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You searched for subject:(swept). Showing records 1 – 30 of 95 total matches.

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University of Miami

1. Bennett, Christopher Lee. Acquisition of Otoacoustic Emissions Using Swept-Tone Techniques.

Degree: PhD, Biomedical Engineering (Engineering), 2010, University of Miami

  Otoacoustic emissions (OAEs) have been under investigation since their discovery 30 years ago (Kemp, 1978). Otoacoustic emissions are quiet sounds generated within the cochlea… (more)

Subjects/Keywords: Swept-sine Analysis; TEOAE; Time-frequency; Audiometry

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APA (6th Edition):

Bennett, C. L. (2010). Acquisition of Otoacoustic Emissions Using Swept-Tone Techniques. (Doctoral Dissertation). University of Miami. Retrieved from https://scholarlyrepository.miami.edu/oa_dissertations/454

Chicago Manual of Style (16th Edition):

Bennett, Christopher Lee. “Acquisition of Otoacoustic Emissions Using Swept-Tone Techniques.” 2010. Doctoral Dissertation, University of Miami. Accessed January 25, 2021. https://scholarlyrepository.miami.edu/oa_dissertations/454.

MLA Handbook (7th Edition):

Bennett, Christopher Lee. “Acquisition of Otoacoustic Emissions Using Swept-Tone Techniques.” 2010. Web. 25 Jan 2021.

Vancouver:

Bennett CL. Acquisition of Otoacoustic Emissions Using Swept-Tone Techniques. [Internet] [Doctoral dissertation]. University of Miami; 2010. [cited 2021 Jan 25]. Available from: https://scholarlyrepository.miami.edu/oa_dissertations/454.

Council of Science Editors:

Bennett CL. Acquisition of Otoacoustic Emissions Using Swept-Tone Techniques. [Doctoral Dissertation]. University of Miami; 2010. Available from: https://scholarlyrepository.miami.edu/oa_dissertations/454


Johannes Gutenberg Universität Mainz

2. Dziegielewski, Andreas von. High precision swept volume approximation with conservative error bounds.

Degree: 2012, Johannes Gutenberg Universität Mainz

In technical design processes in the automotive industry, digital prototypes rapidly gain importance, because they allow for a detection of design errors in early development… (more)

Subjects/Keywords: Swept Volume; Wartbarkeitsuntersuchungen; Bewegungsüllen; Bauraumuntersuchungen; Sicherheitsabstände; CAD; Swept Volume; Maintainability Analysis; Safety Analysis; CAD; Data processing Computer science

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APA (6th Edition):

Dziegielewski, A. v. (2012). High precision swept volume approximation with conservative error bounds. (Doctoral Dissertation). Johannes Gutenberg Universität Mainz. Retrieved from http://ubm.opus.hbz-nrw.de/volltexte/2012/3267/

Chicago Manual of Style (16th Edition):

Dziegielewski, Andreas von. “High precision swept volume approximation with conservative error bounds.” 2012. Doctoral Dissertation, Johannes Gutenberg Universität Mainz. Accessed January 25, 2021. http://ubm.opus.hbz-nrw.de/volltexte/2012/3267/.

MLA Handbook (7th Edition):

Dziegielewski, Andreas von. “High precision swept volume approximation with conservative error bounds.” 2012. Web. 25 Jan 2021.

Vancouver:

Dziegielewski Av. High precision swept volume approximation with conservative error bounds. [Internet] [Doctoral dissertation]. Johannes Gutenberg Universität Mainz; 2012. [cited 2021 Jan 25]. Available from: http://ubm.opus.hbz-nrw.de/volltexte/2012/3267/.

Council of Science Editors:

Dziegielewski Av. High precision swept volume approximation with conservative error bounds. [Doctoral Dissertation]. Johannes Gutenberg Universität Mainz; 2012. Available from: http://ubm.opus.hbz-nrw.de/volltexte/2012/3267/


North Carolina State University

3. Roberts, David William. The Aerodynamic Analysis and Aeroelastic Tailoring of a Forward-Swept Wing.

Degree: MS, Aerospace Engineering, 2006, North Carolina State University

 The use of forward-swept wings has aerodynamic benefits at high angles of attack and in supersonic regimes. These consist of reduction in wave drag, profile… (more)

Subjects/Keywords: Aeroelastic; Forward-Swept; Divergence

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APA (6th Edition):

Roberts, D. W. (2006). The Aerodynamic Analysis and Aeroelastic Tailoring of a Forward-Swept Wing. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/2141

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):

Roberts, David William. “The Aerodynamic Analysis and Aeroelastic Tailoring of a Forward-Swept Wing.” 2006. Thesis, North Carolina State University. Accessed January 25, 2021. http://www.lib.ncsu.edu/resolver/1840.16/2141.

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

MLA Handbook (7th Edition):

Roberts, David William. “The Aerodynamic Analysis and Aeroelastic Tailoring of a Forward-Swept Wing.” 2006. Web. 25 Jan 2021.

Vancouver:

Roberts DW. The Aerodynamic Analysis and Aeroelastic Tailoring of a Forward-Swept Wing. [Internet] [Thesis]. North Carolina State University; 2006. [cited 2021 Jan 25]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/2141.

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

Council of Science Editors:

Roberts DW. The Aerodynamic Analysis and Aeroelastic Tailoring of a Forward-Swept Wing. [Thesis]. North Carolina State University; 2006. Available from: http://www.lib.ncsu.edu/resolver/1840.16/2141

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


University of Miami

4. Mihajloski, Todor. Swept - Tone Evoked Otoacoustic Emissions: Stimulus Calibration and Equalization.

Degree: MS, Biomedical Engineering (Engineering), 2011, University of Miami

 Otoacoustic Emissions (OAE) are minute acoustic responses originating from the cochlea as a result of an external acoustic stimulus and are recorded using a sensitive… (more)

Subjects/Keywords: Otoacoustic Emissions; OAE; Swept-Tone; Hearing Level; DSP; Signal Processing

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APA (6th Edition):

Mihajloski, T. (2011). Swept - Tone Evoked Otoacoustic Emissions: Stimulus Calibration and Equalization. (Thesis). University of Miami. Retrieved from https://scholarlyrepository.miami.edu/oa_theses/301

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):

Mihajloski, Todor. “Swept - Tone Evoked Otoacoustic Emissions: Stimulus Calibration and Equalization.” 2011. Thesis, University of Miami. Accessed January 25, 2021. https://scholarlyrepository.miami.edu/oa_theses/301.

