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You searched for subject:(boundary layer stability). Showing records 1 – 30 of 51 total matches.

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Texas A&M University

1. Downs, Robert 1982-. Environmental Influences on Crossflow Instability.

Degree: 2012, Texas A&M University

 The laminar-to-turbulent transition process in swept-wing boundary layers is often dominated by an inflectional instability arising from crossflow. It is now known that freestream turbulence… (more)

Subjects/Keywords: boundary-layer stability; Crossflow instability

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APA (6th Edition):

Downs, R. 1. (2012). Environmental Influences on Crossflow Instability. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148060

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):

Downs, Robert 1982-. “Environmental Influences on Crossflow Instability.” 2012. Thesis, Texas A&M University. Accessed December 16, 2019. http://hdl.handle.net/1969.1/148060.

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

MLA Handbook (7th Edition):

Downs, Robert 1982-. “Environmental Influences on Crossflow Instability.” 2012. Web. 16 Dec 2019.

Vancouver:

Downs R1. Environmental Influences on Crossflow Instability. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/1969.1/148060.

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

Council of Science Editors:

Downs R1. Environmental Influences on Crossflow Instability. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148060

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


Texas A&M University

2. Kocian, Travis Scott. Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC.

Degree: PhD, Aerospace Engineering, 2018, Texas A&M University

 Laminar-to-turbulent transition is a process that is critical in determining the system drag and surface heating of a flight vehicle, and the ability to predict,… (more)

Subjects/Keywords: Hypersonics; stability; boundary-layer; CFD

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APA (6th Edition):

Kocian, T. S. (2018). Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/173633

Chicago Manual of Style (16th Edition):

Kocian, Travis Scott. “Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC.” 2018. Doctoral Dissertation, Texas A&M University. Accessed December 16, 2019. http://hdl.handle.net/1969.1/173633.

MLA Handbook (7th Edition):

Kocian, Travis Scott. “Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC.” 2018. Web. 16 Dec 2019.

Vancouver:

Kocian TS. Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC. [Internet] [Doctoral dissertation]. Texas A&M University; 2018. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/1969.1/173633.

Council of Science Editors:

Kocian TS. Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC. [Doctoral Dissertation]. Texas A&M University; 2018. Available from: http://hdl.handle.net/1969.1/173633


University of Manchester

3. Williams, Anthony James. Boundary-layer flows with short-scale spanwise disturbances.

Degree: 2019, University of Manchester

 This work considers the three-dimensional laminar boundary layer on a semi-infinite plate aligned with a uniform oncoming stream or driven by a favourable pressure gradient… (more)

Subjects/Keywords: Boundary-layer; Short spanwise scale; Injection; Stability

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APA (6th Edition):

Williams, A. J. (2019). Boundary-layer flows with short-scale spanwise disturbances. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:318010

Chicago Manual of Style (16th Edition):

Williams, Anthony James. “Boundary-layer flows with short-scale spanwise disturbances.” 2019. Doctoral Dissertation, University of Manchester. Accessed December 16, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:318010.

MLA Handbook (7th Edition):

Williams, Anthony James. “Boundary-layer flows with short-scale spanwise disturbances.” 2019. Web. 16 Dec 2019.

Vancouver:

Williams AJ. Boundary-layer flows with short-scale spanwise disturbances. [Internet] [Doctoral dissertation]. University of Manchester; 2019. [cited 2019 Dec 16]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:318010.

Council of Science Editors:

Williams AJ. Boundary-layer flows with short-scale spanwise disturbances. [Doctoral Dissertation]. University of Manchester; 2019. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:318010


University of Manchester

4. Williams, Anthony. Boundary-layer flows with short-scale spanwise disturbances.

Degree: PhD, 2018, University of Manchester

 This work considers the three-dimensional laminar boundary layer on a semi-infinite plate aligned with a uniform oncoming stream or driven by a favourable pressure gradient… (more)

Subjects/Keywords: Boundary-layer; Short spanwise scale; Injection; Stability

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APA (6th Edition):

Williams, A. (2018). Boundary-layer flows with short-scale spanwise disturbances. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/boundarylayer-flows-with-shortscale-spanwise-disturbances(4c50004f-5f0c-4252-9adb-680d18cb36e1).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.771371

Chicago Manual of Style (16th Edition):

Williams, Anthony. “Boundary-layer flows with short-scale spanwise disturbances.” 2018. Doctoral Dissertation, University of Manchester. Accessed December 16, 2019. https://www.research.manchester.ac.uk/portal/en/theses/boundarylayer-flows-with-shortscale-spanwise-disturbances(4c50004f-5f0c-4252-9adb-680d18cb36e1).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.771371.

MLA Handbook (7th Edition):

Williams, Anthony. “Boundary-layer flows with short-scale spanwise disturbances.” 2018. Web. 16 Dec 2019.

Vancouver:

Williams A. Boundary-layer flows with short-scale spanwise disturbances. [Internet] [Doctoral dissertation]. University of Manchester; 2018. [cited 2019 Dec 16]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/boundarylayer-flows-with-shortscale-spanwise-disturbances(4c50004f-5f0c-4252-9adb-680d18cb36e1).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.771371.

