” 2010. Thesis, University of Illinois – Urbana-Champaign. Accessed January 24, 2020. http://hdl.handle.net/2142/14621.

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

MLA Handbook (7th Edition):

Yeong, Yong Han. “Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft.” 2010. Web. 24 Jan 2020.

Vancouver:

Yeong YH. Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2010. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/2142/14621.

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

Council of Science Editors:

Yeong YH. Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft. [Thesis]. University of Illinois – Urbana-Champaign; 2010. Available from: http://hdl.handle.net/2142/14621

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


Texas A&M University

8. 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 24, 2020. http://hdl.handle.net/1969.1/165968.

MLA Handbook (7th Edition):

Ellis, Dean William. “Thermochemistry Measurements in Non-Isobaric Flows.” 2017. Web. 24 Jan 2020.

Vancouver:

Ellis DW. Thermochemistry Measurements in Non-Isobaric Flows. [Internet] [Doctoral dissertation]. Texas A&M University; 2017. [cited 2020 Jan 24]. 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


Mississippi State University

9. 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 24, 2020. 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. 24 Jan 2020.

Vancouver:

Ratliff WC. REVITALIZATION AND INITIAL TESTING OF A BLOWDOWN SUPERSONIC WIND TUNNEL. [Internet] [Masters thesis]. Mississippi State University; 2008. [cited 2020 Jan 24]. 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/ ;


McGill University

10. O'Connell, Kevin John. Shock interaction due to blunt leading edges of two-dimensional hypersonic inlets.

Degree: M. Eng., Department of Mechanical Engineering, 1969, McGill University

Subjects/Keywords: Aerodynamics; Supersonic

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APA (6th Edition):

O'Connell, K. J. (1969). Shock interaction due to blunt leading edges of two-dimensional hypersonic inlets. (Masters Thesis). McGill University. Retrieved from http://digitool.library.mcgill.ca/thesisfile49033.pdf

Chicago Manual of Style (16th Edition):

O'Connell, Kevin John. “Shock interaction due to blunt leading edges of two-dimensional hypersonic inlets.” 1969. Masters Thesis, McGill University. Accessed January 24, 2020. http://digitool.library.mcgill.ca/thesisfile49033.pdf.

MLA Handbook (7th Edition):

O'Connell, Kevin John. “Shock interaction due to blunt leading edges of two-dimensional hypersonic inlets.” 1969. Web. 24 Jan 2020.

Vancouver:

O'Connell KJ. Shock interaction due to blunt leading edges of two-dimensional hypersonic inlets. [Internet] [Masters thesis]. McGill University; 1969. [cited 2020 Jan 24]. Available from: http://digitool.library.mcgill.ca/thesisfile49033.pdf.

Council of Science Editors:

O'Connell KJ. Shock interaction due to blunt leading edges of two-dimensional hypersonic inlets. [Masters Thesis]. McGill University; 1969. Available from: http://digitool.library.mcgill.ca/thesisfile49033.pdf


Rutgers University

11. Anderson, Kellie, 1980-. Interaction of heated filaments with a blunt body in supersonic flow:.

Degree: MS, Mechanical and Aerospace Engineering, 2010, Rutgers University

 Two computational studies are performed to examine the influence of energy deposition on a blunt body in supersonic flow. The first objective is to determine… (more)

Subjects/Keywords: Heat – Transmission; Aerodynamics, Supersonic

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APA (6th Edition):

Anderson, Kellie, 1. (2010). Interaction of heated filaments with a blunt body in supersonic flow:. (Masters Thesis). Rutgers University. Retrieved from http://hdl.rutgers.edu/1782.2/rucore10001600001.ETD.000052093

Chicago Manual of Style (16th Edition):

Anderson, Kellie, 1980-. “Interaction of heated filaments with a blunt body in supersonic flow:.” 2010. Masters Thesis, Rutgers University. Accessed January 24, 2020. http://hdl.rutgers.edu/1782.2/rucore10001600001.ETD.000052093.

