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You searched for subject:(AEROTHERMODYNAMICS). Showing records 1 – 30 of 58 total matches.

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University of New South Wales

1. Khraibut, Amna. Laminar Hypersonic Leading Edge Separation.

Degree: Engineering & Information Technology, 2018, University of New South Wales

 A numerical and analytical investigation of hypersonic leading edge separation has been conducted. This particular configuration was first analyzed by Chapman in the 1950s for… (more)

Subjects/Keywords: flow separation; hypersonic flows; aerothermodynamics

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APA (6th Edition):

Khraibut, A. (2018). Laminar Hypersonic Leading Edge Separation. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/59808 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:49842/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Khraibut, Amna. “Laminar Hypersonic Leading Edge Separation.” 2018. Doctoral Dissertation, University of New South Wales. Accessed January 20, 2020. http://handle.unsw.edu.au/1959.4/59808 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:49842/SOURCE01?view=true.

MLA Handbook (7th Edition):

Khraibut, Amna. “Laminar Hypersonic Leading Edge Separation.” 2018. Web. 20 Jan 2020.

Vancouver:

Khraibut A. Laminar Hypersonic Leading Edge Separation. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2020 Jan 20]. Available from: http://handle.unsw.edu.au/1959.4/59808 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:49842/SOURCE01?view=true.

Council of Science Editors:

Khraibut A. Laminar Hypersonic Leading Edge Separation. [Doctoral Dissertation]. University of New South Wales; 2018. Available from: http://handle.unsw.edu.au/1959.4/59808 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:49842/SOURCE01?view=true


University of New South Wales

2. Park, Gisu. Hypervelocity aerothermodynamics of blunt bodies including real gas effects.

Degree: Engineering & Information Technology, 2010, University of New South Wales

 Hypervelocity aerothermodynamics of blunt bodies such as a circular cylinder and a 45◦ half-angle blunted cone have been investigated experimentally, analytically, and numerically. Particular emphasis… (more)

Subjects/Keywords: Real gas effects; Hypervelocity aerothermodynamics; Blunt bodies; Aerothermodynamics

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APA (6th Edition):

Park, G. (2010). Hypervelocity aerothermodynamics of blunt bodies including real gas effects. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/45698 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8980/SOURCE1?view=true

Chicago Manual of Style (16th Edition):

Park, Gisu. “Hypervelocity aerothermodynamics of blunt bodies including real gas effects.” 2010. Doctoral Dissertation, University of New South Wales. Accessed January 20, 2020. http://handle.unsw.edu.au/1959.4/45698 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8980/SOURCE1?view=true.

MLA Handbook (7th Edition):

Park, Gisu. “Hypervelocity aerothermodynamics of blunt bodies including real gas effects.” 2010. Web. 20 Jan 2020.

Vancouver:

Park G. Hypervelocity aerothermodynamics of blunt bodies including real gas effects. [Internet] [Doctoral dissertation]. University of New South Wales; 2010. [cited 2020 Jan 20]. Available from: http://handle.unsw.edu.au/1959.4/45698 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8980/SOURCE1?view=true.

Council of Science Editors:

Park G. Hypervelocity aerothermodynamics of blunt bodies including real gas effects. [Doctoral Dissertation]. University of New South Wales; 2010. Available from: http://handle.unsw.edu.au/1959.4/45698 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8980/SOURCE1?view=true


University of Minnesota

3. Kirk, Lindsay Christine. Geometric effects on the amplification of first mode instability waves.

Degree: MS, Aerospace Engineering and Mechanics, 2013, University of Minnesota

University of Minnesota M.S. thesis. May 2013. Major: Aerospace Engineering and Mechanics. Advisor: Graham V. Candler. 1 computer file (PDF); vii, 54 pages, appendix A.… (more)

Subjects/Keywords: Aerothermodynamics; Boundary layer stability; First mode; Hypersonic; Supersonic

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APA (6th Edition):

Kirk, L. C. (2013). Geometric effects on the amplification of first mode instability waves. (Masters Thesis). University of Minnesota. Retrieved from http://purl.umn.edu/156851

Chicago Manual of Style (16th Edition):

Kirk, Lindsay Christine. “Geometric effects on the amplification of first mode instability waves.” 2013. Masters Thesis, University of Minnesota. Accessed January 20, 2020. http://purl.umn.edu/156851.

MLA Handbook (7th Edition):

Kirk, Lindsay Christine. “Geometric effects on the amplification of first mode instability waves.” 2013. Web. 20 Jan 2020.

Vancouver:

Kirk LC. Geometric effects on the amplification of first mode instability waves. [Internet] [Masters thesis]. University of Minnesota; 2013. [cited 2020 Jan 20]. Available from: http://purl.umn.edu/156851.

Council of Science Editors:

Kirk LC. Geometric effects on the amplification of first mode instability waves. [Masters Thesis]. University of Minnesota; 2013. Available from: http://purl.umn.edu/156851


University of Minnesota

4. Kirk, Lindsay Christine. Geometric effects on the amplification of first mode instability waves.

Degree: MS, Aerospace Engineering and Mechanics, 2013, University of Minnesota

 The effects of geometric changes on the amplification of first mode instability waves in an external supersonic boundary layer were investigated using numerical techniques. Boundary… (more)

Subjects/Keywords: Aerothermodynamics; Boundary layer stability; First mode; Hypersonic; Supersonic

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APA (6th Edition):

Kirk, L. C. (2013). Geometric effects on the amplification of first mode instability waves. (Masters Thesis). University of Minnesota. Retrieved from http://purl.umn.edu/156851

Chicago Manual of Style (16th Edition):

Kirk, Lindsay Christine. “Geometric effects on the amplification of first mode instability waves.” 2013. Masters Thesis, University of Minnesota. Accessed January 20, 2020. http://purl.umn.edu/156851.