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

MLA Handbook (7th Edition):

Mihajloski, Todor. “Swept - Tone Evoked Otoacoustic Emissions: Stimulus Calibration and Equalization.” 2011. Web. 25 Jan 2021.

Vancouver:

Mihajloski T. Swept - Tone Evoked Otoacoustic Emissions: Stimulus Calibration and Equalization. [Internet] [Thesis]. University of Miami; 2011. [cited 2021 Jan 25]. Available from: https://scholarlyrepository.miami.edu/oa_theses/301.

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

Council of Science Editors:

Mihajloski T. Swept - Tone Evoked Otoacoustic Emissions: Stimulus Calibration and Equalization. [Thesis]. University of Miami; 2011. Available from: https://scholarlyrepository.miami.edu/oa_theses/301

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


Delft University of Technology

5. Sol, M.B. (author). Conceptual Design of Swept Wing Root Aerofoils.

Degree: 2015, Delft University of Technology

 For modern transonic transport aeroplanes, it is important to produce low drag at high cruise speeds. The root effect, caused by effects of symmetry on… (more)

Subjects/Keywords: conceptual; design; swept wing; wing root; aerofoil; straight isobars

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APA (6th Edition):

Sol, M. B. (. (2015). Conceptual Design of Swept Wing Root Aerofoils. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9

Chicago Manual of Style (16th Edition):

Sol, M B (author). “Conceptual Design of Swept Wing Root Aerofoils.” 2015. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9.

MLA Handbook (7th Edition):

Sol, M B (author). “Conceptual Design of Swept Wing Root Aerofoils.” 2015. Web. 25 Jan 2021.

Vancouver:

Sol MB(. Conceptual Design of Swept Wing Root Aerofoils. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9.

Council of Science Editors:

Sol MB(. Conceptual Design of Swept Wing Root Aerofoils. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9


Delft University of Technology

6. Munaro, Filippo (author). Mechanisms of boundary layer transition due to isolated roughness on swept wings: An experimental study.

Degree: 2017, Delft University of Technology

 In the context of the ongoing research regarding boundary layer transition, this project aims to study the effects of isolated cylindrical roughness elements on the… (more)

Subjects/Keywords: Aerodynamics; Transition; Boundary Layer; Swept Wing; Wind Tunnel; Isolated Roughness

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APA (6th Edition):

Munaro, F. (. (2017). Mechanisms of boundary layer transition due to isolated roughness on swept wings: An experimental study. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:bf38047c-96ea-4090-8d1a-9e5760e3f9d3

Chicago Manual of Style (16th Edition):

Munaro, Filippo (author). “Mechanisms of boundary layer transition due to isolated roughness on swept wings: An experimental study.” 2017. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:bf38047c-96ea-4090-8d1a-9e5760e3f9d3.

MLA Handbook (7th Edition):

Munaro, Filippo (author). “Mechanisms of boundary layer transition due to isolated roughness on swept wings: An experimental study.” 2017. Web. 25 Jan 2021.

Vancouver:

Munaro F(. Mechanisms of boundary layer transition due to isolated roughness on swept wings: An experimental study. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:bf38047c-96ea-4090-8d1a-9e5760e3f9d3.

Council of Science Editors:

Munaro F(. Mechanisms of boundary layer transition due to isolated roughness on swept wings: An experimental study. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:bf38047c-96ea-4090-8d1a-9e5760e3f9d3


University of Washington

7. Yoshida, William Tsuyoshi. Investigation of the Flowfield Downstream of a Discontinuous Backward-Facing Step on a Swept Flat Plate.

Degree: 2020, University of Washington

 An experimental study of a swept flat plate has been performed in the University of Washington 3’ by 3’ Low-Speed Wind Tunnel to improve the… (more)

Subjects/Keywords: Backward-facing step; Icing; Swept; Aerospace engineering; Aeronautics and astronautics

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APA (6th Edition):

Yoshida, W. T. (2020). Investigation of the Flowfield Downstream of a Discontinuous Backward-Facing Step on a Swept Flat Plate. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/46362

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):

Yoshida, William Tsuyoshi. “Investigation of the Flowfield Downstream of a Discontinuous Backward-Facing Step on a Swept Flat Plate.” 2020. Thesis, University of Washington. Accessed January 25, 2021. http://hdl.handle.net/1773/46362.

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

MLA Handbook (7th Edition):

Yoshida, William Tsuyoshi. “Investigation of the Flowfield Downstream of a Discontinuous Backward-Facing Step on a Swept Flat Plate.” 2020. Web. 25 Jan 2021.

Vancouver:

Yoshida WT. Investigation of the Flowfield Downstream of a Discontinuous Backward-Facing Step on a Swept Flat Plate. [Internet] [Thesis]. University of Washington; 2020. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1773/46362.

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

Council of Science Editors:

Yoshida WT. Investigation of the Flowfield Downstream of a Discontinuous Backward-Facing Step on a Swept Flat Plate. [Thesis]. University of Washington; 2020. Available from: http://hdl.handle.net/1773/46362

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


University of Arizona

8. Gluck, Jeffrey Weston. Water Tunnel Experiments on Span-wise Variation of Laminar Separation Bubbles for Swept and Unswept Wings using Particle Image Velocimetry .

Degree: 2016, University of Arizona

 An inverted airfoil mounted above a flat plate was used to create laminar separation bubbles on a flat plate in water tunnel experiments at low… (more)

Subjects/Keywords: Swept; Unswept; Water Tunnel; Wing; Aerospace Engineering; PIV

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APA (6th Edition):

Gluck, J. W. (2016). Water Tunnel Experiments on Span-wise Variation of Laminar Separation Bubbles for Swept and Unswept Wings using Particle Image Velocimetry . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/621851

Chicago Manual of Style (16th Edition):

Gluck, Jeffrey Weston. “Water Tunnel Experiments on Span-wise Variation of Laminar Separation Bubbles for Swept and Unswept Wings using Particle Image Velocimetry .” 2016. Masters Thesis, University of Arizona. Accessed January 25, 2021. http://hdl.handle.net/10150/621851.

