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You searched for subject:(Hypersonic). Showing records 1 – 30 of 358 total matches.

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Penn State University

1. Feldick, Andrew Mark. Coupled Nonequilibrium Flow, Energy And Radiation Transport For Hypersonic Planetary Entry.

Degree: 2013, Penn State University

Hypersonic atmospheric entry is an important problem for space exploration. Vehicles which travel through space and enter into planetary atmospheres often travel at extreme speeds,… (more)

Subjects/Keywords: Radiation; Hypersonic Flow; Hypersonic; RTE; Monte Carlo

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APA (6th Edition):

Feldick, A. M. (2013). Coupled Nonequilibrium Flow, Energy And Radiation Transport For Hypersonic Planetary Entry. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19764

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):

Feldick, Andrew Mark. “Coupled Nonequilibrium Flow, Energy And Radiation Transport For Hypersonic Planetary Entry.” 2013. Thesis, Penn State University. Accessed March 01, 2021. https://submit-etda.libraries.psu.edu/catalog/19764.

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

MLA Handbook (7th Edition):

Feldick, Andrew Mark. “Coupled Nonequilibrium Flow, Energy And Radiation Transport For Hypersonic Planetary Entry.” 2013. Web. 01 Mar 2021.

Vancouver:

Feldick AM. Coupled Nonequilibrium Flow, Energy And Radiation Transport For Hypersonic Planetary Entry. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Mar 01]. Available from: https://submit-etda.libraries.psu.edu/catalog/19764.

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

Council of Science Editors:

Feldick AM. Coupled Nonequilibrium Flow, Energy And Radiation Transport For Hypersonic Planetary Entry. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19764

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


Virginia Tech

2. DellaFera, Andrew Brian. Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods.

Degree: MS, Aerospace Engineering, 2019, Virginia Tech

 Ramjets and scramjets are the key to sustained flight at speeds above five times the speed of sound. These propulsion systems pose a challenging simulation… (more)

Subjects/Keywords: Hypersonic; Propulsion; Optimization

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APA (6th Edition):

DellaFera, A. B. (2019). Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/95512

Chicago Manual of Style (16th Edition):

DellaFera, Andrew Brian. “Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods.” 2019. Masters Thesis, Virginia Tech. Accessed March 01, 2021. http://hdl.handle.net/10919/95512.

MLA Handbook (7th Edition):

DellaFera, Andrew Brian. “Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods.” 2019. Web. 01 Mar 2021.

Vancouver:

DellaFera AB. Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods. [Internet] [Masters thesis]. Virginia Tech; 2019. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10919/95512.

Council of Science Editors:

DellaFera AB. Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods. [Masters Thesis]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/95512


Ryerson University

3. 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 March 01, 2021. 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. 01 Mar 2021.

Vancouver:

Miri SH. Shock-less Hypersonic Intakes. [Internet] [Thesis]. Ryerson University; 2012. [cited 2021 Mar 01]. 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


San Jose State University

4. Carlozzi, Alexander Anthony. Estimating Stagnation-Point Radiative Heating Using Maslen's Inverse Method And High-Temperature Equilibrium Air Properties.

Degree: MS, Aerospace Engineering, 2015, San Jose State University

  This thesis attempts to estimate stagnation point radiative heat flux for hypervelocity reentry vehicles. To begin, a shock shape is assumed. Using the inverse… (more)

Subjects/Keywords: Heating; Hypersonic; Radiative; Reentry

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APA (6th Edition):

Carlozzi, A. A. (2015). Estimating Stagnation-Point Radiative Heating Using Maslen's Inverse Method And High-Temperature Equilibrium Air Properties. (Masters Thesis). San Jose State University. Retrieved from https://doi.org/10.31979/etd.95nk-nuqz ; https://scholarworks.sjsu.edu/etd_theses/4533

Chicago Manual of Style (16th Edition):

Carlozzi, Alexander Anthony. “Estimating Stagnation-Point Radiative Heating Using Maslen's Inverse Method And High-Temperature Equilibrium Air Properties.” 2015. Masters Thesis, San Jose State University. Accessed March 01, 2021. https://doi.org/10.31979/etd.95nk-nuqz ; https://scholarworks.sjsu.edu/etd_theses/4533.

MLA Handbook (7th Edition):

Carlozzi, Alexander Anthony. “Estimating Stagnation-Point Radiative Heating Using Maslen's Inverse Method And High-Temperature Equilibrium Air Properties.” 2015. Web. 01 Mar 2021.

Vancouver:

Carlozzi AA. Estimating Stagnation-Point Radiative Heating Using Maslen's Inverse Method And High-Temperature Equilibrium Air Properties. [Internet] [Masters thesis]. San Jose State University; 2015. [cited 2021 Mar 01]. Available from: https://doi.org/10.31979/etd.95nk-nuqz ; https://scholarworks.sjsu.edu/etd_theses/4533.

Council of Science Editors:

Carlozzi AA. Estimating Stagnation-Point Radiative Heating Using Maslen's Inverse Method And High-Temperature Equilibrium Air Properties. [Masters Thesis]. San Jose State University; 2015. Available from: https://doi.org/10.31979/etd.95nk-nuqz ; https://scholarworks.sjsu.edu/etd_theses/4533


Clemson University

5. Wilson, Daniel Mason. Rapid, Low-Fidelity Analysis Methods Using Historical Aircraft Data for Initializing the Conceptual Design of Hypersonic Aircraft.