Council of Science Editors:

Williams A. Boundary-layer flows with short-scale spanwise disturbances. [Doctoral Dissertation]. University of Manchester; 2018. Available from: https://www.research.manchester.ac.uk/portal/en/theses/boundarylayer-flows-with-shortscale-spanwise-disturbances(4c50004f-5f0c-4252-9adb-680d18cb36e1).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.771371


Michigan State University

5. Chawla Mangal Dass. The stability of boundary layer flow subject to rotation.

Degree: PhD, Department of Mechanical Engineering, 1969, Michigan State University

Subjects/Keywords: Boundary layer; Stability

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APA (6th Edition):

Dass, C. M. (1969). The stability of boundary layer flow subject to rotation. (Doctoral Dissertation). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:44411

Chicago Manual of Style (16th Edition):

Dass, Chawla Mangal. “The stability of boundary layer flow subject to rotation.” 1969. Doctoral Dissertation, Michigan State University. Accessed December 16, 2019. http://etd.lib.msu.edu/islandora/object/etd:44411.

MLA Handbook (7th Edition):

Dass, Chawla Mangal. “The stability of boundary layer flow subject to rotation.” 1969. Web. 16 Dec 2019.

Vancouver:

Dass CM. The stability of boundary layer flow subject to rotation. [Internet] [Doctoral dissertation]. Michigan State University; 1969. [cited 2019 Dec 16]. Available from: http://etd.lib.msu.edu/islandora/object/etd:44411.

Council of Science Editors:

Dass CM. The stability of boundary layer flow subject to rotation. [Doctoral Dissertation]. Michigan State University; 1969. Available from: http://etd.lib.msu.edu/islandora/object/etd:44411


Louisiana State University

6. Tollefson, William. Effect of atmospheric boundary layer conditions on agricultural spray drift.

Degree: MS, Social and Behavioral Sciences, 2013, Louisiana State University

 Drift of pesticides can be a significant health hazard, particularly in areas where agricultural land is adjacent to a school, retirement home, or other populated… (more)

Subjects/Keywords: boundary layer; drift; spray drift; pesticides; atmospheric boundary layer; spray dispersion; pasquill stability classes; stability; atmospheric stability

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APA (6th Edition):

Tollefson, W. (2013). Effect of atmospheric boundary layer conditions on agricultural spray drift. (Masters Thesis). Louisiana State University. Retrieved from etd-11182013-120951 ; https://digitalcommons.lsu.edu/gradschool_theses/2667

Chicago Manual of Style (16th Edition):

Tollefson, William. “Effect of atmospheric boundary layer conditions on agricultural spray drift.” 2013. Masters Thesis, Louisiana State University. Accessed December 16, 2019. etd-11182013-120951 ; https://digitalcommons.lsu.edu/gradschool_theses/2667.

MLA Handbook (7th Edition):

Tollefson, William. “Effect of atmospheric boundary layer conditions on agricultural spray drift.” 2013. Web. 16 Dec 2019.

Vancouver:

Tollefson W. Effect of atmospheric boundary layer conditions on agricultural spray drift. [Internet] [Masters thesis]. Louisiana State University; 2013. [cited 2019 Dec 16]. Available from: etd-11182013-120951 ; https://digitalcommons.lsu.edu/gradschool_theses/2667.

Council of Science Editors:

Tollefson W. Effect of atmospheric boundary layer conditions on agricultural spray drift. [Masters Thesis]. Louisiana State University; 2013. Available from: etd-11182013-120951 ; https://digitalcommons.lsu.edu/gradschool_theses/2667


The Ohio State University

7. Riley, Zachary Bryce, Riley. Interaction Between Aerothermally Compliant Structures and Boundary-Layer Transition in Hypersonic Flow.

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

 The use of thin-gauge, light-weight structures in combination with the severe aero-thermodynamic loading makes reusable hypersonic cruise vehicles prone to fluid-thermal-structural interactions. These interactions result… (more)

Subjects/Keywords: Aerospace Engineering; hypersonic; boundary-layer stability; boundary-layer transition; aerothermoelastic; parabolized stability equations; surrogate modeling; kriging

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APA (6th Edition):

Riley, Zachary Bryce, R. (2016). Interaction Between Aerothermally Compliant Structures and Boundary-Layer Transition in Hypersonic Flow. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1471618528

Chicago Manual of Style (16th Edition):

Riley, Zachary Bryce, Riley. “Interaction Between Aerothermally Compliant Structures and Boundary-Layer Transition in Hypersonic Flow.” 2016. Doctoral Dissertation, The Ohio State University. Accessed December 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1471618528.

MLA Handbook (7th Edition):

Riley, Zachary Bryce, Riley. “Interaction Between Aerothermally Compliant Structures and Boundary-Layer Transition in Hypersonic Flow.” 2016. Web. 16 Dec 2019.

Vancouver:

Riley, Zachary Bryce R. Interaction Between Aerothermally Compliant Structures and Boundary-Layer Transition in Hypersonic Flow. [Internet] [Doctoral dissertation]. The Ohio State University; 2016. [cited 2019 Dec 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1471618528.

Council of Science Editors:

Riley, Zachary Bryce R. Interaction Between Aerothermally Compliant Structures and Boundary-Layer Transition in Hypersonic Flow. [Doctoral Dissertation]. The Ohio State University; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1471618528

8. Denissen, Nicholas Allen. Roughness-induced Transient Growth: Continuous-spectrum Receptivity and Secondary Instability Analysis.

Degree: 2012, Texas A&M University

 This dissertation analyzes the effect of periodic roughness elements on the stability of a flat plate boundary layer. Receptivity data is extracted from direct numerical… (more)

Subjects/Keywords: boundary layer stability; transition

…the results of secondary stability calculations for a model boundary layer based on optimal… …118 3 Complex plane of the Orr–Sommerfeld equation for boundary layer flow… …to occur lower in the boundary layer . 124 14 λk /3 continuous spectrum amplitudes for… …thickness δavg (x) Average boundary layer thickness λk Roughness element spacing k… …sufficient amplitude that their distortion of the boundary layer becomes significant. This leads to… 

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

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APA (6th Edition):

Denissen, N. A. (2012). Roughness-induced Transient Growth: Continuous-spectrum Receptivity and Secondary Instability Analysis. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9192

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):

Denissen, Nicholas Allen. “Roughness-induced Transient Growth: Continuous-spectrum Receptivity and Secondary Instability Analysis.” 2012. Thesis, Texas A&M University. Accessed December 16, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9192.