MLA Handbook (7th Edition):

Kirk, Lindsay Christine. “Geometric effects on the amplification of first mode instability waves.” 2013. Web. 20 Jan 2020.

Vancouver:

Kirk LC. Geometric effects on the amplification of first mode instability waves. [Internet] [Masters thesis]. University of Minnesota; 2013. [cited 2020 Jan 20]. Available from: http://purl.umn.edu/156851.

Council of Science Editors:

Kirk LC. Geometric effects on the amplification of first mode instability waves. [Masters Thesis]. University of Minnesota; 2013. Available from: http://purl.umn.edu/156851


Ryerson University

5. Miri, Seyed Hossein. Shock-less Hypersonic Intakes.

Degree: 2012, Ryerson University

 The accuracy of CFD for simulating hypersonic air intake flow is verified by calculating the flow inside a Busemann type intake. The CFD results are… (more)

Subjects/Keywords: Aerodynamics; Hypersonic; Aerothermodynamics; Aerodynamics; Hypersonic  – Mathematics; Aerodynamics; Hypersonic  – Mathematical models

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APA (6th Edition):

Miri, S. H. (2012). Shock-less Hypersonic Intakes. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1565

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):

Miri, Seyed Hossein. “Shock-less Hypersonic Intakes.” 2012. Thesis, Ryerson University. Accessed January 20, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A1565.

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

MLA Handbook (7th Edition):

Miri, Seyed Hossein. “Shock-less Hypersonic Intakes.” 2012. Web. 20 Jan 2020.

Vancouver:

Miri SH. Shock-less Hypersonic Intakes. [Internet] [Thesis]. Ryerson University; 2012. [cited 2020 Jan 20]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1565.

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

Council of Science Editors:

Miri SH. Shock-less Hypersonic Intakes. [Thesis]. Ryerson University; 2012. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1565

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


Virginia Tech

6. Studebaker, Karen F. Probalistic vibration analysis of nearly periodic structures.

Degree: MS, Aerospace Engineering, 1988, Virginia Tech

 The localization of modes of nearly periodic structures causes a concentration of energy in one part of the mode shape. It occurs for a disordered… (more)

Subjects/Keywords: Aerothermodynamics; LD5655.V855 1988.S893

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APA (6th Edition):

Studebaker, K. F. (1988). Probalistic vibration analysis of nearly periodic structures. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/44087

Chicago Manual of Style (16th Edition):

Studebaker, Karen F. “Probalistic vibration analysis of nearly periodic structures.” 1988. Masters Thesis, Virginia Tech. Accessed January 20, 2020. http://hdl.handle.net/10919/44087.

MLA Handbook (7th Edition):

Studebaker, Karen F. “Probalistic vibration analysis of nearly periodic structures.” 1988. Web. 20 Jan 2020.

Vancouver:

Studebaker KF. Probalistic vibration analysis of nearly periodic structures. [Internet] [Masters thesis]. Virginia Tech; 1988. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/10919/44087.

Council of Science Editors:

Studebaker KF. Probalistic vibration analysis of nearly periodic structures. [Masters Thesis]. Virginia Tech; 1988. Available from: http://hdl.handle.net/10919/44087


Virginia Tech

7. MacKay, James D. Analytical method for turbine blade temperature mapping to estimate a pyrometer input signal.

Degree: MS, Mechanical Engineering, 1987, Virginia Tech

  The purpose of this thesis is to develop a method to estimate local blade temperatures in a gas turbine for comparison with the output… (more)

Subjects/Keywords: Aerothermodynamics; LD5655.V855 1987.M334

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APA (6th Edition):

MacKay, J. D. (1987). Analytical method for turbine blade temperature mapping to estimate a pyrometer input signal. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45797

Chicago Manual of Style (16th Edition):

MacKay, James D. “Analytical method for turbine blade temperature mapping to estimate a pyrometer input signal.” 1987. Masters Thesis, Virginia Tech. Accessed January 20, 2020. http://hdl.handle.net/10919/45797.

MLA Handbook (7th Edition):

MacKay, James D. “Analytical method for turbine blade temperature mapping to estimate a pyrometer input signal.” 1987. Web. 20 Jan 2020.

Vancouver:

MacKay JD. Analytical method for turbine blade temperature mapping to estimate a pyrometer input signal. [Internet] [Masters thesis]. Virginia Tech; 1987. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/10919/45797.

Council of Science Editors:

MacKay JD. Analytical method for turbine blade temperature mapping to estimate a pyrometer input signal. [Masters Thesis]. Virginia Tech; 1987. Available from: http://hdl.handle.net/10919/45797


University of Arizona

8. Coon, Carlos Weldon, 1938-. THE TRANSITION FROM THE TURBULENT TO THE LAMINAR REGIME FOR INTERNAL CONVECTIVE FLOW WITH LARGE PROPERTY VARIATIONS .

Degree: 1968, University of Arizona

Subjects/Keywords: Aerothermodynamics.; Turbulence.; Laminar flow.

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APA (6th Edition):

Coon, Carlos Weldon, 1. (1968). THE TRANSITION FROM THE TURBULENT TO THE LAMINAR REGIME FOR INTERNAL CONVECTIVE FLOW WITH LARGE PROPERTY VARIATIONS . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/284994

Chicago Manual of Style (16th Edition):

Coon, Carlos Weldon, 1938-. “THE TRANSITION FROM THE TURBULENT TO THE LAMINAR REGIME FOR INTERNAL CONVECTIVE FLOW WITH LARGE PROPERTY VARIATIONS .” 1968. Doctoral Dissertation, University of Arizona. Accessed January 20, 2020. http://hdl.handle.net/10150/284994.