Degree: MS, Mechanical Engineering, 2020, Clemson University

Hypersonic flight is generally considered greater than Mach 5 and represents an important frontier in aircraft capabilities. Difficulties arise because hypersonic flow differs from… (more)

Subjects/Keywords: Design; Hypersonic; Initialization; Regression

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APA (6th Edition):

Wilson, D. M. (2020). Rapid, Low-Fidelity Analysis Methods Using Historical Aircraft Data for Initializing the Conceptual Design of Hypersonic Aircraft. (Masters Thesis). Clemson University. Retrieved from https://tigerprints.clemson.edu/all_theses/3336

Chicago Manual of Style (16th Edition):

Wilson, Daniel Mason. “Rapid, Low-Fidelity Analysis Methods Using Historical Aircraft Data for Initializing the Conceptual Design of Hypersonic Aircraft.” 2020. Masters Thesis, Clemson University. Accessed March 01, 2021. https://tigerprints.clemson.edu/all_theses/3336.

MLA Handbook (7th Edition):

Wilson, Daniel Mason. “Rapid, Low-Fidelity Analysis Methods Using Historical Aircraft Data for Initializing the Conceptual Design of Hypersonic Aircraft.” 2020. Web. 01 Mar 2021.

Vancouver:

Wilson DM. Rapid, Low-Fidelity Analysis Methods Using Historical Aircraft Data for Initializing the Conceptual Design of Hypersonic Aircraft. [Internet] [Masters thesis]. Clemson University; 2020. [cited 2021 Mar 01]. Available from: https://tigerprints.clemson.edu/all_theses/3336.

Council of Science Editors:

Wilson DM. Rapid, Low-Fidelity Analysis Methods Using Historical Aircraft Data for Initializing the Conceptual Design of Hypersonic Aircraft. [Masters Thesis]. Clemson University; 2020. Available from: https://tigerprints.clemson.edu/all_theses/3336


Delft University of Technology

6. Viavattene, Giulia (author). Flying Qualities and Controllability of Hypersonic Spaceplanes.

Degree: 2018, Delft University of Technology

 Spaceplanes represent a new promising concept for space flight. A spaceplane is a reusable, safe, efficient and economical space transportation system that can generate lift… (more)

Subjects/Keywords: control; spaceplanes; hypersonic; robust control

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APA (6th Edition):

Viavattene, G. (. (2018). Flying Qualities and Controllability of Hypersonic Spaceplanes. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c731b2d3-91b5-4617-a844-0a1472abcaf6

Chicago Manual of Style (16th Edition):

Viavattene, Giulia (author). “Flying Qualities and Controllability of Hypersonic Spaceplanes.” 2018. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:c731b2d3-91b5-4617-a844-0a1472abcaf6.

MLA Handbook (7th Edition):

Viavattene, Giulia (author). “Flying Qualities and Controllability of Hypersonic Spaceplanes.” 2018. Web. 01 Mar 2021.

Vancouver:

Viavattene G(. Flying Qualities and Controllability of Hypersonic Spaceplanes. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:c731b2d3-91b5-4617-a844-0a1472abcaf6.

Council of Science Editors:

Viavattene G(. Flying Qualities and Controllability of Hypersonic Spaceplanes. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:c731b2d3-91b5-4617-a844-0a1472abcaf6


University of Notre Dame

7. Brock E. Hedlund. Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>.

Degree: Aerospace and Mechanical Engineering, 2018, University of Notre Dame

  This thesis documents the efforts to characterize the Mach 4.5 flow over a flat plate model with a 30° compression ramp over a range… (more)

Subjects/Keywords: Flow Measurement; Scramjet; Hypersonic

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APA (6th Edition):

Hedlund, B. E. (2018). Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>. (Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/d791sf2933j

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):

Hedlund, Brock E.. “Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>.” 2018. Thesis, University of Notre Dame. Accessed March 01, 2021. https://curate.nd.edu/show/d791sf2933j.

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

MLA Handbook (7th Edition):

Hedlund, Brock E.. “Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>.” 2018. Web. 01 Mar 2021.

Vancouver:

Hedlund BE. Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>. [Internet] [Thesis]. University of Notre Dame; 2018. [cited 2021 Mar 01]. Available from: https://curate.nd.edu/show/d791sf2933j.

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

Council of Science Editors:

Hedlund BE. Measurement of Flow Perturbations Occurring Both Naturally and by Plasma Induction over a Mach 4.5 Corner Separation Zone</h1>. [Thesis]. University of Notre Dame; 2018. Available from: https://curate.nd.edu/show/d791sf2933j

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


University of Florida

8. Nivison, Scott A. Sparse and Deep Learning-Based Nonlinear Control Design with Hypersonic Flight Applications.

Degree: PhD, Electrical and Computer Engineering, 2017, University of Florida

The task of hypersonic vehicle (HSV) flight control is both intriguing and complicated. HSV control requires dealing with interactions between structural, aerodynamic Advisors/Committee Members: KHARGONEKAR,PRAMOD P (committee chair), DIXON,WARREN E (committee member), FITZ-COY,NORMAN G (committee member).