MLA Handbook (7th Edition):

Anderson, Kellie, 1980-. “Interaction of heated filaments with a blunt body in supersonic flow:.” 2010. Web. 24 Jan 2020.

Vancouver:

Anderson, Kellie 1. Interaction of heated filaments with a blunt body in supersonic flow:. [Internet] [Masters thesis]. Rutgers University; 2010. [cited 2020 Jan 24]. Available from: http://hdl.rutgers.edu/1782.2/rucore10001600001.ETD.000052093.

Council of Science Editors:

Anderson, Kellie 1. Interaction of heated filaments with a blunt body in supersonic flow:. [Masters Thesis]. Rutgers University; 2010. Available from: http://hdl.rutgers.edu/1782.2/rucore10001600001.ETD.000052093


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 24, 2020. 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. 24 Jan 2020.

Vancouver:

Bailey, Vincent Patrick 1. Design of an axisymmetric, hypersonic nozzle, utilizing the method of characteristics . [Internet] [Masters thesis]. University of Arizona; 1962. [cited 2020 Jan 24]. 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


University of Windsor

13. 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 24, 2020. 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. 24 Jan 2020.

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 2020 Jan 24]. 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


Arizona State University

14. 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 (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 24, 2020. 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. 24 Jan 2020.

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 2020 Jan 24]. 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


The Ohio State University

15. Komar, James Joseph. Investigation of fluid dynamic interactions within multiple nozzle arrays.

Degree: PhD, Graduate School, 1975, The Ohio State University

Subjects/Keywords: Engineering; Supersonic nozzles

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

APA (6th Edition):

Komar, J. J. (1975). Investigation of fluid dynamic interactions within multiple nozzle arrays. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1486991991163993

Chicago Manual of Style (16th Edition):

Komar, James Joseph. “Investigation of fluid dynamic interactions within multiple nozzle arrays.” 1975. Doctoral Dissertation, The Ohio State University. Accessed January 24, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1486991991163993.

MLA Handbook (7th Edition):

Komar, James Joseph. “Investigation of fluid dynamic interactions within multiple nozzle arrays.” 1975. Web. 24 Jan 2020.

Vancouver:

Komar JJ. Investigation of fluid dynamic interactions within multiple nozzle arrays. [Internet] [Doctoral dissertation]. The Ohio State University; 1975. [cited 2020 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486991991163993.

Council of Science Editors:

Komar JJ. Investigation of fluid dynamic interactions within multiple nozzle arrays. [Doctoral Dissertation]. The Ohio State University; 1975. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486991991163993

16. 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 24, 2020. 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. 24 Jan 2020.

Vancouver:

K V. Effect of rib on suddenly expanded supersonic flow;. [Internet] [Thesis]. Anna University; 2014. [cited 2020 Jan 24]. 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

17. 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 24, 2020. 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. 24 Jan 2020.

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 2020 Jan 24]. 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


University of Minnesota

18. 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 24, 2020. http://hdl.handle.net/11299/174797.

MLA Handbook (7th Edition):

Kreitzman, Jordan. “Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet.” 2015. Web. 24 Jan 2020.

Vancouver:

Kreitzman J. Acoustic Source Analysis of a Supersonic Rectangular Chevron Jet. [Internet] [Masters thesis]. University of Minnesota; 2015. [cited 2020 Jan 24]. 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 New Mexico

19. 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 24, 2020. http://hdl.handle.net/1928/31737.

MLA Handbook (7th Edition):

Olmstead, Dell. “Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column.” 2016. Web. 24 Jan 2020.