MLA Handbook (7th Edition):

Coon, Carlos Weldon, 1938-. “THE TRANSITION FROM THE TURBULENT TO THE LAMINAR REGIME FOR INTERNAL CONVECTIVE FLOW WITH LARGE PROPERTY VARIATIONS .” 1968. Web. 20 Jan 2020.

Vancouver:

Coon, Carlos Weldon 1. THE TRANSITION FROM THE TURBULENT TO THE LAMINAR REGIME FOR INTERNAL CONVECTIVE FLOW WITH LARGE PROPERTY VARIATIONS . [Internet] [Doctoral dissertation]. University of Arizona; 1968. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/10150/284994.

Council of Science Editors:

Coon, Carlos Weldon 1. THE TRANSITION FROM THE TURBULENT TO THE LAMINAR REGIME FOR INTERNAL CONVECTIVE FLOW WITH LARGE PROPERTY VARIATIONS . [Doctoral Dissertation]. University of Arizona; 1968. Available from: http://hdl.handle.net/10150/284994


University of Oklahoma

9. Roland, Jay Roy. Time asymptotic determination of the effects of ablation-product absorption coefficient enhancement on the mass loss rate from the stagnation point of a blunt body in the massive blowing regime.

Degree: PhD, 1972, University of Oklahoma

Subjects/Keywords: Ablation (Aerothermodynamics); Engineering, Aerospace.

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APA (6th Edition):

Roland, J. R. (1972). Time asymptotic determination of the effects of ablation-product absorption coefficient enhancement on the mass loss rate from the stagnation point of a blunt body in the massive blowing regime. (Doctoral Dissertation). University of Oklahoma. Retrieved from http://hdl.handle.net/11244/3444

Chicago Manual of Style (16th Edition):

Roland, Jay Roy. “Time asymptotic determination of the effects of ablation-product absorption coefficient enhancement on the mass loss rate from the stagnation point of a blunt body in the massive blowing regime.” 1972. Doctoral Dissertation, University of Oklahoma. Accessed January 20, 2020. http://hdl.handle.net/11244/3444.

MLA Handbook (7th Edition):

Roland, Jay Roy. “Time asymptotic determination of the effects of ablation-product absorption coefficient enhancement on the mass loss rate from the stagnation point of a blunt body in the massive blowing regime.” 1972. Web. 20 Jan 2020.

Vancouver:

Roland JR. Time asymptotic determination of the effects of ablation-product absorption coefficient enhancement on the mass loss rate from the stagnation point of a blunt body in the massive blowing regime. [Internet] [Doctoral dissertation]. University of Oklahoma; 1972. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/11244/3444.

Council of Science Editors:

Roland JR. Time asymptotic determination of the effects of ablation-product absorption coefficient enhancement on the mass loss rate from the stagnation point of a blunt body in the massive blowing regime. [Doctoral Dissertation]. University of Oklahoma; 1972. Available from: http://hdl.handle.net/11244/3444


Georgia Tech

10. Reynoso, Francisco J. Modeling of near infrared laser-mediated plasmonic heating with optically tunable gold nanoparticles for thermal therapy.

Degree: MS, Mechanical Engineering, 2011, Georgia Tech

 Clinical hyperthermia refers to treatment of tumors by heating the lesions between 40 and 45° C. Several clinical trials have demonstrated that hyperthermia provides significant… (more)

Subjects/Keywords: Thermal ablation; Computational; Heat Physiological effect; Nanoparticles; Ablation (Aerothermodynamics)

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APA (6th Edition):

Reynoso, F. J. (2011). Modeling of near infrared laser-mediated plasmonic heating with optically tunable gold nanoparticles for thermal therapy. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/45966

Chicago Manual of Style (16th Edition):

Reynoso, Francisco J. “Modeling of near infrared laser-mediated plasmonic heating with optically tunable gold nanoparticles for thermal therapy.” 2011. Masters Thesis, Georgia Tech. Accessed January 20, 2020. http://hdl.handle.net/1853/45966.

MLA Handbook (7th Edition):

Reynoso, Francisco J. “Modeling of near infrared laser-mediated plasmonic heating with optically tunable gold nanoparticles for thermal therapy.” 2011. Web. 20 Jan 2020.

Vancouver:

Reynoso FJ. Modeling of near infrared laser-mediated plasmonic heating with optically tunable gold nanoparticles for thermal therapy. [Internet] [Masters thesis]. Georgia Tech; 2011. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/1853/45966.

Council of Science Editors:

Reynoso FJ. Modeling of near infrared laser-mediated plasmonic heating with optically tunable gold nanoparticles for thermal therapy. [Masters Thesis]. Georgia Tech; 2011. Available from: http://hdl.handle.net/1853/45966


Portland State University

11. Hoffman, Matthew James. Spatial and Temporal Variability of Glacier Melt in the McMurdo Dry Valleys, Antarctica.

Degree: PhD, Geology, 2011, Portland State University

  In the McMurdo Dry Valleys, Victoria Land, East Antarctica, melting of glacial ice is the primary source of water to streams, lakes, and associated… (more)

Subjects/Keywords: Meltwater  – Antarctica  – McMurdo Dry Valleys; Glaciers  – Antarctica  – McMurdo Dry Valleys; Ablation (Aerothermodynamics)

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APA (6th Edition):

Hoffman, M. J. (2011). Spatial and Temporal Variability of Glacier Melt in the McMurdo Dry Valleys, Antarctica. (Doctoral Dissertation). Portland State University. Retrieved from http://pdxscholar.library.pdx.edu/open_access_etds/744

Chicago Manual of Style (16th Edition):

Hoffman, Matthew James. “Spatial and Temporal Variability of Glacier Melt in the McMurdo Dry Valleys, Antarctica.” 2011. Doctoral Dissertation, Portland State University. Accessed January 20, 2020. http://pdxscholar.library.pdx.edu/open_access_etds/744.