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

MLA Handbook (7th Edition):

Denissen, Nicholas Allen. “Roughness-induced Transient Growth: Continuous-spectrum Receptivity and Secondary Instability Analysis.” 2012. Web. 16 Dec 2019.

Vancouver:

Denissen NA. Roughness-induced Transient Growth: Continuous-spectrum Receptivity and Secondary Instability Analysis. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9192.

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

Council of Science Editors:

Denissen NA. Roughness-induced Transient Growth: Continuous-spectrum Receptivity and Secondary Instability Analysis. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9192

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


University of Minnesota

9. 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 December 16, 2019. http://purl.umn.edu/156851.

MLA Handbook (7th Edition):

Kirk, Lindsay Christine. “Geometric effects on the amplification of first mode instability waves.” 2013. Web. 16 Dec 2019.

Vancouver:

Kirk LC. Geometric effects on the amplification of first mode instability waves. [Internet] [Masters thesis]. University of Minnesota; 2013. [cited 2019 Dec 16]. 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 Cincinnati

10. Davis, John Matthew. An investigation into the effect of surface-mounted circular obstructions on flow driven diffusion flames.

Degree: MS, Engineering : Aerospace Engineering, 2009, University of Cincinnati

 With little data currently available, designers of aircraft engine nacelle fire-test simulators have little basis to determine the size of geometric detail required to provide… (more)

Subjects/Keywords: Fluid Dynamics; Shear Flow; Surface Mounted Obstructions; Boundary Layer; Flame Stability

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APA (6th Edition):

Davis, J. M. (2009). An investigation into the effect of surface-mounted circular obstructions on flow driven diffusion flames. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1236291952

Chicago Manual of Style (16th Edition):

Davis, John Matthew. “An investigation into the effect of surface-mounted circular obstructions on flow driven diffusion flames.” 2009. Masters Thesis, University of Cincinnati. Accessed December 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1236291952.

MLA Handbook (7th Edition):

Davis, John Matthew. “An investigation into the effect of surface-mounted circular obstructions on flow driven diffusion flames.” 2009. Web. 16 Dec 2019.

Vancouver:

Davis JM. An investigation into the effect of surface-mounted circular obstructions on flow driven diffusion flames. [Internet] [Masters thesis]. University of Cincinnati; 2009. [cited 2019 Dec 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1236291952.

Council of Science Editors:

Davis JM. An investigation into the effect of surface-mounted circular obstructions on flow driven diffusion flames. [Masters Thesis]. University of Cincinnati; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1236291952


Baylor University

11. [No author]. Linear stability analysis of Mach 10 nitrogen flow over 7-deg half-angle cones.

Degree: 2017, Baylor University

 Linear stability theory (LST) analysis was performed on Mach 10 7-degree half-angle straight cones in nitrogen for comparison with experimental results obtained in the Arnold… (more)

Subjects/Keywords: Hypersonic. Boundary layer. Stability. Transition. Cone. Mach 10. Nitrogen.

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APA (6th Edition):

author], [. (2017). Linear stability analysis of Mach 10 nitrogen flow over 7-deg half-angle cones. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/10164

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. “Linear stability analysis of Mach 10 nitrogen flow over 7-deg half-angle cones. ” 2017. Thesis, Baylor University. Accessed December 16, 2019. http://hdl.handle.net/2104/10164.

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. “Linear stability analysis of Mach 10 nitrogen flow over 7-deg half-angle cones. ” 2017. Web. 16 Dec 2019.

Vancouver:

author] [. Linear stability analysis of Mach 10 nitrogen flow over 7-deg half-angle cones. [Internet] [Thesis]. Baylor University; 2017. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/2104/10164.

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

Council of Science Editors:

author] [. Linear stability analysis of Mach 10 nitrogen flow over 7-deg half-angle cones. [Thesis]. Baylor University; 2017. Available from: http://hdl.handle.net/2104/10164

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


University of Minnesota

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

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 December 16, 2019. http://purl.umn.edu/156851.

MLA Handbook (7th Edition):

Kirk, Lindsay Christine. “Geometric effects on the amplification of first mode instability waves.” 2013. Web. 16 Dec 2019.

Vancouver:

Kirk LC. Geometric effects on the amplification of first mode instability waves. [Internet] [Masters thesis]. University of Minnesota; 2013. [cited 2019 Dec 16]. 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


Purdue University

13. Lakebrink, Matthew T. Numerical Investigation of Crossflow Instability on the HIFiRE-5.

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

Stability analysis was performed with the Langley Stability and Transition Analysis Code (LASTRAC) on a 38.1% scale model of the HIFiRE-5 elliptic-cone forebody to… (more)

Subjects/Keywords: Applied sciences; Aerodynamic; Boundary layer; Crossflow; Hypersonic; Stability; Transition; Aerospace Engineering

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APA (6th Edition):

Lakebrink, M. T. (2016). Numerical Investigation of Crossflow Instability on the HIFiRE-5. (Doctoral Dissertation). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_dissertations/962

Chicago Manual of Style (16th Edition):

Lakebrink, Matthew T. “Numerical Investigation of Crossflow Instability on the HIFiRE-5.” 2016. Doctoral Dissertation, Purdue University. Accessed December 16, 2019. https://docs.lib.purdue.edu/open_access_dissertations/962.