MLA Handbook (7th Edition):

Gluck, Jeffrey Weston. “Water Tunnel Experiments on Span-wise Variation of Laminar Separation Bubbles for Swept and Unswept Wings using Particle Image Velocimetry .” 2016. Web. 25 Jan 2021.

Vancouver:

Gluck JW. Water Tunnel Experiments on Span-wise Variation of Laminar Separation Bubbles for Swept and Unswept Wings using Particle Image Velocimetry . [Internet] [Masters thesis]. University of Arizona; 2016. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10150/621851.

Council of Science Editors:

Gluck JW. Water Tunnel Experiments on Span-wise Variation of Laminar Separation Bubbles for Swept and Unswept Wings using Particle Image Velocimetry . [Masters Thesis]. University of Arizona; 2016. Available from: http://hdl.handle.net/10150/621851


University of Arizona

9. Yamauchi, Atsushi. Limitations of Reynolds Averaging in Forced Skewed Turbulent Mixing Layer .

Degree: 2019, University of Arizona

 An experimental investigation aimed at studying the three-dimensional character of a turbulent mixing layer created downstream of a swept-back wing that served as a splitter… (more)

Subjects/Keywords: Mixing layer; Reynolds Averaging; Skewed Turbulent Mixing; Swept-back Wing

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APA (6th Edition):

Yamauchi, A. (2019). Limitations of Reynolds Averaging in Forced Skewed Turbulent Mixing Layer . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/636915

Chicago Manual of Style (16th Edition):

Yamauchi, Atsushi. “Limitations of Reynolds Averaging in Forced Skewed Turbulent Mixing Layer .” 2019. Masters Thesis, University of Arizona. Accessed January 25, 2021. http://hdl.handle.net/10150/636915.

MLA Handbook (7th Edition):

Yamauchi, Atsushi. “Limitations of Reynolds Averaging in Forced Skewed Turbulent Mixing Layer .” 2019. Web. 25 Jan 2021.

Vancouver:

Yamauchi A. Limitations of Reynolds Averaging in Forced Skewed Turbulent Mixing Layer . [Internet] [Masters thesis]. University of Arizona; 2019. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10150/636915.

Council of Science Editors:

Yamauchi A. Limitations of Reynolds Averaging in Forced Skewed Turbulent Mixing Layer . [Masters Thesis]. University of Arizona; 2019. Available from: http://hdl.handle.net/10150/636915


Cal Poly

10. Egorov, Jacob. Wavelength accuracy study for high-density Fiber Bragg grating sensor systems using a Rapidly-Swept Akinetic-Laser source.

Degree: MS, Electrical Engineering, 2016, Cal Poly

  This thesis studies the center wavelength accuracy of a Fiber Bragg Grating Sensor system that has a large number of sensor elements both as… (more)

Subjects/Keywords: photonics; laser; optics; fiber; bragg grating; swept; Electromagnetics and Photonics

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APA (6th Edition):

Egorov, J. (2016). Wavelength accuracy study for high-density Fiber Bragg grating sensor systems using a Rapidly-Swept Akinetic-Laser source. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1654 ; 10.15368/theses.2016.113

Chicago Manual of Style (16th Edition):

Egorov, Jacob. “Wavelength accuracy study for high-density Fiber Bragg grating sensor systems using a Rapidly-Swept Akinetic-Laser source.” 2016. Masters Thesis, Cal Poly. Accessed January 25, 2021. https://digitalcommons.calpoly.edu/theses/1654 ; 10.15368/theses.2016.113.

MLA Handbook (7th Edition):

Egorov, Jacob. “Wavelength accuracy study for high-density Fiber Bragg grating sensor systems using a Rapidly-Swept Akinetic-Laser source.” 2016. Web. 25 Jan 2021.

Vancouver:

Egorov J. Wavelength accuracy study for high-density Fiber Bragg grating sensor systems using a Rapidly-Swept Akinetic-Laser source. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2021 Jan 25]. Available from: https://digitalcommons.calpoly.edu/theses/1654 ; 10.15368/theses.2016.113.

Council of Science Editors:

Egorov J. Wavelength accuracy study for high-density Fiber Bragg grating sensor systems using a Rapidly-Swept Akinetic-Laser source. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1654 ; 10.15368/theses.2016.113


Georgia Tech

11. Rowe, William Thomas. Analysis of wind-tunnel investigations of trailing-edge flaps on swept-back wings.

Degree: MS, Aeronautical Engineering, 1950, Georgia Tech

Subjects/Keywords: Aerodynamics; Airplanes Wings, Swept-back

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APA (6th Edition):

Rowe, W. T. (1950). Analysis of wind-tunnel investigations of trailing-edge flaps on swept-back wings. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/11967

Chicago Manual of Style (16th Edition):

Rowe, William Thomas. “Analysis of wind-tunnel investigations of trailing-edge flaps on swept-back wings.” 1950. Masters Thesis, Georgia Tech. Accessed January 25, 2021. http://hdl.handle.net/1853/11967.

MLA Handbook (7th Edition):

Rowe, William Thomas. “Analysis of wind-tunnel investigations of trailing-edge flaps on swept-back wings.” 1950. Web. 25 Jan 2021.

Vancouver:

Rowe WT. Analysis of wind-tunnel investigations of trailing-edge flaps on swept-back wings. [Internet] [Masters thesis]. Georgia Tech; 1950. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1853/11967.

Council of Science Editors:

Rowe WT. Analysis of wind-tunnel investigations of trailing-edge flaps on swept-back wings. [Masters Thesis]. Georgia Tech; 1950. Available from: http://hdl.handle.net/1853/11967


Georgia Tech

12. Eason, William Myron. An investigation of sweptback wing root stresses.

Degree: MS, Aeronautical Engineering, 1955, Georgia Tech

Subjects/Keywords: Airplanes Wings; Swept-back

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APA (6th Edition):

Eason, W. M. (1955). An investigation of sweptback wing root stresses. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12330

Chicago Manual of Style (16th Edition):

Eason, William Myron. “An investigation of sweptback wing root stresses.” 1955. Masters Thesis, Georgia Tech. Accessed January 25, 2021. http://hdl.handle.net/1853/12330.

MLA Handbook (7th Edition):

Eason, William Myron. “An investigation of sweptback wing root stresses.” 1955. Web. 25 Jan 2021.