MLA Handbook (7th Edition):

Hoffman, Matthew James. “Spatial and Temporal Variability of Glacier Melt in the McMurdo Dry Valleys, Antarctica.” 2011. Web. 20 Jan 2020.

Vancouver:

Hoffman MJ. Spatial and Temporal Variability of Glacier Melt in the McMurdo Dry Valleys, Antarctica. [Internet] [Doctoral dissertation]. Portland State University; 2011. [cited 2020 Jan 20]. Available from: http://pdxscholar.library.pdx.edu/open_access_etds/744.

Council of Science Editors:

Hoffman MJ. Spatial and Temporal Variability of Glacier Melt in the McMurdo Dry Valleys, Antarctica. [Doctoral Dissertation]. Portland State University; 2011. Available from: http://pdxscholar.library.pdx.edu/open_access_etds/744


University of Kansas

12. Underwood, Sean Christopher. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.

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

 The service life of gas turbine engine turbine blades depends on the blade’s material, service temperature and total stress. In high-performance gas turbines, film cooling… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Aerothermodynamics; Film Cooling; Gas Turbine; Impingement Cooling; Propulsion; Turbine Blade Cooling

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APA (6th Edition):

Underwood, S. C. (2018). Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/27605

Chicago Manual of Style (16th Edition):

Underwood, Sean Christopher. “Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.” 2018. Doctoral Dissertation, University of Kansas. Accessed January 20, 2020. http://hdl.handle.net/1808/27605.

MLA Handbook (7th Edition):

Underwood, Sean Christopher. “Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.” 2018. Web. 20 Jan 2020.

Vancouver:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/1808/27605.

Council of Science Editors:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Doctoral Dissertation]. University of Kansas; 2018. Available from: http://hdl.handle.net/1808/27605


University of Washington

13. Drabiak, Daniel Robert. Modeling of Test Section Conditions in a High Enthalpy Flow Facility.

Degree: 2017, University of Washington

 The Shock Wave Reactor laboratory, or SWR, at the University of Washington is a high enthalpy flow facility capable of a wide range of test… (more)

Subjects/Keywords: Aerodynamics; Aerothermodynamics; Heat Transfer; Modeling; Shock; Thermodynamics; Aerospace engineering; Aeronautics and astronautics

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APA (6th Edition):

Drabiak, D. R. (2017). Modeling of Test Section Conditions in a High Enthalpy Flow Facility. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/40469

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):

Drabiak, Daniel Robert. “Modeling of Test Section Conditions in a High Enthalpy Flow Facility.” 2017. Thesis, University of Washington. Accessed January 20, 2020. http://hdl.handle.net/1773/40469.

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

MLA Handbook (7th Edition):

Drabiak, Daniel Robert. “Modeling of Test Section Conditions in a High Enthalpy Flow Facility.” 2017. Web. 20 Jan 2020.

Vancouver:

Drabiak DR. Modeling of Test Section Conditions in a High Enthalpy Flow Facility. [Internet] [Thesis]. University of Washington; 2017. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/1773/40469.

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

Council of Science Editors:

Drabiak DR. Modeling of Test Section Conditions in a High Enthalpy Flow Facility. [Thesis]. University of Washington; 2017. Available from: http://hdl.handle.net/1773/40469

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


The Ohio State University

14. Haering, George William. Boundary layer separation control and wall temperature control by tangential fluid injection.

Degree: PhD, Graduate School, 1968, The Ohio State University

Subjects/Keywords: Engineering; High-speed aeronautics; Boundary layer; Aerothermodynamics

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APA (6th Edition):

Haering, G. W. (1968). Boundary layer separation control and wall temperature control by tangential fluid injection. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1486647415490311

Chicago Manual of Style (16th Edition):

Haering, George William. “Boundary layer separation control and wall temperature control by tangential fluid injection.” 1968. Doctoral Dissertation, The Ohio State University. Accessed January 20, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1486647415490311.

MLA Handbook (7th Edition):

Haering, George William. “Boundary layer separation control and wall temperature control by tangential fluid injection.” 1968. Web. 20 Jan 2020.

Vancouver:

Haering GW. Boundary layer separation control and wall temperature control by tangential fluid injection. [Internet] [Doctoral dissertation]. The Ohio State University; 1968. [cited 2020 Jan 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486647415490311.

Council of Science Editors:

Haering GW. Boundary layer separation control and wall temperature control by tangential fluid injection. [Doctoral Dissertation]. The Ohio State University; 1968. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486647415490311

15. Silvanio Bezerra de Oliveira. Fragmentação por ação aerotermodinâmica e predição da área de impacto de um veículo espacial com injeção controlada da re-entrada.

Degree: 2009, Instituto Nacional de Pesquisas Espaciais

Este trabalho consiste em estudar a fragmentação por ação aerotermodinâmica durante re-entrada de um veículo espacial, com estimativa da área de impacto dos fragmentos na… (more)

Subjects/Keywords: transferência ótima; fragmentação atmosférica; dinâmica da fratura; aerotermodinâmica; orbital decay; optimal transfer; atmospheric fragmentation; fracture dynamics; aerothermodynamics; decaimento orbital

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APA (6th Edition):

Oliveira, S. B. d. (2009). Fragmentação por ação aerotermodinâmica e predição da área de impacto de um veículo espacial com injeção controlada da re-entrada. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2009/07.23.15.26

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):

Oliveira, Silvanio Bezerra de. “Fragmentação por ação aerotermodinâmica e predição da área de impacto de um veículo espacial com injeção controlada da re-entrada.” 2009. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed January 20, 2020. http://urlib.net/sid.inpe.br/[email protected]/2009/07.23.15.26.

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

MLA Handbook (7th Edition):

Oliveira, Silvanio Bezerra de. “Fragmentação por ação aerotermodinâmica e predição da área de impacto de um veículo espacial com injeção controlada da re-entrada.” 2009. Web. 20 Jan 2020.