MLA Handbook (7th Edition):

Lakebrink, Matthew T. “Numerical Investigation of Crossflow Instability on the HIFiRE-5.” 2016. Web. 16 Dec 2019.

Vancouver:

Lakebrink MT. Numerical Investigation of Crossflow Instability on the HIFiRE-5. [Internet] [Doctoral dissertation]. Purdue University; 2016. [cited 2019 Dec 16]. Available from: https://docs.lib.purdue.edu/open_access_dissertations/962.

Council of Science Editors:

Lakebrink MT. Numerical Investigation of Crossflow Instability on the HIFiRE-5. [Doctoral Dissertation]. Purdue University; 2016. Available from: https://docs.lib.purdue.edu/open_access_dissertations/962


Texas A&M University

14. Oliviero, Nick B. EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver.

Degree: 2015, Texas A&M University

 Recent years have witnessed the linear and nonlinear parabolized stability equations (PSE) become a quintessential component toward understanding boundary-layer laminarto-turbulent transition. Because of the abundant… (more)

Subjects/Keywords: aerospace; hypersonic; boundary-layer transition; stability; parabolized stability equations; PSE; NPSE; LPSE

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APA (6th Edition):

Oliviero, N. B. (2015). EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/155252

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):

Oliviero, Nick B. “EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver.” 2015. Thesis, Texas A&M University. Accessed December 16, 2019. http://hdl.handle.net/1969.1/155252.

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

MLA Handbook (7th Edition):

Oliviero, Nick B. “EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver.” 2015. Web. 16 Dec 2019.

Vancouver:

Oliviero NB. EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver. [Internet] [Thesis]. Texas A&M University; 2015. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/1969.1/155252.

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

Council of Science Editors:

Oliviero NB. EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver. [Thesis]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/155252

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


UCLA

15. Knisely, Carleton. Supersonic Unstable Modes in Hypersonic Boundary Layers with Thermochemical Nonequilibrium Effects.

Degree: Aerospace Engineering, 2018, UCLA

 Mack’s second mode has been known to be the dominant disturbance leading to transition to turbulence in traditional hypersonic boundary layer flows at zero angle… (more)

Subjects/Keywords: Fluid mechanics; Aerospace engineering; Computational physics; acoustic; boundary layer; hypersonic; reacting flow; stability; transition

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APA (6th Edition):

Knisely, C. (2018). Supersonic Unstable Modes in Hypersonic Boundary Layers with Thermochemical Nonequilibrium Effects. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/9cj752vt

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):

Knisely, Carleton. “Supersonic Unstable Modes in Hypersonic Boundary Layers with Thermochemical Nonequilibrium Effects.” 2018. Thesis, UCLA. Accessed December 16, 2019. http://www.escholarship.org/uc/item/9cj752vt.

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

MLA Handbook (7th Edition):

Knisely, Carleton. “Supersonic Unstable Modes in Hypersonic Boundary Layers with Thermochemical Nonequilibrium Effects.” 2018. Web. 16 Dec 2019.

Vancouver:

Knisely C. Supersonic Unstable Modes in Hypersonic Boundary Layers with Thermochemical Nonequilibrium Effects. [Internet] [Thesis]. UCLA; 2018. [cited 2019 Dec 16]. Available from: http://www.escholarship.org/uc/item/9cj752vt.

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

Council of Science Editors:

Knisely C. Supersonic Unstable Modes in Hypersonic Boundary Layers with Thermochemical Nonequilibrium Effects. [Thesis]. UCLA; 2018. Available from: http://www.escholarship.org/uc/item/9cj752vt

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


Virginia Tech

16. Kanner, Howard S. Evolution of an Acoustic Disturbance to Transition in the Boundary Layer on an Airfoil.

Degree: PhD, Aerospace and Ocean Engineering, 1999, Virginia Tech

 An experiment has been conducted to examine the generation and subsequent evolution of boundary-layer disturbances on a two-dimensional airfoil up through transition to turbulent flow.… (more)

Subjects/Keywords: Tollmien-Schlichting; stability; boundary layer; transition

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APA (6th Edition):

Kanner, H. S. (1999). Evolution of an Acoustic Disturbance to Transition in the Boundary Layer on an Airfoil. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26603

Chicago Manual of Style (16th Edition):

Kanner, Howard S. “Evolution of an Acoustic Disturbance to Transition in the Boundary Layer on an Airfoil.” 1999. Doctoral Dissertation, Virginia Tech. Accessed December 16, 2019. http://hdl.handle.net/10919/26603.

MLA Handbook (7th Edition):

Kanner, Howard S. “Evolution of an Acoustic Disturbance to Transition in the Boundary Layer on an Airfoil.” 1999. Web. 16 Dec 2019.

Vancouver:

Kanner HS. Evolution of an Acoustic Disturbance to Transition in the Boundary Layer on an Airfoil. [Internet] [Doctoral dissertation]. Virginia Tech; 1999. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/10919/26603.

Council of Science Editors:

Kanner HS. Evolution of an Acoustic Disturbance to Transition in the Boundary Layer on an Airfoil. [Doctoral Dissertation]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/26603


MIT

17. Thompson, Rory Jack. Instabilities of some time-dependent flows .

Degree: PhD, Meteorology, 1968, MIT

Subjects/Keywords: Meteorology.; Stability; Fluid dynamics; Boundary layer

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APA (6th Edition):

Thompson, R. J. (1968). Instabilities of some time-dependent flows . (Doctoral Dissertation). MIT. Retrieved from http://hdl.handle.net/1721.1/58224

Chicago Manual of Style (16th Edition):

Thompson, Rory Jack. “Instabilities of some time-dependent flows .” 1968. Doctoral Dissertation, MIT. Accessed December 16, 2019. http://hdl.handle.net/1721.1/58224.