Vancouver:

Eason WM. An investigation of sweptback wing root stresses. [Internet] [Masters thesis]. Georgia Tech; 1955. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1853/12330.

Council of Science Editors:

Eason WM. An investigation of sweptback wing root stresses. [Masters Thesis]. Georgia Tech; 1955. Available from: http://hdl.handle.net/1853/12330


Georgia Tech

13. Powers, Sidney Alan. The effect of the ground plane on low aspect ratio swept wings.

Degree: MS, Aeronautical Engineering, 1955, Georgia Tech

Subjects/Keywords: Airplanes Wings; Swept-back

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APA (6th Edition):

Powers, S. A. (1955). The effect of the ground plane on low aspect ratio swept wings. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/13073

Chicago Manual of Style (16th Edition):

Powers, Sidney Alan. “The effect of the ground plane on low aspect ratio swept wings.” 1955. Masters Thesis, Georgia Tech. Accessed January 25, 2021. http://hdl.handle.net/1853/13073.

MLA Handbook (7th Edition):

Powers, Sidney Alan. “The effect of the ground plane on low aspect ratio swept wings.” 1955. Web. 25 Jan 2021.

Vancouver:

Powers SA. The effect of the ground plane on low aspect ratio swept wings. [Internet] [Masters thesis]. Georgia Tech; 1955. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1853/13073.

Council of Science Editors:

Powers SA. The effect of the ground plane on low aspect ratio swept wings. [Masters Thesis]. Georgia Tech; 1955. Available from: http://hdl.handle.net/1853/13073


Lehigh University

14. Rumbaugh, Jr., Douglas Bahr. A Design Proposal for a Novel Gun-Launched Unmanned Aerial System.

Degree: MS, Mechanical Engineering, 2018, Lehigh University

 A proposed design for a gun-launched, unmanned aerial system (GLUAS) is presented, along with experimental data pertaining to the characterization of said design, and specifically… (more)

Subjects/Keywords: flexibility; MAV; steady flow; swept wing; UAS; UAV; Mechanical Engineering

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APA (6th Edition):

Rumbaugh, Jr., D. B. (2018). A Design Proposal for a Novel Gun-Launched Unmanned Aerial System. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/4318

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):

Rumbaugh, Jr., Douglas Bahr. “A Design Proposal for a Novel Gun-Launched Unmanned Aerial System.” 2018. Thesis, Lehigh University. Accessed January 25, 2021. https://preserve.lehigh.edu/etd/4318.

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

MLA Handbook (7th Edition):

Rumbaugh, Jr., Douglas Bahr. “A Design Proposal for a Novel Gun-Launched Unmanned Aerial System.” 2018. Web. 25 Jan 2021.

Vancouver:

Rumbaugh, Jr. DB. A Design Proposal for a Novel Gun-Launched Unmanned Aerial System. [Internet] [Thesis]. Lehigh University; 2018. [cited 2021 Jan 25]. Available from: https://preserve.lehigh.edu/etd/4318.

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

Council of Science Editors:

Rumbaugh, Jr. DB. A Design Proposal for a Novel Gun-Launched Unmanned Aerial System. [Thesis]. Lehigh University; 2018. Available from: https://preserve.lehigh.edu/etd/4318

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


Utah State University

15. Reid, Jackson T. A General Approach to Lifting-Line Theory, Applied to Wings with Sweep.

Degree: PhD, Mechanical and Aerospace Engineering, 2020, Utah State University

  Lifting-line theory is one simple method of predicting the lift produced by a wing. The traditional implementation of lifting-line theory, developed in 1918, is… (more)

Subjects/Keywords: Lifting-line theory; swept wings; airfoil; vortex; lift; Aerospace Engineering

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APA (6th Edition):

Reid, J. T. (2020). A General Approach to Lifting-Line Theory, Applied to Wings with Sweep. (Doctoral Dissertation). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/7842

Chicago Manual of Style (16th Edition):

Reid, Jackson T. “A General Approach to Lifting-Line Theory, Applied to Wings with Sweep.” 2020. Doctoral Dissertation, Utah State University. Accessed January 25, 2021. https://digitalcommons.usu.edu/etd/7842.

MLA Handbook (7th Edition):

Reid, Jackson T. “A General Approach to Lifting-Line Theory, Applied to Wings with Sweep.” 2020. Web. 25 Jan 2021.

Vancouver:

Reid JT. A General Approach to Lifting-Line Theory, Applied to Wings with Sweep. [Internet] [Doctoral dissertation]. Utah State University; 2020. [cited 2021 Jan 25]. Available from: https://digitalcommons.usu.edu/etd/7842.

Council of Science Editors:

Reid JT. A General Approach to Lifting-Line Theory, Applied to Wings with Sweep. [Doctoral Dissertation]. Utah State University; 2020. Available from: https://digitalcommons.usu.edu/etd/7842

16. Diebold, Jeffrey. Aerodynamics of a swept wing with leading-edge ice at low Reynolds number.

Degree: MS, 4048, 2012, University of Illinois – Urbana-Champaign

 An experimental study of the aerodynamics of a swept wing with ice at low Reynolds number has been performed. The goal of this work was… (more)

Subjects/Keywords: aircraft icing; swept wing icing; swept wing aerodynamics

…List of Figures Fig. 2.1 Diagram of swept wing… …20 Fig. 2.3 Lift coefficient distribution of a swept wing. Adapted from Katz… …21 Fig. 2.4 Example of staggered pressure distribution on a swept wing… …29 vii Fig. 2.18 Effect of Reynolds number on the lift of a swept wing with ΛLE= 50º… …35 Fig. 2.29 Ice accretion on a swept wing in glaze icing conditions. Arrows indicate… 

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APA (6th Edition):

Diebold, J. (2012). Aerodynamics of a swept wing with leading-edge ice at low Reynolds number. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/34279

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):

Diebold, Jeffrey. “Aerodynamics of a swept wing with leading-edge ice at low Reynolds number.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed January 25, 2021. http://hdl.handle.net/2142/34279.

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

MLA Handbook (7th Edition):

Diebold, Jeffrey. “Aerodynamics of a swept wing with leading-edge ice at low Reynolds number.” 2012. Web. 25 Jan 2021.