Subjects/Keywords: adaptive  – hypersonic  – learning  – lyapunov

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APA (6th Edition):

Nivison, S. A. (2017). Sparse and Deep Learning-Based Nonlinear Control Design with Hypersonic Flight Applications. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0051837

Chicago Manual of Style (16th Edition):

Nivison, Scott A. “Sparse and Deep Learning-Based Nonlinear Control Design with Hypersonic Flight Applications.” 2017. Doctoral Dissertation, University of Florida. Accessed March 01, 2021. https://ufdc.ufl.edu/UFE0051837.

MLA Handbook (7th Edition):

Nivison, Scott A. “Sparse and Deep Learning-Based Nonlinear Control Design with Hypersonic Flight Applications.” 2017. Web. 01 Mar 2021.

Vancouver:

Nivison SA. Sparse and Deep Learning-Based Nonlinear Control Design with Hypersonic Flight Applications. [Internet] [Doctoral dissertation]. University of Florida; 2017. [cited 2021 Mar 01]. Available from: https://ufdc.ufl.edu/UFE0051837.

Council of Science Editors:

Nivison SA. Sparse and Deep Learning-Based Nonlinear Control Design with Hypersonic Flight Applications. [Doctoral Dissertation]. University of Florida; 2017. Available from: https://ufdc.ufl.edu/UFE0051837


University of Illinois – Urbana-Champaign

9. Morgan, Jonathan Deming. Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe.

Degree: MS, Aerospace Engineering, 2018, University of Illinois – Urbana-Champaign

 Spectral radiation is sensitive to many physical chemical aspects of high-enthalpy, non-equilibrium flows affect radiation and heat transfer estimates at low-earth altitudes, which is important… (more)

Subjects/Keywords: hypersonic; nonequilibrium; cubesat; DSMC

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APA (6th Edition):

Morgan, J. D. (2018). Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/101076

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

Chicago Manual of Style (16th Edition):

Morgan, Jonathan Deming. “Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe.” 2018. Thesis, University of Illinois – Urbana-Champaign. Accessed March 01, 2021. http://hdl.handle.net/2142/101076.

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

MLA Handbook (7th Edition):

Morgan, Jonathan Deming. “Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe.” 2018. Web. 01 Mar 2021.

Vancouver:

Morgan JD. Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2018. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2142/101076.

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

Council of Science Editors:

Morgan JD. Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe. [Thesis]. University of Illinois – Urbana-Champaign; 2018. Available from: http://hdl.handle.net/2142/101076

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


University of Arizona

10. Tolle, Frederick Francis, 1921-. AN INVESTIGATION OF THE INFLUENCE OF A FORWARD EJECTED GAS STREAM IN HYPERSONIC FLOW ABOUT BLUNT-BODIES .

Degree: 1973, University of Arizona

Subjects/Keywords: Aerodynamics; Hypersonic.

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APA (6th Edition):

Tolle, Frederick Francis, 1. (1973). AN INVESTIGATION OF THE INFLUENCE OF A FORWARD EJECTED GAS STREAM IN HYPERSONIC FLOW ABOUT BLUNT-BODIES . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/288101

Chicago Manual of Style (16th Edition):

Tolle, Frederick Francis, 1921-. “AN INVESTIGATION OF THE INFLUENCE OF A FORWARD EJECTED GAS STREAM IN HYPERSONIC FLOW ABOUT BLUNT-BODIES .” 1973. Doctoral Dissertation, University of Arizona. Accessed March 01, 2021. http://hdl.handle.net/10150/288101.

MLA Handbook (7th Edition):

Tolle, Frederick Francis, 1921-. “AN INVESTIGATION OF THE INFLUENCE OF A FORWARD EJECTED GAS STREAM IN HYPERSONIC FLOW ABOUT BLUNT-BODIES .” 1973. Web. 01 Mar 2021.

Vancouver:

Tolle, Frederick Francis 1. AN INVESTIGATION OF THE INFLUENCE OF A FORWARD EJECTED GAS STREAM IN HYPERSONIC FLOW ABOUT BLUNT-BODIES . [Internet] [Doctoral dissertation]. University of Arizona; 1973. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10150/288101.

Council of Science Editors:

Tolle, Frederick Francis 1. AN INVESTIGATION OF THE INFLUENCE OF A FORWARD EJECTED GAS STREAM IN HYPERSONIC FLOW ABOUT BLUNT-BODIES . [Doctoral Dissertation]. University of Arizona; 1973. Available from: http://hdl.handle.net/10150/288101


University of Sydney

11. Sharifzadeh, Shayan. Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles .

Degree: 2017, University of Sydney

 Aviation industry is continuously growing especially for very long distance flights due to the globalisation of local economies around the world and the explosive economic… (more)

Subjects/Keywords: Hypersonic; aircraft; design; cryogenic; hydrogen

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APA (6th Edition):

Sharifzadeh, S. (2017). Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles . (Thesis). University of Sydney. Retrieved from http://hdl.handle.net/2123/19127

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):

Sharifzadeh, Shayan. “Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles .” 2017. Thesis, University of Sydney. Accessed March 01, 2021. http://hdl.handle.net/2123/19127.

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

MLA Handbook (7th Edition):

Sharifzadeh, Shayan. “Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles .” 2017. Web. 01 Mar 2021.

Vancouver:

Sharifzadeh S. Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles . [Internet] [Thesis]. University of Sydney; 2017. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2123/19127.