Vancouver:

Olmstead D. Oblique Shock Wave Effects on Impulsively Accelerated Heavy Gas Column. [Internet] [Doctoral dissertation]. University of New Mexico; 2016. [cited 2020 Jan 24]. 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


The Ohio State University

20. Xiao, Ruiyang. The Freezing of Highly Sub-cooled H2O/D2O Droplets.

Degree: MS, Environmental Science, 2008, The Ohio State University

 The condensation of H2O and D2O in a supersonic Laval nozzle was investigated at different stagnation condition by using Pressure Trace Measurements (PTM) and Fourier… (more)

Subjects/Keywords: Chemistry; sub-cooled droplets; FTIR; supersonic nozzle

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APA (6th Edition):

Xiao, R. (2008). The Freezing of Highly Sub-cooled H2O/D2O Droplets. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1211567463

Chicago Manual of Style (16th Edition):

Xiao, Ruiyang. “The Freezing of Highly Sub-cooled H2O/D2O Droplets.” 2008. Masters Thesis, The Ohio State University. Accessed January 24, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1211567463.

MLA Handbook (7th Edition):

Xiao, Ruiyang. “The Freezing of Highly Sub-cooled H2O/D2O Droplets.” 2008. Web. 24 Jan 2020.

Vancouver:

Xiao R. The Freezing of Highly Sub-cooled H2O/D2O Droplets. [Internet] [Masters thesis]. The Ohio State University; 2008. [cited 2020 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1211567463.

Council of Science Editors:

Xiao R. The Freezing of Highly Sub-cooled H2O/D2O Droplets. [Masters Thesis]. The Ohio State University; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1211567463


Penn State University

21. Miller, Steven Arthur Eric. The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions.

Degree: PhD, Aerospace Engineering, 2009, Penn State University

 Broadband shock-associated noise is a component of jet noise generated by supersonic jets operating off-design. It is characterized by multiple broadband peaks and dominates the… (more)

Subjects/Keywords: Jet; Noise; Supersonic; Fluid Dynamics; Shock; Broadband

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APA (6th Edition):

Miller, S. A. E. (2009). The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9945

Chicago Manual of Style (16th Edition):

Miller, Steven Arthur Eric. “The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions.” 2009. Doctoral Dissertation, Penn State University. Accessed January 24, 2020. https://etda.libraries.psu.edu/catalog/9945.

MLA Handbook (7th Edition):

Miller, Steven Arthur Eric. “The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions.” 2009. Web. 24 Jan 2020.

Vancouver:

Miller SAE. The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions. [Internet] [Doctoral dissertation]. Penn State University; 2009. [cited 2020 Jan 24]. Available from: https://etda.libraries.psu.edu/catalog/9945.

Council of Science Editors:

Miller SAE. The Prediction of Broadband Shock-Associated Noise Using Reynolds-Averaged Navier-Stokes Solutions. [Doctoral Dissertation]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9945


Penn State University

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Li, Jian. “IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING.” 2008. Doctoral Dissertation, Penn State University. Accessed January 24, 2020. https://etda.libraries.psu.edu/catalog/9560.

MLA Handbook (7th Edition):

Li, Jian. “IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING.” 2008. Web. 24 Jan 2020.

Vancouver:

Li J. IGNITION TRANSIENT IN AN ETHYLENE FUELED SCRAMJET ENGINE WITH AIR THROTTLING. [Internet] [Doctoral dissertation]. Penn State University; 2008. [cited 2020 Jan 24]. Available from: https://etda.libraries.psu.edu/catalog/9560.

Council of Science Editors:

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


Penn State University

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

Degree: PhD, Aerospace Engineering, 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. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/26397

Chicago Manual of Style (16th Edition):

Powers, Russell. “Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.” 2015. Doctoral Dissertation, Penn State University. Accessed January 24, 2020. https://etda.libraries.psu.edu/catalog/26397.

MLA Handbook (7th Edition):

Powers, Russell. “Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.” 2015. Web. 24 Jan 2020.

Vancouver:

Powers R. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. [Internet] [Doctoral dissertation]. Penn State University; 2015. [cited 2020 Jan 24]. Available from: https://etda.libraries.psu.edu/catalog/26397.