MLA Handbook (7th Edition):

Thompson, Rory Jack. “Instabilities of some time-dependent flows .” 1968. Web. 16 Dec 2019.

Vancouver:

Thompson RJ. Instabilities of some time-dependent flows . [Internet] [Doctoral dissertation]. MIT; 1968. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/1721.1/58224.

Council of Science Editors:

Thompson RJ. Instabilities of some time-dependent flows . [Doctoral Dissertation]. MIT; 1968. Available from: http://hdl.handle.net/1721.1/58224


University of Minnesota

18. Wagnild, Ross Martin. High enthalpy Effects on two boundary layer disturbances in supersonic and hypersonic flow.

Degree: PhD, Aerospace Engineering and Mechanics, 2012, University of Minnesota

 The fluid flow phenomenon of boundary layer transition is a complicated and difficult process to model and predict. The importance of the state of the… (more)

Subjects/Keywords: Acoustics; Boundary Layer Stability; Compressible Flow; High Enthalpy Flow; Second Mode Disturbance; Transient Growth

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APA (6th Edition):

Wagnild, R. M. (2012). High enthalpy Effects on two boundary layer disturbances in supersonic and hypersonic flow. (Doctoral Dissertation). University of Minnesota. Retrieved from http://purl.umn.edu/130339

Chicago Manual of Style (16th Edition):

Wagnild, Ross Martin. “High enthalpy Effects on two boundary layer disturbances in supersonic and hypersonic flow.” 2012. Doctoral Dissertation, University of Minnesota. Accessed December 16, 2019. http://purl.umn.edu/130339.

MLA Handbook (7th Edition):

Wagnild, Ross Martin. “High enthalpy Effects on two boundary layer disturbances in supersonic and hypersonic flow.” 2012. Web. 16 Dec 2019.

Vancouver:

Wagnild RM. High enthalpy Effects on two boundary layer disturbances in supersonic and hypersonic flow. [Internet] [Doctoral dissertation]. University of Minnesota; 2012. [cited 2019 Dec 16]. Available from: http://purl.umn.edu/130339.

Council of Science Editors:

Wagnild RM. High enthalpy Effects on two boundary layer disturbances in supersonic and hypersonic flow. [Doctoral Dissertation]. University of Minnesota; 2012. Available from: http://purl.umn.edu/130339


University of Arizona

19. Salemi, Leonardo da Costa. Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects .

Degree: 2016, University of Arizona

 The spatial stability of hypersonic conical boundary layers is investigated utilizing different numerical techniques. First, the development and verification of a Linearized Compressible Navier-Stokes solver… (more)

Subjects/Keywords: Boundary-Layer; High-Enthalpy; Hydrodynamic Stability; Hypersonics; Wave Packets; Aerospace Engineering; Angle-of-Attack

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APA (6th Edition):

Salemi, L. d. C. (2016). Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/621854

Chicago Manual of Style (16th Edition):

Salemi, Leonardo da Costa. “Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects .” 2016. Doctoral Dissertation, University of Arizona. Accessed December 16, 2019. http://hdl.handle.net/10150/621854.

MLA Handbook (7th Edition):

Salemi, Leonardo da Costa. “Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects .” 2016. Web. 16 Dec 2019.

Vancouver:

Salemi LdC. Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects . [Internet] [Doctoral dissertation]. University of Arizona; 2016. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/10150/621854.

Council of Science Editors:

Salemi LdC. Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects . [Doctoral Dissertation]. University of Arizona; 2016. Available from: http://hdl.handle.net/10150/621854


KTH

20. Roy, Arijit Sinha. Analysis and control of boundary layer transition on a NACA 0008 wing profile.

Degree: Mechanics, 2018, KTH

  The main aim of this thesis was to understand the mechanism behind the classical transition scenario inside the boundary layer over an airfoil and… (more)

Subjects/Keywords: boundary layer stability; laminar - turbulent transition; laminar flow control; Tollmien-Schlichting waves; streaky boundary layers; miniature vortex generators; Falkner-Skan boundary layer.; Engineering and Technology; Teknik och teknologier

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APA (6th Edition):

Roy, A. S. (2018). Analysis and control of boundary layer transition on a NACA 0008 wing profile. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931

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):

Roy, Arijit Sinha. “Analysis and control of boundary layer transition on a NACA 0008 wing profile.” 2018. Thesis, KTH. Accessed December 16, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931.

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

MLA Handbook (7th Edition):

Roy, Arijit Sinha. “Analysis and control of boundary layer transition on a NACA 0008 wing profile.” 2018. Web. 16 Dec 2019.

Vancouver:

Roy AS. Analysis and control of boundary layer transition on a NACA 0008 wing profile. [Internet] [Thesis]. KTH; 2018. [cited 2019 Dec 16]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931.