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

Council of Science Editors:

Sharifzadeh S. Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles . [Thesis]. University of Sydney; 2017. Available from: http://hdl.handle.net/2123/19127

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


University of New South Wales

12. 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 March 01, 2021. 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. 01 Mar 2021.

Vancouver:

Khraibut A. Laminar Hypersonic Leading Edge Separation. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2021 Mar 01]. 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 Texas – Austin

13. Dannemiller, David Paul. Periodic cruise of a hypersonic cruiser for fuel minimization.

Degree: MS, Aerospace Engineering, 1981, University of Texas – Austin

Subjects/Keywords: Aerodynamics; Hypersonic

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APA (6th Edition):

Dannemiller, D. P. (1981). Periodic cruise of a hypersonic cruiser for fuel minimization. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/41765

Chicago Manual of Style (16th Edition):

Dannemiller, David Paul. “Periodic cruise of a hypersonic cruiser for fuel minimization.” 1981. Masters Thesis, University of Texas – Austin. Accessed March 01, 2021. http://hdl.handle.net/2152/41765.

MLA Handbook (7th Edition):

Dannemiller, David Paul. “Periodic cruise of a hypersonic cruiser for fuel minimization.” 1981. Web. 01 Mar 2021.

Vancouver:

Dannemiller DP. Periodic cruise of a hypersonic cruiser for fuel minimization. [Internet] [Masters thesis]. University of Texas – Austin; 1981. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2152/41765.

Council of Science Editors:

Dannemiller DP. Periodic cruise of a hypersonic cruiser for fuel minimization. [Masters Thesis]. University of Texas – Austin; 1981. Available from: http://hdl.handle.net/2152/41765


University of Adelaide

14. Harrland, Alan. Hypersonic inlet for a laser powered propulsion system.

Degree: 2012, University of Adelaide

 The idea of laser powered lightcraft was first conceptualised in the early 1970's as a means of launching small scale satellite payloads into orbit at… (more)

Subjects/Keywords: hypersonic; stream traced inlet; lightcraft; hypersonic inlet design; computational fluid dynamics

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APA (6th Edition):

Harrland, A. (2012). Hypersonic inlet for a laser powered propulsion system. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/79072

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):

Harrland, Alan. “Hypersonic inlet for a laser powered propulsion system.” 2012. Thesis, University of Adelaide. Accessed March 01, 2021. http://hdl.handle.net/2440/79072.

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

MLA Handbook (7th Edition):

Harrland, Alan. “Hypersonic inlet for a laser powered propulsion system.” 2012. Web. 01 Mar 2021.

Vancouver:

Harrland A. Hypersonic inlet for a laser powered propulsion system. [Internet] [Thesis]. University of Adelaide; 2012. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2440/79072.

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

Council of Science Editors:

Harrland A. Hypersonic inlet for a laser powered propulsion system. [Thesis]. University of Adelaide; 2012. Available from: http://hdl.handle.net/2440/79072

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


Indian Institute of Science

15. Nagashetty, K. Experimental Investigations on Hypersonic Waverider.

Degree: MSc Engg, Faculty of Engineering, 2018, Indian Institute of Science

 In the flying field of space transportation domain, the increased efforts involving design and development of hypersonic flight for space missions is on toe to… (more)

Subjects/Keywords: Hypersonic Waverider; Aerothermodynamics; Hypersonic Aerodynamics; Aerodynamics; Hypersonic Shock Tunnel - Heat Transfer; Hypersonic Shock Tunnel HST2; Flow Visualization; Shock Wave Loading; Hypersonic Mach Numbers; Aerospace Engineering

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APA (6th Edition):

Nagashetty, K. (2018). Experimental Investigations on Hypersonic Waverider. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3195

Chicago Manual of Style (16th Edition):

Nagashetty, K. “Experimental Investigations on Hypersonic Waverider.” 2018. Masters Thesis, Indian Institute of Science. Accessed March 01, 2021. http://etd.iisc.ac.in/handle/2005/3195.

MLA Handbook (7th Edition):

Nagashetty, K. “Experimental Investigations on Hypersonic Waverider.” 2018. Web. 01 Mar 2021.

Vancouver:

Nagashetty K. Experimental Investigations on Hypersonic Waverider. [Internet] [Masters thesis]. Indian Institute of Science; 2018. [cited 2021 Mar 01]. Available from: http://etd.iisc.ac.in/handle/2005/3195.

Council of Science Editors:

Nagashetty K. Experimental Investigations on Hypersonic Waverider. [Masters Thesis]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3195


Indian Institute of Science

16. Philip, Sarah Jobin. Investigation of Heat Transfer Rates Around the Aerodynamic Cavities on a Flat Plate at Hypersonic Mach Numbers.