Vancouver:

Diebold J. Aerodynamics of a swept wing with leading-edge ice at low Reynolds number. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/2142/34279.

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

Council of Science Editors:

Diebold J. Aerodynamics of a swept wing with leading-edge ice at low Reynolds number. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/34279

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

17. Ueda, Naoko. Macular Choroidal Thickness and Volume of Eyes With Reticular Pseudodrusen Using Swept-Source Optical Coherence Tomography : 波長掃引光源型光干渉断層計を用いたreticular pseudodrusen眼の黄斑部脈絡膜厚および体積の検討.

Degree: 博士(医学), 2016, Kyoto University / 京都大学

Final publication is available at http://www.sciencedirect.com/science/article/pii/S0002939414000488

新制・課程博士

甲第19586号

医博第4093号

Subjects/Keywords: reticular pseudodrusen; choroidal thickness; swept-source optical coherence tomography; age-related macular degeneration; drusen

Page 1 Page 2

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APA (6th Edition):

Ueda, N. (2016). Macular Choroidal Thickness and Volume of Eyes With Reticular Pseudodrusen Using Swept-Source Optical Coherence Tomography : 波長掃引光源型光干渉断層計を用いたreticular pseudodrusen眼の黄斑部脈絡膜厚および体積の検討. (Thesis). Kyoto University / 京都大学. Retrieved from http://hdl.handle.net/2433/215412 ; http://dx.doi.org/10.14989/doctor.k19586

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):

Ueda, Naoko. “Macular Choroidal Thickness and Volume of Eyes With Reticular Pseudodrusen Using Swept-Source Optical Coherence Tomography : 波長掃引光源型光干渉断層計を用いたreticular pseudodrusen眼の黄斑部脈絡膜厚および体積の検討.” 2016. Thesis, Kyoto University / 京都大学. Accessed January 25, 2021. http://hdl.handle.net/2433/215412 ; http://dx.doi.org/10.14989/doctor.k19586.

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

MLA Handbook (7th Edition):

Ueda, Naoko. “Macular Choroidal Thickness and Volume of Eyes With Reticular Pseudodrusen Using Swept-Source Optical Coherence Tomography : 波長掃引光源型光干渉断層計を用いたreticular pseudodrusen眼の黄斑部脈絡膜厚および体積の検討.” 2016. Web. 25 Jan 2021.

Vancouver:

Ueda N. Macular Choroidal Thickness and Volume of Eyes With Reticular Pseudodrusen Using Swept-Source Optical Coherence Tomography : 波長掃引光源型光干渉断層計を用いたreticular pseudodrusen眼の黄斑部脈絡膜厚および体積の検討. [Internet] [Thesis]. Kyoto University / 京都大学; 2016. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/2433/215412 ; http://dx.doi.org/10.14989/doctor.k19586.

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

Council of Science Editors:

Ueda N. Macular Choroidal Thickness and Volume of Eyes With Reticular Pseudodrusen Using Swept-Source Optical Coherence Tomography : 波長掃引光源型光干渉断層計を用いたreticular pseudodrusen眼の黄斑部脈絡膜厚および体積の検討. [Thesis]. Kyoto University / 京都大学; 2016. Available from: http://hdl.handle.net/2433/215412 ; http://dx.doi.org/10.14989/doctor.k19586

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


University of Alabama

18. Lozes, Brian Andrew. Vibration absorber implementation for space launch vehicle vibration reduction.

Degree: 2010, University of Alabama

 Vibration is a major problem in space launch vehicles during burning sequences. These vehicles are vulnerable to impulsive and pulsed vibrations like those produced by… (more)

Subjects/Keywords: Electronic Thesis or Dissertation;  – thesis; Engineering, Mechanical; Gliding Tone; Modal Analysis; Swept Input; Vibration

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APA (6th Edition):

Lozes, B. A. (2010). Vibration absorber implementation for space launch vehicle vibration reduction. (Thesis). University of Alabama. Retrieved from http://purl.lib.ua.edu/16198

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):

Lozes, Brian Andrew. “Vibration absorber implementation for space launch vehicle vibration reduction.” 2010. Thesis, University of Alabama. Accessed January 25, 2021. http://purl.lib.ua.edu/16198.

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

MLA Handbook (7th Edition):

Lozes, Brian Andrew. “Vibration absorber implementation for space launch vehicle vibration reduction.” 2010. Web. 25 Jan 2021.

Vancouver:

Lozes BA. Vibration absorber implementation for space launch vehicle vibration reduction. [Internet] [Thesis]. University of Alabama; 2010. [cited 2021 Jan 25]. Available from: http://purl.lib.ua.edu/16198.

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

Council of Science Editors:

Lozes BA. Vibration absorber implementation for space launch vehicle vibration reduction. [Thesis]. University of Alabama; 2010. Available from: http://purl.lib.ua.edu/16198

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


Texas A&M University

19. Carbajal, Esteban Franco. Integrating OCT into Surgical Systems and Monitoring Vibrations.

Degree: MS, Biomedical Engineering, 2016, Texas A&M University

 Imaging of the hearing structures can yield information regarding their function as well as insight into the abnormalities and adverse conditions that affect them. Improvements… (more)

Subjects/Keywords: Optical Coherence Tomography; OCT; Imaging; SSOCT; Swept-Source; Phase; Imaging; 3D Printing

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APA (6th Edition):

Carbajal, E. F. (2016). Integrating OCT into Surgical Systems and Monitoring Vibrations. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/187397

Chicago Manual of Style (16th Edition):

Carbajal, Esteban Franco. “Integrating OCT into Surgical Systems and Monitoring Vibrations.” 2016. Masters Thesis, Texas A&M University. Accessed January 25, 2021. http://hdl.handle.net/1969.1/187397.

MLA Handbook (7th Edition):

Carbajal, Esteban Franco. “Integrating OCT into Surgical Systems and Monitoring Vibrations.” 2016. Web. 25 Jan 2021.

Vancouver:

Carbajal EF. Integrating OCT into Surgical Systems and Monitoring Vibrations. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1969.1/187397.

Council of Science Editors:

Carbajal EF. Integrating OCT into Surgical Systems and Monitoring Vibrations. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/187397


Texas A&M University

20. Tofighi Zavareh, Amir. Systems and Methods for the Spectral Calibration of Swept Source Optical Coherence Tomography Systems.