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

Council of Science Editors:

Roy AS. Analysis and control of boundary layer transition on a NACA 0008 wing profile. [Thesis]. KTH; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931

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


Texas A&M University

21. Sharp, Nicole Susanne. Hypersonic Measurements of Roughness-Induced Transient Growth.

Degree: 2014, Texas A&M University

 The effects of surface roughness on boundary-layer disturbance growth and laminar-to-turbulent transition are not well understood, especially in hypersonic boundary layers. The transient growth mechanism… (more)

Subjects/Keywords: fluid dynamics; boundary layer stability; laminar-to-turbulent transition; hypersonic flow; surface roughness; boundary layers; transient growth; nonmodal growth

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APA (6th Edition):

Sharp, N. S. (2014). Hypersonic Measurements of Roughness-Induced Transient Growth. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/152647

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):

Sharp, Nicole Susanne. “Hypersonic Measurements of Roughness-Induced Transient Growth.” 2014. Thesis, Texas A&M University. Accessed December 16, 2019. http://hdl.handle.net/1969.1/152647.

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

MLA Handbook (7th Edition):

Sharp, Nicole Susanne. “Hypersonic Measurements of Roughness-Induced Transient Growth.” 2014. Web. 16 Dec 2019.

Vancouver:

Sharp NS. Hypersonic Measurements of Roughness-Induced Transient Growth. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/1969.1/152647.

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

Council of Science Editors:

Sharp NS. Hypersonic Measurements of Roughness-Induced Transient Growth. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/152647

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


University of Arizona

22. Hader, Christoph. Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Flared Cone .

Degree: 2019, University of Arizona

 Direct Numerical Simulations (DNS) were carried out to investigate the laminar-turbulent transition for a flared cone at Mach 6 and zero angle of attack. The… (more)

Subjects/Keywords: boundary layer stability; compressible boundary layers; direct numerical simulations; high-speed flow; hypersonic transition; transition to turbulence

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APA (6th Edition):

Hader, C. (2019). Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Flared Cone . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/632585

Chicago Manual of Style (16th Edition):

Hader, Christoph. “Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Flared Cone .” 2019. Doctoral Dissertation, University of Arizona. Accessed December 16, 2019. http://hdl.handle.net/10150/632585.

MLA Handbook (7th Edition):

Hader, Christoph. “Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Flared Cone .” 2019. Web. 16 Dec 2019.

Vancouver:

Hader C. Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Flared Cone . [Internet] [Doctoral dissertation]. University of Arizona; 2019. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/10150/632585.

Council of Science Editors:

Hader C. Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Flared Cone . [Doctoral Dissertation]. University of Arizona; 2019. Available from: http://hdl.handle.net/10150/632585


Michigan Technological University

23. He, Xin. SLIP BOUNDARY LAYER FLOW STABILITY ANALYSIS AND MICRO-PLASMA JET END FLOW MODELLING.

Degree: PhD, Department of Mechanical Engineering-Engineering Mechanics, 2019, Michigan Technological University

  This dissertation is comprised of two parts. Part I includes the study of the compressible gas boundary layer (BL) flows over a flat plate… (more)

Subjects/Keywords: Boundary layer flow; linear stability analysis; slip boundary conditions; micro-plasma; Fluid Dynamics; Plasma and Beam Physics

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APA (6th Edition):

He, X. (2019). SLIP BOUNDARY LAYER FLOW STABILITY ANALYSIS AND MICRO-PLASMA JET END FLOW MODELLING. (Doctoral Dissertation). Michigan Technological University. Retrieved from https://digitalcommons.mtu.edu/etdr/854

Chicago Manual of Style (16th Edition):

He, Xin. “SLIP BOUNDARY LAYER FLOW STABILITY ANALYSIS AND MICRO-PLASMA JET END FLOW MODELLING.” 2019. Doctoral Dissertation, Michigan Technological University. Accessed December 16, 2019. https://digitalcommons.mtu.edu/etdr/854.

MLA Handbook (7th Edition):

He, Xin. “SLIP BOUNDARY LAYER FLOW STABILITY ANALYSIS AND MICRO-PLASMA JET END FLOW MODELLING.” 2019. Web. 16 Dec 2019.

Vancouver:

He X. SLIP BOUNDARY LAYER FLOW STABILITY ANALYSIS AND MICRO-PLASMA JET END FLOW MODELLING. [Internet] [Doctoral dissertation]. Michigan Technological University; 2019. [cited 2019 Dec 16]. Available from: https://digitalcommons.mtu.edu/etdr/854.

Council of Science Editors:

He X. SLIP BOUNDARY LAYER FLOW STABILITY ANALYSIS AND MICRO-PLASMA JET END FLOW MODELLING. [Doctoral Dissertation]. Michigan Technological University; 2019. Available from: https://digitalcommons.mtu.edu/etdr/854


Baylor University

24. [No author]. Modal analysis of aerospace and geophysical boundary layers.

Degree: 2018, Baylor University

 A linear stability code was written and used to calculate the stability of surface and bottom Ekman layers. Then, the stability of a water column… (more)

Subjects/Keywords: Fluid mechanics; boundary layer stability; ocean transport; Langmuir supercell; mode decomposition; POD; SOD; DMD; Ekman layer

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APA (6th Edition):

author], [. (2018). Modal analysis of aerospace and geophysical boundary layers. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/10385

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. “Modal analysis of aerospace and geophysical boundary layers. ” 2018. Thesis, Baylor University. Accessed December 16, 2019. http://hdl.handle.net/2104/10385.

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. “Modal analysis of aerospace and geophysical boundary layers. ” 2018. Web. 16 Dec 2019.

Vancouver:

author] [. Modal analysis of aerospace and geophysical boundary layers. [Internet] [Thesis]. Baylor University; 2018. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/2104/10385.

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

Council of Science Editors:

author] [. Modal analysis of aerospace and geophysical boundary layers. [Thesis]. Baylor University; 2018. Available from: http://hdl.handle.net/2104/10385

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


University of Houston

25. Martin, Natalie 1981-. Accurate Modeling of the Neutral and Unstable Atmospheric Boundary Layer at Horns Rev using the k-ε Method in FLUENT 6.3.