Degree: MSc Engg, Faculty of Engineering, 2018, Indian Institute of Science

 Aerodynamic cavities are common features on hypersonic vehicles which are caused in both large and small scale features like surface defects, pitting, gap in joints… (more)

Subjects/Keywords: Aerodynamics; Hypersonic Cavity Flow Physics; Hypersonic Shock Tunnel HST2; Convective Heat Transfer; Hypersonic Flow - Numerical Simulation; Flow Visualization; Hypersonic Mach Numbers; Hypersonic Flow; Hypersonic Shock Tunnels - Aerodynamic Cavities; Aerodynmaic Cavities - Heat Transfer; Hypersonic Shock Tunnels - Heat Transfer; Flat Plates; Uncertainty Analysis; Aerospace Engineering

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APA (6th Edition):

Philip, S. J. (2018). Investigation of Heat Transfer Rates Around the Aerodynamic Cavities on a Flat Plate at Hypersonic Mach Numbers. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3900

Chicago Manual of Style (16th Edition):

Philip, Sarah Jobin. “Investigation of Heat Transfer Rates Around the Aerodynamic Cavities on a Flat Plate at Hypersonic Mach Numbers.” 2018. Masters Thesis, Indian Institute of Science. Accessed March 01, 2021. http://etd.iisc.ac.in/handle/2005/3900.

MLA Handbook (7th Edition):

Philip, Sarah Jobin. “Investigation of Heat Transfer Rates Around the Aerodynamic Cavities on a Flat Plate at Hypersonic Mach Numbers.” 2018. Web. 01 Mar 2021.

Vancouver:

Philip SJ. Investigation of Heat Transfer Rates Around the Aerodynamic Cavities on a Flat Plate at Hypersonic Mach Numbers. [Internet] [Masters thesis]. Indian Institute of Science; 2018. [cited 2021 Mar 01]. Available from: http://etd.iisc.ac.in/handle/2005/3900.

Council of Science Editors:

Philip SJ. Investigation of Heat Transfer Rates Around the Aerodynamic Cavities on a Flat Plate at Hypersonic Mach Numbers. [Masters Thesis]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3900


Texas A&M University

17. Brown II, Robert Lee. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 This dissertation examines the following subjects important to hypersonic aerothermoelastic flows: aerodynamic heating on a double-wedge airfoil, active cooling on a double-wedge airfoil, and aerothermoelastic… (more)

Subjects/Keywords: hypersonic; panel flutter; aerothermal; aeroelastic; aerothermoelastic; simulation

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APA (6th Edition):

Brown II, R. L. (2016). Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158046

Chicago Manual of Style (16th Edition):

Brown II, Robert Lee. “Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.” 2016. Doctoral Dissertation, Texas A&M University. Accessed March 01, 2021. http://hdl.handle.net/1969.1/158046.

MLA Handbook (7th Edition):

Brown II, Robert Lee. “Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.” 2016. Web. 01 Mar 2021.

Vancouver:

Brown II RL. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1969.1/158046.

Council of Science Editors:

Brown II RL. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158046


Penn State University

18. Patil, Varun Nandan. Study of Shock-Shock Interactions for the HET Facility Double Wedge Configuration using the DSMC Approach.

Degree: 2013, Penn State University

 A set of numerical simulations designed to study the laminar, shock-shock interactions from hypersonic flows about a double wedge configuration for the Hypervelocity Expansion Tube… (more)

Subjects/Keywords: Hypersonic Flows; Shock-shock interactions; DSMC

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APA (6th Edition):

Patil, V. N. (2013). Study of Shock-Shock Interactions for the HET Facility Double Wedge Configuration using the DSMC Approach. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19072

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):

Patil, Varun Nandan. “Study of Shock-Shock Interactions for the HET Facility Double Wedge Configuration using the DSMC Approach.” 2013. Thesis, Penn State University. Accessed March 01, 2021. https://submit-etda.libraries.psu.edu/catalog/19072.

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

MLA Handbook (7th Edition):

Patil, Varun Nandan. “Study of Shock-Shock Interactions for the HET Facility Double Wedge Configuration using the DSMC Approach.” 2013. Web. 01 Mar 2021.

Vancouver:

Patil VN. Study of Shock-Shock Interactions for the HET Facility Double Wedge Configuration using the DSMC Approach. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Mar 01]. Available from: https://submit-etda.libraries.psu.edu/catalog/19072.

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

Council of Science Editors:

Patil VN. Study of Shock-Shock Interactions for the HET Facility Double Wedge Configuration using the DSMC Approach. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19072

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


Penn State University

19. Sohn, Ilyoup. Modeling and Simulation of Radiation from Hypersonic Flows using Monte Carlo Methods.

Degree: 2011, Penn State University

 During extreme-Mach number reentry into Earth's atmosphere, spacecraft experience hypersonic non-equilibrium flow conditions that dissociate molecules and ionize atoms. Such situations occur behind a shock… (more)

Subjects/Keywords: Radiation; Hypersonic; Monte Carlo Methods; Nonequilibrium

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APA (6th Edition):

Sohn, I. (2011). Modeling and Simulation of Radiation from Hypersonic Flows using Monte Carlo Methods. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/11737

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):

Sohn, Ilyoup. “Modeling and Simulation of Radiation from Hypersonic Flows using Monte Carlo Methods.” 2011. Thesis, Penn State University. Accessed March 01, 2021. https://submit-etda.libraries.psu.edu/catalog/11737.

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

MLA Handbook (7th Edition):

Sohn, Ilyoup. “Modeling and Simulation of Radiation from Hypersonic Flows using Monte Carlo Methods.” 2011. Web. 01 Mar 2021.

Vancouver:

Sohn I. Modeling and Simulation of Radiation from Hypersonic Flows using Monte Carlo Methods. [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Mar 01]. Available from: https://submit-etda.libraries.psu.edu/catalog/11737.