Degree: PhD, Electrical Engineering, 2019, Texas A&M University

 This dissertation relates to the transition of the state of the art of swept source optical coherence tomography (SS-OCT) systems to a new realm in… (more)

Subjects/Keywords: Optical Coherence Tomography; Swept Source Optical Coherence Tomography; Spectral Calibration; Machine Learning; Kalman Filtering

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APA (6th Edition):

Tofighi Zavareh, A. (2019). Systems and Methods for the Spectral Calibration of Swept Source Optical Coherence Tomography Systems. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/188806

Chicago Manual of Style (16th Edition):

Tofighi Zavareh, Amir. “Systems and Methods for the Spectral Calibration of Swept Source Optical Coherence Tomography Systems.” 2019. Doctoral Dissertation, Texas A&M University. Accessed January 25, 2021. http://hdl.handle.net/1969.1/188806.

MLA Handbook (7th Edition):

Tofighi Zavareh, Amir. “Systems and Methods for the Spectral Calibration of Swept Source Optical Coherence Tomography Systems.” 2019. Web. 25 Jan 2021.

Vancouver:

Tofighi Zavareh A. Systems and Methods for the Spectral Calibration of Swept Source Optical Coherence Tomography Systems. [Internet] [Doctoral dissertation]. Texas A&M University; 2019. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1969.1/188806.

Council of Science Editors:

Tofighi Zavareh A. Systems and Methods for the Spectral Calibration of Swept Source Optical Coherence Tomography Systems. [Doctoral Dissertation]. Texas A&M University; 2019. Available from: http://hdl.handle.net/1969.1/188806


University of Toronto

21. Felts Almog, Ilan. Endoscopic Full-Field Swept-Source Optical Coherence Tomography Neuroimaging System.

Degree: 2018, University of Toronto

Optical Coherence Tomography (OCT) has the capability to differentiate brain elements with intrinsic contrast and at a resolution an order-of-magnitude higher than other imaging modalities.… (more)

Subjects/Keywords: endoscopic; full-field; neuroimaging; optical coherence tomography; stereotactic surgery; swept-source; 0544

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APA (6th Edition):

Felts Almog, I. (2018). Endoscopic Full-Field Swept-Source Optical Coherence Tomography Neuroimaging System. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/82908

Chicago Manual of Style (16th Edition):

Felts Almog, Ilan. “Endoscopic Full-Field Swept-Source Optical Coherence Tomography Neuroimaging System.” 2018. Masters Thesis, University of Toronto. Accessed January 25, 2021. http://hdl.handle.net/1807/82908.

MLA Handbook (7th Edition):

Felts Almog, Ilan. “Endoscopic Full-Field Swept-Source Optical Coherence Tomography Neuroimaging System.” 2018. Web. 25 Jan 2021.

Vancouver:

Felts Almog I. Endoscopic Full-Field Swept-Source Optical Coherence Tomography Neuroimaging System. [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1807/82908.

Council of Science Editors:

Felts Almog I. Endoscopic Full-Field Swept-Source Optical Coherence Tomography Neuroimaging System. [Masters Thesis]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/82908


University of Washington

22. Sandhu, Navdeep. Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number.

Degree: 2018, University of Washington

 This thesis studied the aerodynamic effects of a single high-fidelity scalloped ice accretion simulation and a low-fidelity simulation of the same shape. These data were… (more)

Subjects/Keywords: aerodynamics; aircraft icing; CRM65; swept wing; wake survey; Aerospace engineering; Aeronautics and astronautics

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APA (6th Edition):

Sandhu, N. (2018). Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/42162

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):

Sandhu, Navdeep. “Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number.” 2018. Thesis, University of Washington. Accessed January 25, 2021. http://hdl.handle.net/1773/42162.

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

MLA Handbook (7th Edition):

Sandhu, Navdeep. “Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number.” 2018. Web. 25 Jan 2021.

Vancouver:

Sandhu N. Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number. [Internet] [Thesis]. University of Washington; 2018. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1773/42162.

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

Council of Science Editors:

Sandhu N. Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number. [Thesis]. University of Washington; 2018. Available from: http://hdl.handle.net/1773/42162

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


Delft University of Technology

23. Camps Pons, Carlos (author). Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren.

Degree: 2019, Delft University of Technology

Transonic buffet is an aerodynamic instability that appears on aerofoils and wings at certain combinations of Mach number and angle of attack, and which limits… (more)

Subjects/Keywords: Transonic buffet; Swept Wing; Stereoscopic Particle Image Velocimetry (SPIV); Background Oriented Schlieren

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APA (6th Edition):

Camps Pons, C. (. (2019). Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c1a52829-0267-4211-bf93-109fba0db350

Chicago Manual of Style (16th Edition):

Camps Pons, Carlos (author). “Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren.” 2019. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:c1a52829-0267-4211-bf93-109fba0db350.

MLA Handbook (7th Edition):

Camps Pons, Carlos (author). “Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren.” 2019. Web. 25 Jan 2021.

Vancouver:

Camps Pons C(. Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:c1a52829-0267-4211-bf93-109fba0db350.

Council of Science Editors:

Camps Pons C(. Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:c1a52829-0267-4211-bf93-109fba0db350


University of Minnesota

24. Mullen, Michael. Experimental Techniques and Image Reconstruction for Magnetic Resonance Imaging with Inhomogeneous Fields.

Degree: PhD, Physics, 2019, University of Minnesota

 Magnetic resonance imaging is quite sensitive to experimental imperfections, necessitating extremely expensive electrical infrastructure and design requirements to permit high-quality experiments to be performed. By… (more)

Subjects/Keywords: frequency-swept pulses; magnetic resonance imaging; multidimensional pulses; parallel imaging; radiofrequency pulses; spatiotemporal

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APA (6th Edition):

Mullen, M. (2019). Experimental Techniques and Image Reconstruction for Magnetic Resonance Imaging with Inhomogeneous Fields. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/209115

Chicago Manual of Style (16th Edition):

Mullen, Michael. “Experimental Techniques and Image Reconstruction for Magnetic Resonance Imaging with Inhomogeneous Fields.” 2019. Doctoral Dissertation, University of Minnesota. Accessed January 25, 2021. http://hdl.handle.net/11299/209115.