Degree: Mechanical Engineering, Department of, 2012, University of Houston

 A k-ε code is customized in FLUENT 6.3 to simulate neutral and unstable atmospheric boundary layers (ABL) derived from Monin-Obukhov (MO) similarity theory. The code… (more)

Subjects/Keywords: wind profile; k-ε turbulence method; k-epsilon; FLUENT; Horns Rev; atmospheric boundary layer; ABL; neutral boundary layer; unstable boundary layer; Monin-Obukhov similarity theory; MOST; diabatic; convective; stability; Mechanical engineering

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APA (6th Edition):

Martin, N. 1. (2012). Accurate Modeling of the Neutral and Unstable Atmospheric Boundary Layer at Horns Rev using the k-ε Method in FLUENT 6.3. (Thesis). University of Houston. Retrieved from http://hdl.handle.net/10657/855

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):

Martin, Natalie 1981-. “Accurate Modeling of the Neutral and Unstable Atmospheric Boundary Layer at Horns Rev using the k-ε Method in FLUENT 6.3.” 2012. Thesis, University of Houston. Accessed December 16, 2019. http://hdl.handle.net/10657/855.

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

MLA Handbook (7th Edition):

Martin, Natalie 1981-. “Accurate Modeling of the Neutral and Unstable Atmospheric Boundary Layer at Horns Rev using the k-ε Method in FLUENT 6.3.” 2012. Web. 16 Dec 2019.

Vancouver:

Martin N1. Accurate Modeling of the Neutral and Unstable Atmospheric Boundary Layer at Horns Rev using the k-ε Method in FLUENT 6.3. [Internet] [Thesis]. University of Houston; 2012. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/10657/855.

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

Council of Science Editors:

Martin N1. Accurate Modeling of the Neutral and Unstable Atmospheric Boundary Layer at Horns Rev using the k-ε Method in FLUENT 6.3. [Thesis]. University of Houston; 2012. Available from: http://hdl.handle.net/10657/855

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


Texas A&M University

26. Zhang, Zheng. Observational and Numerical Modeling Studies of Turbulence on the Texas-Louisiana Continental Shelf.

Degree: 2013, Texas A&M University

 Turbulent dynamics at two sites (C and D) in a hypoxic zone on the Texas- Louisiana continental shelf were studied by investigating turbulence quantities i.e.… (more)

Subjects/Keywords: turbulence; continental shelf; bottom boundary layer; two-equation turbulence models; second-moment turbulence closures; stability functions; turbulent oxygen flux; bottom hypoxia

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APA (6th Edition):

Zhang, Z. (2013). Observational and Numerical Modeling Studies of Turbulence on the Texas-Louisiana Continental Shelf. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151031

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):

Zhang, Zheng. “Observational and Numerical Modeling Studies of Turbulence on the Texas-Louisiana Continental Shelf.” 2013. Thesis, Texas A&M University. Accessed December 16, 2019. http://hdl.handle.net/1969.1/151031.

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

MLA Handbook (7th Edition):

Zhang, Zheng. “Observational and Numerical Modeling Studies of Turbulence on the Texas-Louisiana Continental Shelf.” 2013. Web. 16 Dec 2019.

Vancouver:

Zhang Z. Observational and Numerical Modeling Studies of Turbulence on the Texas-Louisiana Continental Shelf. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Dec 16]. Available from: http://hdl.handle.net/1969.1/151031.

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

Council of Science Editors:

Zhang Z. Observational and Numerical Modeling Studies of Turbulence on the Texas-Louisiana Continental Shelf. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151031

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


University of Colorado

27. Vanderwende, Brian Joseph. Exploring the Influence of Boundary Layer Stability on Wind Farms and their Interplay with the Surrounding Environment.

Degree: PhD, Atmospheric & Oceanic Sciences, 2015, University of Colorado

  There is growing awareness in the wind power industry that boundary-layer stability influences wind turbine performance in meaningful ways. Stability is inextricably tied to… (more)

Subjects/Keywords: atmospheric stability; computer modeling; low-level jets; planetary boundary layer; wind energy; Atmospheric Sciences; Power and Energy

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APA (6th Edition):

Vanderwende, B. J. (2015). Exploring the Influence of Boundary Layer Stability on Wind Farms and their Interplay with the Surrounding Environment. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/atoc_gradetds/54

Chicago Manual of Style (16th Edition):

Vanderwende, Brian Joseph. “Exploring the Influence of Boundary Layer Stability on Wind Farms and their Interplay with the Surrounding Environment.” 2015. Doctoral Dissertation, University of Colorado. Accessed December 16, 2019. http://scholar.colorado.edu/atoc_gradetds/54.

MLA Handbook (7th Edition):

Vanderwende, Brian Joseph. “Exploring the Influence of Boundary Layer Stability on Wind Farms and their Interplay with the Surrounding Environment.” 2015. Web. 16 Dec 2019.

Vancouver:

Vanderwende BJ. Exploring the Influence of Boundary Layer Stability on Wind Farms and their Interplay with the Surrounding Environment. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Dec 16]. Available from: http://scholar.colorado.edu/atoc_gradetds/54.

Council of Science Editors:

Vanderwende BJ. Exploring the Influence of Boundary Layer Stability on Wind Farms and their Interplay with the Surrounding Environment. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/atoc_gradetds/54

28. Sartor, Fulvio. Unsteadiness in transonic shock-wave/boundary layer interactions : experimental investigation and global stability analysis : Iterative coherent photon adjunction for the generation of mesoscopic quantum states of the electromagnetic field.