Council of Science Editors:

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


Washington University in St. Louis

24. Lee, Han Ju. CFD Performance of Turbulence Models for Flow from Supersonic Nozzle Exhausts.

Degree: MS, Mechanical Engineering & Materials Science, 2017, Washington University in St. Louis

  The goal of this thesis is to compare the performance of several eddy-viscosity turbulence models for computing supersonic nozzle exhaust flows. These flows are… (more)

Subjects/Keywords: Supersonic nozzle; CFD; turbulence models; Engineering

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APA (6th Edition):

Lee, H. J. (2017). CFD Performance of Turbulence Models for Flow from Supersonic Nozzle Exhausts. (Thesis). Washington University in St. Louis. Retrieved from https://openscholarship.wustl.edu/eng_etds/260

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):

Lee, Han Ju. “CFD Performance of Turbulence Models for Flow from Supersonic Nozzle Exhausts.” 2017. Thesis, Washington University in St. Louis. Accessed January 24, 2020. https://openscholarship.wustl.edu/eng_etds/260.

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

MLA Handbook (7th Edition):

Lee, Han Ju. “CFD Performance of Turbulence Models for Flow from Supersonic Nozzle Exhausts.” 2017. Web. 24 Jan 2020.

Vancouver:

Lee HJ. CFD Performance of Turbulence Models for Flow from Supersonic Nozzle Exhausts. [Internet] [Thesis]. Washington University in St. Louis; 2017. [cited 2020 Jan 24]. Available from: https://openscholarship.wustl.edu/eng_etds/260.

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

Council of Science Editors:

Lee HJ. CFD Performance of Turbulence Models for Flow from Supersonic Nozzle Exhausts. [Thesis]. Washington University in St. Louis; 2017. Available from: https://openscholarship.wustl.edu/eng_etds/260

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


University of Cambridge

25. 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 (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 24, 2020. 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. 24 Jan 2020.

Vancouver:

Coles C. The Impact of Surface Roughness on Transonic Inlet Lip-Flows at Incidence. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2020 Jan 24]. 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


Delft University of Technology

26. Mathijssen, T. Stereoscopic PIV on a delta wing in supersonic flow:.

Degree: 2008, Delft University of Technology

 Ever since the 1950s delta wings are being used as an efficient planform for supersonic flight. Over time extensive research on the aerodynamics of this… (more)

Subjects/Keywords: deltawing; delta wing; supersonic; PIV; stereoscopic

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APA (6th Edition):

Mathijssen, T. (2008). Stereoscopic PIV on a delta wing in supersonic flow:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:7e9c2e25-a519-45a7-a685-53a446b37588

Chicago Manual of Style (16th Edition):

Mathijssen, T. “Stereoscopic PIV on a delta wing in supersonic flow:.” 2008. Masters Thesis, Delft University of Technology. Accessed January 24, 2020. http://resolver.tudelft.nl/uuid:7e9c2e25-a519-45a7-a685-53a446b37588.

MLA Handbook (7th Edition):

Mathijssen, T. “Stereoscopic PIV on a delta wing in supersonic flow:.” 2008. Web. 24 Jan 2020.

Vancouver:

Mathijssen T. Stereoscopic PIV on a delta wing in supersonic flow:. [Internet] [Masters thesis]. Delft University of Technology; 2008. [cited 2020 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:7e9c2e25-a519-45a7-a685-53a446b37588.

Council of Science Editors:

Mathijssen T. Stereoscopic PIV on a delta wing in supersonic flow:. [Masters Thesis]. Delft University of Technology; 2008. Available from: http://resolver.tudelft.nl/uuid:7e9c2e25-a519-45a7-a685-53a446b37588


Université Catholique de Louvain

27. 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 24, 2020. 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. 24 Jan 2020.

Vancouver:

Lamberts O. Choking and mixing phenomena in supersonic ejectors. [Internet] [Thesis]. Université Catholique de Louvain; 2018. [cited 2020 Jan 24]. 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


Vanderbilt University

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

Degree: MS, Mechanical Engineering, 2010, Vanderbilt University

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Grady, Nathan Ryan. “Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut.” 2010. Masters Thesis, Vanderbilt University. Accessed January 24, 2020. http://etd.library.vanderbilt.edu/available/etd-12102010-144923/ ;.