Vancouver:

Oliveira SBd. Fragmentação por ação aerotermodinâmica e predição da área de impacto de um veículo espacial com injeção controlada da re-entrada. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. [cited 2020 Jan 20]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/07.23.15.26.

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

Council of Science Editors:

Oliveira SBd. Fragmentação por ação aerotermodinâmica e predição da área de impacto de um veículo espacial com injeção controlada da re-entrada. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/07.23.15.26

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


Purdue University

16. Luo, Han. Ab initio based State Specific Modeling of N2+O System.

Degree: MSin Aeronautics and Astronautics, Aeronautics and Astronautics, 2016, Purdue University

  Nitrogen and atomic oxygen play an important role in high temperature gas systems. Their Zeldovich reaction product nitric oxide not only affects aerothermal loads… (more)

Subjects/Keywords: Pure sciences; Applied sciences; Dsmc; Hypersonic aerothermodynamics; Nonequilibrium reacting flow; Qct; State-specic modeling; Aerospace Engineering; Chemistry

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APA (6th Edition):

Luo, H. (2016). Ab initio based State Specific Modeling of N2+O System. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/958

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):

Luo, Han. “Ab initio based State Specific Modeling of N2+O System.” 2016. Thesis, Purdue University. Accessed January 20, 2020. https://docs.lib.purdue.edu/open_access_theses/958.

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

MLA Handbook (7th Edition):

Luo, Han. “Ab initio based State Specific Modeling of N2+O System.” 2016. Web. 20 Jan 2020.

Vancouver:

Luo H. Ab initio based State Specific Modeling of N2+O System. [Internet] [Thesis]. Purdue University; 2016. [cited 2020 Jan 20]. Available from: https://docs.lib.purdue.edu/open_access_theses/958.

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

Council of Science Editors:

Luo H. Ab initio based State Specific Modeling of N2+O System. [Thesis]. Purdue University; 2016. Available from: https://docs.lib.purdue.edu/open_access_theses/958

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


University of KwaZulu-Natal

17. [No author]. An experimental and numerical convective heat transfer analysis over a transonic gas turbine rotor blade.

Degree: Mechanical engineering, 2006, University of KwaZulu-Natal

 An experimental and numerical investigation of the flow and convective heat transfer distribution around a high turning angle gas turbine rotor blade has been carried… (more)

Subjects/Keywords: Mechanical engineering.; Turbines – Blades.; Aerothermodynamics.; Gas-turbines.

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APA (6th Edition):

author], [. (2006). An experimental and numerical convective heat transfer analysis over a transonic gas turbine rotor blade. (Thesis). University of KwaZulu-Natal. Retrieved from http://hdl.handle.net/10413/2222

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):

author], [No. “An experimental and numerical convective heat transfer analysis over a transonic gas turbine rotor blade. ” 2006. Thesis, University of KwaZulu-Natal. Accessed January 20, 2020. http://hdl.handle.net/10413/2222.

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

MLA Handbook (7th Edition):

author], [No. “An experimental and numerical convective heat transfer analysis over a transonic gas turbine rotor blade. ” 2006. Web. 20 Jan 2020.

Vancouver:

author] [. An experimental and numerical convective heat transfer analysis over a transonic gas turbine rotor blade. [Internet] [Thesis]. University of KwaZulu-Natal; 2006. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/10413/2222.

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

Council of Science Editors:

author] [. An experimental and numerical convective heat transfer analysis over a transonic gas turbine rotor blade. [Thesis]. University of KwaZulu-Natal; 2006. Available from: http://hdl.handle.net/10413/2222

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

18. Boyd, Daniel A. Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle.

Degree: MS, Mechanical & Aerospace Engineering, 2018, Old Dominion University

  Because of the severe quarantine constraints that must be imposed on any returned extraterrestrial samples, the Mars sample return Earth-entry vehicle must remain intact… (more)

Subjects/Keywords: Aerothermodynamics; Convective heating; Heat flux; LAURA; Mars sample; Radiative heating; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Space Vehicles; Thermodynamics

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APA (6th Edition):

Boyd, D. A. (2018). Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle. (Thesis). Old Dominion University. Retrieved from 9780438538399 ; https://digitalcommons.odu.edu/mae_etds/43

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):

Boyd, Daniel A. “Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle.” 2018. Thesis, Old Dominion University. Accessed January 20, 2020. 9780438538399 ; https://digitalcommons.odu.edu/mae_etds/43.

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

MLA Handbook (7th Edition):

Boyd, Daniel A. “Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle.” 2018. Web. 20 Jan 2020.

Vancouver:

Boyd DA. Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle. [Internet] [Thesis]. Old Dominion University; 2018. [cited 2020 Jan 20]. Available from: 9780438538399 ; https://digitalcommons.odu.edu/mae_etds/43.

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

Council of Science Editors:

Boyd DA. Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle. [Thesis]. Old Dominion University; 2018. Available from: 9780438538399 ; https://digitalcommons.odu.edu/mae_etds/43

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


McGill University

19. Adams, W. Peter. Studies of ablation and run-off on an Arctic glacier.

Degree: PhD, Department of Geography., 1966, McGill University

 Ablation and run-off on the White Glacier (38 km2), Axel Heiberg Island, N.W.T., were studied during the summers 1959-61 and some comparisons were made with… (more)

Subjects/Keywords: Geography.; Glaciers  – Nunavut  – Axel Heiberg Island.; Glaciology.; Ablation (Aerothermodynamics).

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APA (6th Edition):

Adams, W. P. (1966). Studies of ablation and run-off on an Arctic glacier. (Doctoral Dissertation). McGill University. Retrieved from http://digitool.library.mcgill.ca/thesisfile118085.pdf

Chicago Manual of Style (16th Edition):

Adams, W Peter. “Studies of ablation and run-off on an Arctic glacier.” 1966. Doctoral Dissertation, McGill University. Accessed January 20, 2020. http://digitool.library.mcgill.ca/thesisfile118085.pdf.