MLA Handbook (7th Edition):

Mullen, Michael. “Experimental Techniques and Image Reconstruction for Magnetic Resonance Imaging with Inhomogeneous Fields.” 2019. Web. 25 Jan 2021.

Vancouver:

Mullen M. Experimental Techniques and Image Reconstruction for Magnetic Resonance Imaging with Inhomogeneous Fields. [Internet] [Doctoral dissertation]. University of Minnesota; 2019. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/11299/209115.

Council of Science Editors:

Mullen M. Experimental Techniques and Image Reconstruction for Magnetic Resonance Imaging with Inhomogeneous Fields. [Doctoral Dissertation]. University of Minnesota; 2019. Available from: http://hdl.handle.net/11299/209115


University of Arizona

25. Sassu, Matthew George. Software Implementation of a Combined Fluorescence and Swept Source Optical Coherence Tomography Imaging System .

Degree: 2018, University of Arizona

 This paper serves as a detailed overview of the software developed for the Falloposcope endoscope being developed by the Jennifer Barton Optics Tissue Laboratory. The… (more)

Subjects/Keywords: AlazarTech; CCD Imaging; C++/CLI; Fluorescence Imaging; SS-OCT; Swept Source Optical Coherence Tomography

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APA (6th Edition):

Sassu, M. G. (2018). Software Implementation of a Combined Fluorescence and Swept Source Optical Coherence Tomography Imaging System . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/631417

Chicago Manual of Style (16th Edition):

Sassu, Matthew George. “Software Implementation of a Combined Fluorescence and Swept Source Optical Coherence Tomography Imaging System .” 2018. Masters Thesis, University of Arizona. Accessed January 25, 2021. http://hdl.handle.net/10150/631417.

MLA Handbook (7th Edition):

Sassu, Matthew George. “Software Implementation of a Combined Fluorescence and Swept Source Optical Coherence Tomography Imaging System .” 2018. Web. 25 Jan 2021.

Vancouver:

Sassu MG. Software Implementation of a Combined Fluorescence and Swept Source Optical Coherence Tomography Imaging System . [Internet] [Masters thesis]. University of Arizona; 2018. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10150/631417.

Council of Science Editors:

Sassu MG. Software Implementation of a Combined Fluorescence and Swept Source Optical Coherence Tomography Imaging System . [Masters Thesis]. University of Arizona; 2018. Available from: http://hdl.handle.net/10150/631417


University of Arizona

26. McGee, Oliver Gregory, III. A three dimensional elasticity based solution for free vibrations of simultaneously skewed and twisted cantilever parallelepipeds.

Degree: 1988, University of Arizona

 This work is the first 3-D continuum study of the free vibration of skewed and simultaneously skewed and twisted, cantilever parallelepipeds. The purpose of this… (more)

Subjects/Keywords: Airplanes  – Wings, Swept-back.; Vibration (Aeronautics)

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APA (6th Edition):

McGee, Oliver Gregory, I. (1988). A three dimensional elasticity based solution for free vibrations of simultaneously skewed and twisted cantilever parallelepipeds. (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/184517

Chicago Manual of Style (16th Edition):

McGee, Oliver Gregory, III. “A three dimensional elasticity based solution for free vibrations of simultaneously skewed and twisted cantilever parallelepipeds. ” 1988. Doctoral Dissertation, University of Arizona. Accessed January 25, 2021. http://hdl.handle.net/10150/184517.

MLA Handbook (7th Edition):

McGee, Oliver Gregory, III. “A three dimensional elasticity based solution for free vibrations of simultaneously skewed and twisted cantilever parallelepipeds. ” 1988. Web. 25 Jan 2021.

Vancouver:

McGee, Oliver Gregory I. A three dimensional elasticity based solution for free vibrations of simultaneously skewed and twisted cantilever parallelepipeds. [Internet] [Doctoral dissertation]. University of Arizona; 1988. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10150/184517.

Council of Science Editors:

McGee, Oliver Gregory I. A three dimensional elasticity based solution for free vibrations of simultaneously skewed and twisted cantilever parallelepipeds. [Doctoral Dissertation]. University of Arizona; 1988. Available from: http://hdl.handle.net/10150/184517

27. Tufts, Matthew W. Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections.

Degree: PhD, Aerospace Engineering, 2015, Texas A&M University

 The interaction between two-dimensional steps and gaps with stationary crossflow vortices on a swept laminar wing has been investigated using computational methods. Using flow conditions… (more)

Subjects/Keywords: Laminar Flow; Transition; Swept-Wing

…SWIFT Swept-Wing In-Flight Testing (Model with No Excrescence) SWIFTER Swept… …SWIFTEST Swept-Wing In-Flight Testing Excrescence Stability Theory (Model with 1% x/c… …Flows with Forward-Facing Steps . . . . . Unswept Open Flows with Swept Backward-Facing Steps… …Unswept Open Flows with Swept Forward-Facing Steps . Swept-Wing Flows with Backward-Facing Steps… …Swept-Wing Flows with Forward-Facing Steps . . . . . . Current Experiments… 

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APA (6th Edition):

Tufts, M. W. (2015). Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156386

Chicago Manual of Style (16th Edition):

Tufts, Matthew W. “Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections.” 2015. Doctoral Dissertation, Texas A&M University. Accessed January 25, 2021. http://hdl.handle.net/1969.1/156386.

MLA Handbook (7th Edition):

Tufts, Matthew W. “Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections.” 2015. Web. 25 Jan 2021.

Vancouver:

Tufts MW. Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections. [Internet] [Doctoral dissertation]. Texas A&M University; 2015. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1969.1/156386.

Council of Science Editors:

Tufts MW. Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections. [Doctoral Dissertation]. Texas A&M University; 2015. Available from: http://hdl.handle.net/1969.1/156386

28. Wiedemann, Arthur David. A Study of the Aeroacoustics of Swept Propellers for Small Unmanned Aerial Vehicles.

Degree: MS, Mechanical & Aerospace Engineering, 2020, Old Dominion University

  In recent years, small unmanned aerial vehicles (UAVs) have increased in availability and use in both public and commercial sectors. This increased use of… (more)

Subjects/Keywords: Acoustics; Aeroacoustics; Aerodynamics; Propeller; Sweep; Swept; Acoustics, Dynamics, and Controls; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Wiedemann, A. D. (2020). A Study of the Aeroacoustics of Swept Propellers for Small Unmanned Aerial Vehicles. (Thesis). Old Dominion University. Retrieved from 9798641821429 ; https://digitalcommons.odu.edu/mae_etds/309

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):

Wiedemann, Arthur David. “A Study of the Aeroacoustics of Swept Propellers for Small Unmanned Aerial Vehicles.” 2020. Thesis, Old Dominion University. Accessed January 25, 2021. 9798641821429 ; https://digitalcommons.odu.edu/mae_etds/309.

