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Texas A&M University

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

Degree: 2012, Texas A&M University

URL: http://hdl.handle.net/1969.1/148060

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

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

URL: http://hdl.handle.net/1969.1/173633

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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*-

Degree: 2019, University of Manchester

URL: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:318010

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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*-

Degree: PhD, 2018, University of Manchester

URL: 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

► 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

Record Details Similar Records

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APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://etd.lib.msu.edu/islandora/object/etd:44411

Subjects/Keywords: Boundary layer; Stability

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APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: etd-11182013-120951 ; https://digitalcommons.lsu.edu/gradschool_theses/2667

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://rave.ohiolink.edu/etdc/view?acc_num=osu1471618528

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9192

► 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…

Record Details Similar Records

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APA (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://purl.umn.edu/156851

►

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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1236291952

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2104/10164

► 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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://purl.umn.edu/156851

► 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

Record Details Similar Records

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://docs.lib.purdue.edu/open_access_dissertations/962

► *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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/1969.1/155252

► 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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://www.escholarship.org/uc/item/9cj752vt

► 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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://hdl.handle.net/10919/26603

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/1721.1/58224

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

Record Details Similar Records

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APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://purl.umn.edu/130339

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/10150/621854

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931

► 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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://hdl.handle.net/1969.1/152647

► 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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://hdl.handle.net/10150/632585

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: https://digitalcommons.mtu.edu/etdr/854

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2104/10385

► 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 (6^{th} Edition):

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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://hdl.handle.net/10657/855

► 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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://hdl.handle.net/1969.1/151031

► 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 (6^{th} 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

Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^{th} 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.

Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^{th} 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.

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

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

URL: http://scholar.colorado.edu/atoc_gradetds/54

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://www.theses.fr/2014AIXM4705

►

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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://purl.umn.edu/143207

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://www.theses.fr/2018SACLX025

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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