MLA Handbook (7th Edition):

Adams, W Peter. “Studies of ablation and run-off on an Arctic glacier.” 1966. Web. 20 Jan 2020.

Vancouver:

Adams WP. Studies of ablation and run-off on an Arctic glacier. [Internet] [Doctoral dissertation]. McGill University; 1966. [cited 2020 Jan 20]. Available from: http://digitool.library.mcgill.ca/thesisfile118085.pdf.

Council of Science Editors:

Adams WP. Studies of ablation and run-off on an Arctic glacier. [Doctoral Dissertation]. McGill University; 1966. Available from: http://digitool.library.mcgill.ca/thesisfile118085.pdf

20. Prévereaud, Ysolde. Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris.

Degree: Docteur es, Dynamique des fluides et Energétique et transferts, 2014, Toulouse, ISAE

Afin de déterminer l’état dans lequel les fragments arrivent au sol et leurs points d’impact, une compréhension fine des phénomènes physiques intervenant lors de la… (more)

Subjects/Keywords: Rentrée atmosphérique; Débris spatiaux; Aérothermodynamique; Conduction; Oxydation; Ablation; Atmospheric re-Entry; Space debris; Aerothermodynamics; Conduction; Oxidation; Ablation; 532

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APA (6th Edition):

Prévereaud, Y. (2014). Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2014ESAE0021

Chicago Manual of Style (16th Edition):

Prévereaud, Ysolde. “Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris.” 2014. Doctoral Dissertation, Toulouse, ISAE. Accessed January 20, 2020. http://www.theses.fr/2014ESAE0021.

MLA Handbook (7th Edition):

Prévereaud, Ysolde. “Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris.” 2014. Web. 20 Jan 2020.

Vancouver:

Prévereaud Y. Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2014. [cited 2020 Jan 20]. Available from: http://www.theses.fr/2014ESAE0021.

Council of Science Editors:

Prévereaud Y. Contribution à la modélisation de la rentrée atmosphérique des débris spatiaux : Development of models for the atmospheric re-entry of space debris. [Doctoral Dissertation]. Toulouse, ISAE; 2014. Available from: http://www.theses.fr/2014ESAE0021


Virginia Tech

21. O'Hare, Brian J. An analysis of the spallation of carbon phenolic ablators.

Degree: MS, Aerospace Engineering, 1967, Virginia Tech

Subjects/Keywords: LD5655.V855 1967.O32; Spallation (Nuclear physics); Ablation (Aerothermodynamics)

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APA (6th Edition):

O'Hare, B. J. (1967). An analysis of the spallation of carbon phenolic ablators. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71204

Chicago Manual of Style (16th Edition):

O'Hare, Brian J. “An analysis of the spallation of carbon phenolic ablators.” 1967. Masters Thesis, Virginia Tech. Accessed January 20, 2020. http://hdl.handle.net/10919/71204.

MLA Handbook (7th Edition):

O'Hare, Brian J. “An analysis of the spallation of carbon phenolic ablators.” 1967. Web. 20 Jan 2020.

Vancouver:

O'Hare BJ. An analysis of the spallation of carbon phenolic ablators. [Internet] [Masters thesis]. Virginia Tech; 1967. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/10919/71204.

Council of Science Editors:

O'Hare BJ. An analysis of the spallation of carbon phenolic ablators. [Masters Thesis]. Virginia Tech; 1967. Available from: http://hdl.handle.net/10919/71204


Virginia Tech

22. Song, Dong Joo. Hypersonic nonequilibrium flow over an ablating teflon surface.

Degree: PhD, Aerospace Engineering, 1986, Virginia Tech

Subjects/Keywords: LD5655.V856 1986.S663; Aerodynamics, Hypersonic; Ablation (Aerothermodynamics)

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APA (6th Edition):

Song, D. J. (1986). Hypersonic nonequilibrium flow over an ablating teflon surface. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71192

Chicago Manual of Style (16th Edition):

Song, Dong Joo. “Hypersonic nonequilibrium flow over an ablating teflon surface.” 1986. Doctoral Dissertation, Virginia Tech. Accessed January 20, 2020. http://hdl.handle.net/10919/71192.

MLA Handbook (7th Edition):

Song, Dong Joo. “Hypersonic nonequilibrium flow over an ablating teflon surface.” 1986. Web. 20 Jan 2020.

Vancouver:

Song DJ. Hypersonic nonequilibrium flow over an ablating teflon surface. [Internet] [Doctoral dissertation]. Virginia Tech; 1986. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/10919/71192.

Council of Science Editors:

Song DJ. Hypersonic nonequilibrium flow over an ablating teflon surface. [Doctoral Dissertation]. Virginia Tech; 1986. Available from: http://hdl.handle.net/10919/71192


Stellenbosch University

23. Van Rooyen, J. A. Performance trends of an air-cooled steam condenser under windy conditions.

Degree: Mechanical and Mechatronic Engineering, 2007, Stellenbosch University

Thesis (MScEng (Mechanical and Mechatronic Engineering)) – University of Stellenbosch, 2007.

Air-cooled steam condensers (ACSC’s) are increasingly employed to reject heat in modern power plants. Unfortunately… (more)

Subjects/Keywords: Mechanical engineering; Condensers (Steam); Aerothermodynamics; Mechanical and Mechatronic Engineering

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APA (6th Edition):

Van Rooyen, J. A. (2007). Performance trends of an air-cooled steam condenser under windy conditions. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/1629

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):

Van Rooyen, J A. “Performance trends of an air-cooled steam condenser under windy conditions.” 2007. Thesis, Stellenbosch University. Accessed January 20, 2020. http://hdl.handle.net/10019.1/1629.