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

MLA Handbook (7th Edition):

Wiedemann, Arthur David. “A Study of the Aeroacoustics of Swept Propellers for Small Unmanned Aerial Vehicles.” 2020. Web. 25 Jan 2021.

Vancouver:

Wiedemann AD. A Study of the Aeroacoustics of Swept Propellers for Small Unmanned Aerial Vehicles. [Internet] [Thesis]. Old Dominion University; 2020. [cited 2021 Jan 25]. Available from: 9798641821429 ; https://digitalcommons.odu.edu/mae_etds/309.

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

Council of Science Editors:

Wiedemann AD. A Study of the Aeroacoustics of Swept Propellers for Small Unmanned Aerial Vehicles. [Thesis]. Old Dominion University; 2020. Available from: 9798641821429 ; https://digitalcommons.odu.edu/mae_etds/309

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


Delft University of Technology

29. Serpieri, J. Cross-Flow Instability: Flow diagnostics and control of swept wing boundary layers.

Degree: 2018, Delft University of Technology

 The research presented in this booklet focusses on the cross-flow instability. Applying traditional and advanced flow diagnostics, the boundary layer evolution is studied in detail.… (more)

Subjects/Keywords: Swept wings; Boundary layer transition; Cross-flow instability

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APA (6th Edition):

Serpieri, J. (2018). Cross-Flow Instability: Flow diagnostics and control of swept wing boundary layers. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; urn:NBN:nl:ui:24-uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; 3dac1e78-fcc3-437f-9579-048b74439f55 ; 10.4233/uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; urn:isbn:978-94-6186-879-4 ; urn:NBN:nl:ui:24-uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; http://resolver.tudelft.nl/uuid:3dac1e78-fcc3-437f-9579-048b74439f55

Chicago Manual of Style (16th Edition):

Serpieri, J. “Cross-Flow Instability: Flow diagnostics and control of swept wing boundary layers.” 2018. Doctoral Dissertation, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; urn:NBN:nl:ui:24-uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; 3dac1e78-fcc3-437f-9579-048b74439f55 ; 10.4233/uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; urn:isbn:978-94-6186-879-4 ; urn:NBN:nl:ui:24-uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; http://resolver.tudelft.nl/uuid:3dac1e78-fcc3-437f-9579-048b74439f55.

MLA Handbook (7th Edition):

Serpieri, J. “Cross-Flow Instability: Flow diagnostics and control of swept wing boundary layers.” 2018. Web. 25 Jan 2021.

Vancouver:

Serpieri J. Cross-Flow Instability: Flow diagnostics and control of swept wing boundary layers. [Internet] [Doctoral dissertation]. Delft University of Technology; 2018. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; urn:NBN:nl:ui:24-uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; 3dac1e78-fcc3-437f-9579-048b74439f55 ; 10.4233/uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; urn:isbn:978-94-6186-879-4 ; urn:NBN:nl:ui:24-uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; http://resolver.tudelft.nl/uuid:3dac1e78-fcc3-437f-9579-048b74439f55.

Council of Science Editors:

Serpieri J. Cross-Flow Instability: Flow diagnostics and control of swept wing boundary layers. [Doctoral Dissertation]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; urn:NBN:nl:ui:24-uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; 3dac1e78-fcc3-437f-9579-048b74439f55 ; 10.4233/uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; urn:isbn:978-94-6186-879-4 ; urn:NBN:nl:ui:24-uuid:3dac1e78-fcc3-437f-9579-048b74439f55 ; http://resolver.tudelft.nl/uuid:3dac1e78-fcc3-437f-9579-048b74439f55


University of Manchester

30. Chard, James. Tangential leading edge blowing for flow control on non-slender delta wings.

Degree: PhD, 2018, University of Manchester

 In the military arena there is an increase in demand for Low Observable (LO) flight vehicles. This drive for low observability imposes limits on Leading… (more)

Subjects/Keywords: 629.13; Leading edge separation; Delta wing; UCAV; Tangential blowing; Swept wing; Flow control; Leading edge blowing; Fluidic control

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

APA (6th Edition):

Chard, J. (2018). Tangential leading edge blowing for flow control on non-slender delta wings. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/tangential-leading-edge-blowing-for-flow-control-on-nonslender-delta-wings(0ed0f6fa-23ad-44a2-a187-e8e1e8f1ac8a).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748051

Chicago Manual of Style (16th Edition):

Chard, James. “Tangential leading edge blowing for flow control on non-slender delta wings.” 2018. Doctoral Dissertation, University of Manchester. Accessed January 25, 2021. https://www.research.manchester.ac.uk/portal/en/theses/tangential-leading-edge-blowing-for-flow-control-on-nonslender-delta-wings(0ed0f6fa-23ad-44a2-a187-e8e1e8f1ac8a).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748051.

MLA Handbook (7th Edition):

Chard, James. “Tangential leading edge blowing for flow control on non-slender delta wings.” 2018. Web. 25 Jan 2021.

Vancouver:

Chard J. Tangential leading edge blowing for flow control on non-slender delta wings. [Internet] [Doctoral dissertation]. University of Manchester; 2018. [cited 2021 Jan 25]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/tangential-leading-edge-blowing-for-flow-control-on-nonslender-delta-wings(0ed0f6fa-23ad-44a2-a187-e8e1e8f1ac8a).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748051.

Council of Science Editors:

Chard J. Tangential leading edge blowing for flow control on non-slender delta wings. [Doctoral Dissertation]. University of Manchester; 2018. Available from: https://www.research.manchester.ac.uk/portal/en/theses/tangential-leading-edge-blowing-for-flow-control-on-nonslender-delta-wings(0ed0f6fa-23ad-44a2-a187-e8e1e8f1ac8a).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748051

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