Degree: Docteur es, Mécanique et Physique des Fluides, 2014, Aix Marseille Université

Dans cette étude nous considérons l'interaction entre une onde de choc et une couche limite turbulente sur un écoulement transsonique sur une bosse d'un point… (more)

Subjects/Keywords: Transsonique; Onde de choc; Couche limite; Stabilité; Tremblement; Transonic; Shock wave; Boundary layer; Stability analysis; Buffet

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APA (6th Edition):

Sartor, F. (2014). Unsteadiness in transonic shock-wave/boundary layer interactions : experimental investigation and global stability analysis : Iterative coherent photon adjunction for the generation of mesoscopic quantum states of the electromagnetic field. (Doctoral Dissertation). Aix Marseille Université. Retrieved from http://www.theses.fr/2014AIXM4705

Chicago Manual of Style (16th Edition):

Sartor, Fulvio. “Unsteadiness in transonic shock-wave/boundary layer interactions : experimental investigation and global stability analysis : Iterative coherent photon adjunction for the generation of mesoscopic quantum states of the electromagnetic field.” 2014. Doctoral Dissertation, Aix Marseille Université. Accessed December 16, 2019. http://www.theses.fr/2014AIXM4705.

MLA Handbook (7th Edition):

Sartor, Fulvio. “Unsteadiness in transonic shock-wave/boundary layer interactions : experimental investigation and global stability analysis : Iterative coherent photon adjunction for the generation of mesoscopic quantum states of the electromagnetic field.” 2014. Web. 16 Dec 2019.

Vancouver:

Sartor F. Unsteadiness in transonic shock-wave/boundary layer interactions : experimental investigation and global stability analysis : Iterative coherent photon adjunction for the generation of mesoscopic quantum states of the electromagnetic field. [Internet] [Doctoral dissertation]. Aix Marseille Université 2014. [cited 2019 Dec 16]. Available from: http://www.theses.fr/2014AIXM4705.

Council of Science Editors:

Sartor F. Unsteadiness in transonic shock-wave/boundary layer interactions : experimental investigation and global stability analysis : Iterative coherent photon adjunction for the generation of mesoscopic quantum states of the electromagnetic field. [Doctoral Dissertation]. Aix Marseille Université 2014. Available from: http://www.theses.fr/2014AIXM4705

29. Gronvall, Joel Edwin. Computational study of hypersonic boundary layer stability on cones.

Degree: PhD, Aerospace Engineering and Mechanics, 2012, University of Minnesota

 Due to the complex nature of boundary layer laminar-turbulent transition in hypersonic flows and the resultant effect on the design of re-entry vehicles, there remains… (more)

Subjects/Keywords: Boundary Layer; Cones; Crossflow; Hypersonic; Stability; Transition

…presents boundary layer stability calculations which were based on the recent transition… …of great interest. In particular, boundary layer stability of two-dimensional and… …with these experiments, boundary layer analysis techniques such as linear stability theory… …boundary layer stability and are well suited to axisymmetric flows. The recent focus on the… …60 vii List of Figures 1.1 Boundary layer transition to turbulence map[2]… 

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APA (6th Edition):

Gronvall, J. E. (2012). Computational study of hypersonic boundary layer stability on cones. (Doctoral Dissertation). University of Minnesota. Retrieved from http://purl.umn.edu/143207

Chicago Manual of Style (16th Edition):

Gronvall, Joel Edwin. “Computational study of hypersonic boundary layer stability on cones.” 2012. Doctoral Dissertation, University of Minnesota. Accessed December 16, 2019. http://purl.umn.edu/143207.

MLA Handbook (7th Edition):

Gronvall, Joel Edwin. “Computational study of hypersonic boundary layer stability on cones.” 2012. Web. 16 Dec 2019.

Vancouver:

Gronvall JE. Computational study of hypersonic boundary layer stability on cones. [Internet] [Doctoral dissertation]. University of Minnesota; 2012. [cited 2019 Dec 16]. Available from: http://purl.umn.edu/143207.

Council of Science Editors:

Gronvall JE. Computational study of hypersonic boundary layer stability on cones. [Doctoral Dissertation]. University of Minnesota; 2012. Available from: http://purl.umn.edu/143207

30. Bonne, Nicolas. Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction.

Degree: Docteur es, Mécanique des fluides, 2018, Paris Saclay

 Le phénomène d’interaction onde de choc/couche limite (CL) est omniprésent en aérodynamique. De manière générale, il génère des oscillations basses fréquences qui peuvent être néfastes… (more)

Subjects/Keywords: Stabilité globale; Choc; Couche limite; Transition; Séparation; RANS; Global stability; Shock; Boundary layer; Transition; Separation; RANS; 532.059 3

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

APA (6th Edition):

Bonne, N. (2018). Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction. (Doctoral Dissertation). Paris Saclay. Retrieved from http://www.theses.fr/2018SACLX025

Chicago Manual of Style (16th Edition):

Bonne, Nicolas. “Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction.” 2018. Doctoral Dissertation, Paris Saclay. Accessed December 16, 2019. http://www.theses.fr/2018SACLX025.

MLA Handbook (7th Edition):

Bonne, Nicolas. “Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction.” 2018. Web. 16 Dec 2019.

Vancouver:

Bonne N. Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction. [Internet] [Doctoral dissertation]. Paris Saclay; 2018. [cited 2019 Dec 16]. Available from: http://www.theses.fr/2018SACLX025.

Council of Science Editors:

Bonne N. Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction. [Doctoral Dissertation]. Paris Saclay; 2018. Available from: http://www.theses.fr/2018SACLX025

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