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

MLA Handbook (7th Edition):

Van Rooyen, J A. “Performance trends of an air-cooled steam condenser under windy conditions.” 2007. Web. 20 Jan 2020.

Vancouver:

Van Rooyen JA. Performance trends of an air-cooled steam condenser under windy conditions. [Internet] [Thesis]. Stellenbosch University; 2007. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/10019.1/1629.

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

Council of Science Editors:

Van Rooyen JA. Performance trends of an air-cooled steam condenser under windy conditions. [Thesis]. Stellenbosch University; 2007. Available from: http://hdl.handle.net/10019.1/1629

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


University of Oklahoma

24. Merliss, Frederick E. Molecular diffusion coefficients in aqueous binary solutions.

Degree: PhD, 1967, University of Oklahoma

Subjects/Keywords: Ablation (Aerothermodynamics); Engineering, Chemical.; Mass transfer.; Diffusion.

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APA (6th Edition):

Merliss, F. E. (1967). Molecular diffusion coefficients in aqueous binary solutions. (Doctoral Dissertation). University of Oklahoma. Retrieved from http://hdl.handle.net/11244/2291

Chicago Manual of Style (16th Edition):

Merliss, Frederick E. “Molecular diffusion coefficients in aqueous binary solutions.” 1967. Doctoral Dissertation, University of Oklahoma. Accessed January 20, 2020. http://hdl.handle.net/11244/2291.

MLA Handbook (7th Edition):

Merliss, Frederick E. “Molecular diffusion coefficients in aqueous binary solutions.” 1967. Web. 20 Jan 2020.

Vancouver:

Merliss FE. Molecular diffusion coefficients in aqueous binary solutions. [Internet] [Doctoral dissertation]. University of Oklahoma; 1967. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/11244/2291.

Council of Science Editors:

Merliss FE. Molecular diffusion coefficients in aqueous binary solutions. [Doctoral Dissertation]. University of Oklahoma; 1967. Available from: http://hdl.handle.net/11244/2291

25. Ferrier, Loïc. Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid.

Degree: Docteur es, Dynamiques des fluides, 2012, Toulouse, ISAE

Quotidiennement, des objets orbitant à proximité de la Terre (ou géocroiseurs) impactent cette dernière. Lorsque la dimension de l'objet atteint une taille critique (autour de… (more)

Subjects/Keywords: Hypersonique; Trajectographie; Aérothermodynamique; Entrée atmosphérique; Géocroiseurs; Rayonnement; Ablation; Fragmentation; Hypersonic; Trajectography; AeroThermoDynamics; Atmospheric Entry; NEOs; Radiation; Ablation; Fragmentation; 532

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APA (6th Edition):

Ferrier, L. (2012). Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2012ESAE0017

Chicago Manual of Style (16th Edition):

Ferrier, Loïc. “Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid.” 2012. Doctoral Dissertation, Toulouse, ISAE. Accessed January 20, 2020. http://www.theses.fr/2012ESAE0017.

MLA Handbook (7th Edition):

Ferrier, Loïc. “Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid.” 2012. Web. 20 Jan 2020.

Vancouver:

Ferrier L. Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2012. [cited 2020 Jan 20]. Available from: http://www.theses.fr/2012ESAE0017.

Council of Science Editors:

Ferrier L. Analyse aérothermodynamique de l'entrée atmosphérique d'un géocroiseur à occurence séculaire : AeroThermoDynamics analysis of the atmospheric entry of a secular asteroid. [Doctoral Dissertation]. Toulouse, ISAE; 2012. Available from: http://www.theses.fr/2012ESAE0017

26. Scoggins, James. Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry.

Degree: Docteur es, Énergétique, 2017, Paris Saclay

Cette thèse est centrée sur le couplage entre les phénomènes d’écoulement, d’ablation et de rayonnement au voisinage du point d’arrêt de véhicules d’entrée atmosphérique pourvus… (more)

Subjects/Keywords: Entrée atmosphérique; Hypersonique; Aerothermodynamique; Rayonnement; Ablation; Équilibre multiphase; Atmospheric entry; Hypersonics; Aerothermodynamics; Radiation; Ablation; Coupling; Multiphase equilibrium

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APA (6th Edition):

Scoggins, J. (2017). Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry. (Doctoral Dissertation). Paris Saclay. Retrieved from http://www.theses.fr/2017SACLC048

Chicago Manual of Style (16th Edition):

Scoggins, James. “Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry.” 2017. Doctoral Dissertation, Paris Saclay. Accessed January 20, 2020. http://www.theses.fr/2017SACLC048.

MLA Handbook (7th Edition):

Scoggins, James. “Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry.” 2017. Web. 20 Jan 2020.

Vancouver:

Scoggins J. Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry. [Internet] [Doctoral dissertation]. Paris Saclay; 2017. [cited 2020 Jan 20]. Available from: http://www.theses.fr/2017SACLC048.

Council of Science Editors:

Scoggins J. Développement de méthodes numériques et étude des phénomènes couplés d’écoulement, de rayonnement, et d’ablation dans les problèmes d’entrée atmosphérique : Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry. [Doctoral Dissertation]. Paris Saclay; 2017. Available from: http://www.theses.fr/2017SACLC048


University of Michigan

27. Farbar, Erin D. Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields.

Degree: PhD, Aerospace Engineering, 2010, University of Michigan

 When a vehicle enters the Earth's atmosphere at the very large velocities associated with Lunar and Mars return, a strong bow shock is formed in… (more)

Subjects/Keywords: Direct Simulation Monte Carlo; Nonequilibrium Flow; Reentry Flow; Rarefied Gas Dynamics; Weakly Ionized Plasma; Hypersonic Aerothermodynamics; Aerospace Engineering; Engineering

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APA (6th Edition):

Farbar, E. D. (2010). Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/78779

Chicago Manual of Style (16th Edition):

Farbar, Erin D. “Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields.” 2010. Doctoral Dissertation, University of Michigan. Accessed January 20, 2020. http://hdl.handle.net/2027.42/78779.