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

Council of Science Editors:

Sohn I. Modeling and Simulation of Radiation from Hypersonic Flows using Monte Carlo Methods. [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/11737

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


Purdue University

20. Sparapany, Michael. Towards the Real-Time Application of Indirect Methods for Hypersonic Missions.

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

 Conceptual hypersonic mission design has typically been performed in a computationally intensive, iterative manner using direct optimization methods. The introduction of modern computing has resulted… (more)

Subjects/Keywords: Hypersonic; Indirect; Methods; Optimization; Real; Time

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APA (6th Edition):

Sparapany, M. (2015). Towards the Real-Time Application of Indirect Methods for Hypersonic Missions. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/1161

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):

Sparapany, Michael. “Towards the Real-Time Application of Indirect Methods for Hypersonic Missions.” 2015. Thesis, Purdue University. Accessed March 01, 2021. https://docs.lib.purdue.edu/open_access_theses/1161.

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

MLA Handbook (7th Edition):

Sparapany, Michael. “Towards the Real-Time Application of Indirect Methods for Hypersonic Missions.” 2015. Web. 01 Mar 2021.

Vancouver:

Sparapany M. Towards the Real-Time Application of Indirect Methods for Hypersonic Missions. [Internet] [Thesis]. Purdue University; 2015. [cited 2021 Mar 01]. Available from: https://docs.lib.purdue.edu/open_access_theses/1161.

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

Council of Science Editors:

Sparapany M. Towards the Real-Time Application of Indirect Methods for Hypersonic Missions. [Thesis]. Purdue University; 2015. Available from: https://docs.lib.purdue.edu/open_access_theses/1161

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


Indian Institute of Science

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

Degree: MSc Engg, Faculty of Engineering, 2011, 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 (6th Edition):

Hima Bindu, V. (2011). Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1120

Chicago Manual of Style (16th Edition):

Hima Bindu, V. “Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration.” 2011. Masters Thesis, Indian Institute of Science. Accessed March 01, 2021. http://etd.iisc.ac.in/handle/2005/1120.

MLA Handbook (7th Edition):

Hima Bindu, V. “Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration.” 2011. Web. 01 Mar 2021.

Vancouver:

Hima Bindu V. Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration. [Internet] [Masters thesis]. Indian Institute of Science; 2011. [cited 2021 Mar 01]. Available from: http://etd.iisc.ac.in/handle/2005/1120.

Council of Science Editors:

Hima Bindu V. Experimental Investigations Of Aerothermodynamics Of A Scramjet Engine Configuration. [Masters Thesis]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ac.in/handle/2005/1120


University of Toronto

22. Chan, Jonathan. Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11.

Degree: 2010, University of Toronto

This study investigates the design and aeropropulsive performance of a complete, hydrogen powered, shock-induced combustion ramjet (shcramjet) at a flight Mach number of 11 and… (more)

Subjects/Keywords: hypersonic; propulsion; scramjet; shcramjet; performance; simulation; 0538

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APA (6th Edition):

Chan, J. (2010). Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/25446

Chicago Manual of Style (16th Edition):

Chan, Jonathan. “Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11.” 2010. Masters Thesis, University of Toronto. Accessed March 01, 2021. http://hdl.handle.net/1807/25446.

MLA Handbook (7th Edition):

Chan, Jonathan. “Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11.” 2010. Web. 01 Mar 2021.

Vancouver:

Chan J. Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11. [Internet] [Masters thesis]. University of Toronto; 2010. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1807/25446.

Council of Science Editors:

Chan J. Numerically Simulated Comparative Performance of a Scramjet and Shcramjet at Mach 11. [Masters Thesis]. University of Toronto; 2010. Available from: http://hdl.handle.net/1807/25446


University of Manchester

23. Yang, Leichao. Flow control using energy deposition at Mach 5.

Degree: PhD, 2012, University of Manchester

 Flow control has always been an intense research subject with the pursuit of favourable control effects like drag reduction, transition delay, and separation prevention. In… (more)

Subjects/Keywords: 629.132; Hypersonic Flow; Energy Deposition;

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APA (6th Edition):

Yang, L. (2012). Flow control using energy deposition at Mach 5. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/flow-control-using-energy-deposition-at-mach-5(09bb331e-c3d3-4365-bdfc-6001a54c5702).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.564303

Chicago Manual of Style (16th Edition):

Yang, Leichao. “Flow control using energy deposition at Mach 5.” 2012. Doctoral Dissertation, University of Manchester. Accessed March 01, 2021. https://www.research.manchester.ac.uk/portal/en/theses/flow-control-using-energy-deposition-at-mach-5(09bb331e-c3d3-4365-bdfc-6001a54c5702).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.564303.

MLA Handbook (7th Edition):

Yang, Leichao. “Flow control using energy deposition at Mach 5.” 2012. Web. 01 Mar 2021.

Vancouver:

Yang L. Flow control using energy deposition at Mach 5. [Internet] [Doctoral dissertation]. University of Manchester; 2012. [cited 2021 Mar 01]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/flow-control-using-energy-deposition-at-mach-5(09bb331e-c3d3-4365-bdfc-6001a54c5702).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.564303.