MLA Handbook (7th Edition):

Grady, Nathan Ryan. “Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut.” 2010. Web. 24 Jan 2020.

Vancouver:

Grady NR. Hydroxyl Tagging Velocimetry in a Supersonic Flow Over a Ramped-Wall Cavity Flameholder with an Upstream Strut. [Internet] [Masters thesis]. Vanderbilt University; 2010. [cited 2020 Jan 24]. Available from: http://etd.library.vanderbilt.edu/available/etd-12102010-144923/ ;.

Council of Science Editors:

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


University of New South Wales

29. Wittig, Sven. Diode-Laser-Based Velocity and Temperature Measurements from Subsonic to Hypersonic Flow Regimes.

Degree: Engineering & Information Technology, 2011, University of New South Wales

 This thesis describes the development and application of two laser-based diagnostic techniques that allow the non-intrusive measurement of flow properties such as temperature and velocity… (more)

Subjects/Keywords: Spectroscopy; Liaser-based diagnostics; Supersonic combustion engines

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APA (6th Edition):

Wittig, S. (2011). Diode-Laser-Based Velocity and Temperature Measurements from Subsonic to Hypersonic Flow Regimes. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/53659 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12354/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Wittig, Sven. “Diode-Laser-Based Velocity and Temperature Measurements from Subsonic to Hypersonic Flow Regimes.” 2011. Doctoral Dissertation, University of New South Wales. Accessed January 24, 2020. http://handle.unsw.edu.au/1959.4/53659 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12354/SOURCE01?view=true.

MLA Handbook (7th Edition):

Wittig, Sven. “Diode-Laser-Based Velocity and Temperature Measurements from Subsonic to Hypersonic Flow Regimes.” 2011. Web. 24 Jan 2020.

Vancouver:

Wittig S. Diode-Laser-Based Velocity and Temperature Measurements from Subsonic to Hypersonic Flow Regimes. [Internet] [Doctoral dissertation]. University of New South Wales; 2011. [cited 2020 Jan 24]. Available from: http://handle.unsw.edu.au/1959.4/53659 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12354/SOURCE01?view=true.

Council of Science Editors:

Wittig S. Diode-Laser-Based Velocity and Temperature Measurements from Subsonic to Hypersonic Flow Regimes. [Doctoral Dissertation]. University of New South Wales; 2011. Available from: http://handle.unsw.edu.au/1959.4/53659 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12354/SOURCE01?view=true


University of New South Wales

30. Schomberg, Kyll. Design of rocket nozzle contours using conjugate circular arcs.

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

 The use of conjugate circular arcs in rocket nozzle design has been investigated by achieving three research aims: the outline of a clear arc-based design… (more)

Subjects/Keywords: Contour design; Rocket nozzle; Supersonic flow

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

APA (6th Edition):

Schomberg, K. (2018). Design of rocket nozzle contours using conjugate circular arcs. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/61691 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:56805/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Schomberg, Kyll. “Design of rocket nozzle contours using conjugate circular arcs.” 2018. Doctoral Dissertation, University of New South Wales. Accessed January 24, 2020. http://handle.unsw.edu.au/1959.4/61691 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:56805/SOURCE02?view=true.

MLA Handbook (7th Edition):

Schomberg, Kyll. “Design of rocket nozzle contours using conjugate circular arcs.” 2018. Web. 24 Jan 2020.

Vancouver:

Schomberg K. Design of rocket nozzle contours using conjugate circular arcs. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2020 Jan 24]. Available from: http://handle.unsw.edu.au/1959.4/61691 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:56805/SOURCE02?view=true.

Council of Science Editors:

Schomberg K. Design of rocket nozzle contours using conjugate circular arcs. [Doctoral Dissertation]. University of New South Wales; 2018. Available from: http://handle.unsw.edu.au/1959.4/61691 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:56805/SOURCE02?view=true

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