MLA Handbook (7th Edition):

Farbar, Erin D. “Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields.” 2010. Web. 20 Jan 2020.

Vancouver:

Farbar ED. Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields. [Internet] [Doctoral dissertation]. University of Michigan; 2010. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/2027.42/78779.

Council of Science Editors:

Farbar ED. Kinetic Simulation of Rarefied and Weakly Ionized Hypersonic Flow Fields. [Doctoral Dissertation]. University of Michigan; 2010. Available from: http://hdl.handle.net/2027.42/78779


Michigan State University

28. Pawlowski, Conrad Matthew. In situ laser ablation deposition of YBa2Cu3O7-X thin films using a microwave plasma disk reactor oxygen source.

Degree: MS, Department of Electrical Engineering, 1992, Michigan State University

Subjects/Keywords: Lasers; Ablation (Aerothermodynamics); Microwave plasmas; Thin films

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APA (6th Edition):

Pawlowski, C. M. (1992). In situ laser ablation deposition of YBa2Cu3O7-X thin films using a microwave plasma disk reactor oxygen source. (Masters Thesis). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:22296

Chicago Manual of Style (16th Edition):

Pawlowski, Conrad Matthew. “In situ laser ablation deposition of YBa2Cu3O7-X thin films using a microwave plasma disk reactor oxygen source.” 1992. Masters Thesis, Michigan State University. Accessed January 20, 2020. http://etd.lib.msu.edu/islandora/object/etd:22296.

MLA Handbook (7th Edition):

Pawlowski, Conrad Matthew. “In situ laser ablation deposition of YBa2Cu3O7-X thin films using a microwave plasma disk reactor oxygen source.” 1992. Web. 20 Jan 2020.

Vancouver:

Pawlowski CM. In situ laser ablation deposition of YBa2Cu3O7-X thin films using a microwave plasma disk reactor oxygen source. [Internet] [Masters thesis]. Michigan State University; 1992. [cited 2020 Jan 20]. Available from: http://etd.lib.msu.edu/islandora/object/etd:22296.

Council of Science Editors:

Pawlowski CM. In situ laser ablation deposition of YBa2Cu3O7-X thin films using a microwave plasma disk reactor oxygen source. [Masters Thesis]. Michigan State University; 1992. Available from: http://etd.lib.msu.edu/islandora/object/etd:22296


Florida Atlantic University

29. Rodriguez, Daniel. Numerical Simulation of a Flowfield Around a Hypersonic Missile with Lateral Jets.

Degree: 2017, Florida Atlantic University

Summary: This work uses computational fluid dynamics to study the flowfield around a hypersonic missile with two lateral jets to provide control in place of… (more)

Subjects/Keywords: Aerodynamics, Hypersonic.; Nonequilibrium thermodynamics.; Aerothermodynamics – Mathematica.; Hypersonic planes – Design and construction – Mathematical models.; Vortex-motion – Mathematical models.

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APA (6th Edition):

Rodriguez, D. (2017). Numerical Simulation of a Flowfield Around a Hypersonic Missile with Lateral Jets. (Thesis). Florida Atlantic University. Retrieved from http://purl.flvc.org/fau/fd/FA00004893 ; (URL) http://purl.flvc.org/fau/fd/FA00004893

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):

Rodriguez, Daniel. “Numerical Simulation of a Flowfield Around a Hypersonic Missile with Lateral Jets.” 2017. Thesis, Florida Atlantic University. Accessed January 20, 2020. http://purl.flvc.org/fau/fd/FA00004893 ; (URL) http://purl.flvc.org/fau/fd/FA00004893.

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

MLA Handbook (7th Edition):

Rodriguez, Daniel. “Numerical Simulation of a Flowfield Around a Hypersonic Missile with Lateral Jets.” 2017. Web. 20 Jan 2020.

Vancouver:

Rodriguez D. Numerical Simulation of a Flowfield Around a Hypersonic Missile with Lateral Jets. [Internet] [Thesis]. Florida Atlantic University; 2017. [cited 2020 Jan 20]. Available from: http://purl.flvc.org/fau/fd/FA00004893 ; (URL) http://purl.flvc.org/fau/fd/FA00004893.

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

Council of Science Editors:

Rodriguez D. Numerical Simulation of a Flowfield Around a Hypersonic Missile with Lateral Jets. [Thesis]. Florida Atlantic University; 2017. Available from: http://purl.flvc.org/fau/fd/FA00004893 ; (URL) http://purl.flvc.org/fau/fd/FA00004893

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


Indian Institute of Science

30. Hima Bindu, V. Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration.

Degree: 2009, Indian Institute of Science

 The recent resurgence in hypersonics is centered around the development of SCRAMJET engine technology to power future hypersonic vehicles. Successful flight trials by Australian and… (more)

Subjects/Keywords: Aerothermodynamics; Scramjet Engines; Hypersonic Flows; Convective Heat Transfer; Aerodynamic Heating; Aerodynamic Forces; Hypersonic Shock Tunnel; Aerodynamic Measurements; Combustion Chambers - Heat Transfer; Accelerometer; Hypersonic Flow; Hypersonic Vehicles; Aeronautics

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

APA (6th Edition):

Hima Bindu, V. (2009). Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1120

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):

Hima Bindu, V. “Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration.” 2009. Thesis, Indian Institute of Science. Accessed January 20, 2020. http://hdl.handle.net/2005/1120.

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

MLA Handbook (7th Edition):

Hima Bindu, V. “Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration.” 2009. Web. 20 Jan 2020.

Vancouver:

Hima Bindu V. Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/2005/1120.

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

Council of Science Editors:

Hima Bindu V. Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/1120

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

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