Council of Science Editors:

Yang L. Flow control using energy deposition at Mach 5. [Doctoral Dissertation]. University of Manchester; 2012. Available from: https://www.research.manchester.ac.uk/portal/en/theses/flow-control-using-energy-deposition-at-mach-5(09bb331e-c3d3-4365-bdfc-6001a54c5702).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.564303


Delft University of Technology

24. Van Dooren, R.M. (author). The controllability of a winged hypersonic vehicle under aeroelastic effects.

Degree: 2016, Delft University of Technology

Aerospace Engineering

Space Engineering

Space Flight

Advisors/Committee Members: Mooij, E. (mentor).

Subjects/Keywords: Aeroelasticity; Controllability; hypersonic

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APA (6th Edition):

Van Dooren, R. M. (. (2016). The controllability of a winged hypersonic vehicle under aeroelastic effects. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e8527460-df6c-4a08-838d-247566fa4c44

Chicago Manual of Style (16th Edition):

Van Dooren, R M (author). “The controllability of a winged hypersonic vehicle under aeroelastic effects.” 2016. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:e8527460-df6c-4a08-838d-247566fa4c44.

MLA Handbook (7th Edition):

Van Dooren, R M (author). “The controllability of a winged hypersonic vehicle under aeroelastic effects.” 2016. Web. 01 Mar 2021.

Vancouver:

Van Dooren RM(. The controllability of a winged hypersonic vehicle under aeroelastic effects. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:e8527460-df6c-4a08-838d-247566fa4c44.

Council of Science Editors:

Van Dooren RM(. The controllability of a winged hypersonic vehicle under aeroelastic effects. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:e8527460-df6c-4a08-838d-247566fa4c44


University of Minnesota

25. Reinert, John. Conjugate Heat Transfer Simulations for Hypersonic Vehicles.

Degree: PhD, Aerospace Engineering and Mechanics, 2020, University of Minnesota

 The accurate prediction of thermal responses is important for optimizing the design and operability for hypersonic flight vehicles. In order to efficiently simulate this process,… (more)

Subjects/Keywords: aerothermal; CFD; conjugate heat transfer; hypersonic

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APA (6th Edition):

Reinert, J. (2020). Conjugate Heat Transfer Simulations for Hypersonic Vehicles. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/216841

Chicago Manual of Style (16th Edition):

Reinert, John. “Conjugate Heat Transfer Simulations for Hypersonic Vehicles.” 2020. Doctoral Dissertation, University of Minnesota. Accessed March 01, 2021. http://hdl.handle.net/11299/216841.

MLA Handbook (7th Edition):

Reinert, John. “Conjugate Heat Transfer Simulations for Hypersonic Vehicles.” 2020. Web. 01 Mar 2021.

Vancouver:

Reinert J. Conjugate Heat Transfer Simulations for Hypersonic Vehicles. [Internet] [Doctoral dissertation]. University of Minnesota; 2020. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/11299/216841.

Council of Science Editors:

Reinert J. Conjugate Heat Transfer Simulations for Hypersonic Vehicles. [Doctoral Dissertation]. University of Minnesota; 2020. Available from: http://hdl.handle.net/11299/216841


Princeton University

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

Degree: PhD, 2020, Princeton University

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Grube, Nathan Elias. “Shock Wave – Turbulence Interactions .” 2020. Doctoral Dissertation, Princeton University. Accessed March 01, 2021. http://arks.princeton.edu/ark:/88435/dsp01j6731673z.

MLA Handbook (7th Edition):

Grube, Nathan Elias. “Shock Wave – Turbulence Interactions .” 2020. Web. 01 Mar 2021.

Vancouver:

Grube NE. Shock Wave – Turbulence Interactions . [Internet] [Doctoral dissertation]. Princeton University; 2020. [cited 2021 Mar 01]. Available from: http://arks.princeton.edu/ark:/88435/dsp01j6731673z.

Council of Science Editors:

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


Indian Institute of Science

27. Srinath, S. Experimental Study Of Large Angle Blunt Cone With Telescopic Aerospike Flying At Hypersonic Mach Numbers.

Degree: MSc Engg, Faculty of Engineering, 2011, Indian Institute of Science

 The emerging and competitive environment in the space technology requires the improvements in the capability of aerodynamic vehicles. This leads to the analysis in drag… (more)

Subjects/Keywords: Hypersonic Aerodynamics; Aerospike; Hypersonic Mach Numbers; Hypersonic Flow; Drag (Aerodynamics); Aerodynamic Heating; Cone-Aerodynamics; Telescopic Aerospike; Hypersonic Shock Tunnel HST2; Blunt Cone; Aeronautics

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APA (6th Edition):

Srinath, S. (2011). Experimental Study Of Large Angle Blunt Cone With Telescopic Aerospike Flying At Hypersonic Mach Numbers. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1116

Chicago Manual of Style (16th Edition):

Srinath, S. “Experimental Study Of Large Angle Blunt Cone With Telescopic Aerospike Flying At Hypersonic Mach Numbers.” 2011. Masters Thesis, Indian Institute of Science. Accessed March 01, 2021. http://etd.iisc.ac.in/handle/2005/1116.

MLA Handbook (7th Edition):

Srinath, S. “Experimental Study Of Large Angle Blunt Cone With Telescopic Aerospike Flying At Hypersonic Mach Numbers.” 2011. Web. 01 Mar 2021.

Vancouver:

Srinath S. Experimental Study Of Large Angle Blunt Cone With Telescopic Aerospike Flying At Hypersonic Mach Numbers. [Internet] [Masters thesis]. Indian Institute of Science; 2011. [cited 2021 Mar 01]. Available from: http://etd.iisc.ac.in/handle/2005/1116.

Council of Science Editors:

Srinath S. Experimental Study Of Large Angle Blunt Cone With Telescopic Aerospike Flying At Hypersonic Mach Numbers. [Masters Thesis]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ac.in/handle/2005/1116


University of New South Wales

28. Bright, Courtney. Secondary Injection Thrust Vector Control for Spacecraft Propulsion.

Degree: Engineering & Information Technology, 2019, University of New South Wales

 This thesis explores the application of secondary injection thrust vector control (SITVC) to spacecraft propulsion, where propellant consumption and system complexity are often increased by… (more)

Subjects/Keywords: Hypersonic; Propulsion; Injection pressure; Spacecraft; Vectoring

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APA (6th Edition):

Bright, C. (2019). Secondary Injection Thrust Vector Control for Spacecraft Propulsion. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/64934 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:63059/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Bright, Courtney. “Secondary Injection Thrust Vector Control for Spacecraft Propulsion.” 2019. Doctoral Dissertation, University of New South Wales. Accessed March 01, 2021. http://handle.unsw.edu.au/1959.4/64934 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:63059/SOURCE02?view=true.

MLA Handbook (7th Edition):

Bright, Courtney. “Secondary Injection Thrust Vector Control for Spacecraft Propulsion.” 2019. Web. 01 Mar 2021.

Vancouver:

Bright C. Secondary Injection Thrust Vector Control for Spacecraft Propulsion. [Internet] [Doctoral dissertation]. University of New South Wales; 2019. [cited 2021 Mar 01]. Available from: http://handle.unsw.edu.au/1959.4/64934 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:63059/SOURCE02?view=true.

Council of Science Editors:

Bright C. Secondary Injection Thrust Vector Control for Spacecraft Propulsion. [Doctoral Dissertation]. University of New South Wales; 2019. Available from: http://handle.unsw.edu.au/1959.4/64934 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:63059/SOURCE02?view=true


Delft University of Technology

29. Carvalho Barreira Lages Ribeiro, André (author). Optimal Aeroassisted Maneuvers for Orbital Transfer.

Degree: 2019, Delft University of Technology

 Orbital plane changes require a considerable amount of propellant to be completed if the traditional fully propulsive maneuver is used. The cost associated with this… (more)

Subjects/Keywords: Optimization; Re-entry; Aeroassisted; Astrodynamics; Hypersonic

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APA (6th Edition):

Carvalho Barreira Lages Ribeiro, A. (. (2019). Optimal Aeroassisted Maneuvers for Orbital Transfer. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398

Chicago Manual of Style (16th Edition):

Carvalho Barreira Lages Ribeiro, André (author). “Optimal Aeroassisted Maneuvers for Orbital Transfer.” 2019. Masters Thesis, Delft University of Technology. Accessed March 01, 2021. http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398.

MLA Handbook (7th Edition):

Carvalho Barreira Lages Ribeiro, André (author). “Optimal Aeroassisted Maneuvers for Orbital Transfer.” 2019. Web. 01 Mar 2021.

Vancouver:

Carvalho Barreira Lages Ribeiro A(. Optimal Aeroassisted Maneuvers for Orbital Transfer. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Mar 01]. Available from: http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398.

Council of Science Editors:

Carvalho Barreira Lages Ribeiro A(. Optimal Aeroassisted Maneuvers for Orbital Transfer. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:89acba76-65ed-438d-810e-f3a863546398


University of Minnesota

30. Houston, Mary. Hypersonic Boundary Layer Stability Analysis Using Momentum Potential Theory.

Degree: MS, Aerospace Engineering and Mechanics, 2020, University of Minnesota

 Linear Stability Theory (LST) and the Parabolized Stability Equations (PSE) have provided valuable tools for analysis and prediction of laminar to turbulent transition for plates,… (more)

Subjects/Keywords: CDF; Fluid dynamics; High speed; Hypersonic; Transition

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Houston, M. (2020). Hypersonic Boundary Layer Stability Analysis Using Momentum Potential Theory. (Masters Thesis). University of Minnesota. Retrieved from http://hdl.handle.net/11299/217112

Chicago Manual of Style (16th Edition):

Houston, Mary. “Hypersonic Boundary Layer Stability Analysis Using Momentum Potential Theory.” 2020. Masters Thesis, University of Minnesota. Accessed March 01, 2021. http://hdl.handle.net/11299/217112.

MLA Handbook (7th Edition):

Houston, Mary. “Hypersonic Boundary Layer Stability Analysis Using Momentum Potential Theory.” 2020. Web. 01 Mar 2021.

Vancouver:

Houston M. Hypersonic Boundary Layer Stability Analysis Using Momentum Potential Theory. [Internet] [Masters thesis]. University of Minnesota; 2020. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/11299/217112.

Council of Science Editors:

Houston M. Hypersonic Boundary Layer Stability Analysis Using Momentum Potential Theory. [Masters Thesis]. University of Minnesota; 2020. Available from: http://hdl.handle.net/11299/217112

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