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You searched for subject:( Swept gull wing configuration). Showing records 1 – 30 of 2312 total matches.

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University of Pretoria

1. [No author]. Longitudinal handling characteristics of a tailless gull-wing aircraft .

Degree: 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

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

APA (6th Edition):

author], [. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft . (Masters Thesis). University of Pretoria. Retrieved from http://upetd.up.ac.za/thesis/available/etd-09182008-132941/

Chicago Manual of Style (16th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Masters Thesis, University of Pretoria. Accessed January 24, 2021. http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

MLA Handbook (7th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Web. 24 Jan 2021.

Vancouver:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 24]. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

Council of Science Editors:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Masters Thesis]. University of Pretoria; 2008. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/


University of Pretoria

2. Agenbag, Daniel Sarel. Longitudinal handling characteristics of a tailless gull-wing aircraft.

Degree: Mechanical and Aeronautical Engineering, 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

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APA (6th Edition):

Agenbag, D. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft. (Masters Thesis). University of Pretoria. Retrieved from http://hdl.handle.net/2263/28011

Chicago Manual of Style (16th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Masters Thesis, University of Pretoria. Accessed January 24, 2021. http://hdl.handle.net/2263/28011.

MLA Handbook (7th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Web. 24 Jan 2021.

Vancouver:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2263/28011.

Council of Science Editors:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Masters Thesis]. University of Pretoria; 2008. Available from: http://hdl.handle.net/2263/28011


Delft University of Technology

3. 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 24, 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. 24 Jan 2021.

Vancouver:

Sol MB(. Conceptual Design of Swept Wing Root Aerofoils. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 24]. 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

4. 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 24, 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. 24 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 24]. 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 Arizona

5. 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 24, 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. 24 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 24]. 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

6. 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 24, 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. 24 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 24]. 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


Lehigh University

7. 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 24, 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. 24 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 24]. 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


Cranfield University

8. Huang, Haidong. Optimal design of a flying-wing aircraft inner wing structure configuration.

Degree: MSc by Research, 2012, Cranfield University

 Flying-wing aircraft are considered to have great advantages and potentials in aerodynamic performance and weight saving. However, they also have many challenges in design. One… (more)

Subjects/Keywords: Flying-wing aircraft; inner wing configuration; Wave-Section Configuration; optimal; FE analysis

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APA (6th Edition):

Huang, H. (2012). Optimal design of a flying-wing aircraft inner wing structure configuration. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7439

Chicago Manual of Style (16th Edition):

Huang, Haidong. “Optimal design of a flying-wing aircraft inner wing structure configuration.” 2012. Masters Thesis, Cranfield University. Accessed January 24, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/7439.

MLA Handbook (7th Edition):

Huang, Haidong. “Optimal design of a flying-wing aircraft inner wing structure configuration.” 2012. Web. 24 Jan 2021.

Vancouver:

Huang H. Optimal design of a flying-wing aircraft inner wing structure configuration. [Internet] [Masters thesis]. Cranfield University; 2012. [cited 2021 Jan 24]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7439.

Council of Science Editors:

Huang H. Optimal design of a flying-wing aircraft inner wing structure configuration. [Masters Thesis]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7439

9. Barbosa, Átila Antunes França. Influência da asa em gaivota nos coeficientes aerodinâmicos de uma aeronave.

Degree: Mestrado, Aeronaves, 2015, University of São Paulo

Desde o início da década de 2010, o aumento do preço do combustível de aviação e a pressão da sociedade para redução da emissão de… (more)

Subjects/Keywords: Asas com diedro variável; Asas em gaivota; Ensaio em túnel de vento; Gull wing; Multi dihedral wing; Wind tunnel testing

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APA (6th Edition):

Barbosa, . A. F. (2015). Influência da asa em gaivota nos coeficientes aerodinâmicos de uma aeronave. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-15112015-170422/ ;

Chicago Manual of Style (16th Edition):

Barbosa, Átila Antunes França. “Influência da asa em gaivota nos coeficientes aerodinâmicos de uma aeronave.” 2015. Masters Thesis, University of São Paulo. Accessed January 24, 2021. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-15112015-170422/ ;.

MLA Handbook (7th Edition):

Barbosa, Átila Antunes França. “Influência da asa em gaivota nos coeficientes aerodinâmicos de uma aeronave.” 2015. Web. 24 Jan 2021.

Vancouver:

Barbosa AF. Influência da asa em gaivota nos coeficientes aerodinâmicos de uma aeronave. [Internet] [Masters thesis]. University of São Paulo; 2015. [cited 2021 Jan 24]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-15112015-170422/ ;.

Council of Science Editors:

Barbosa AF. Influência da asa em gaivota nos coeficientes aerodinâmicos de uma aeronave. [Masters Thesis]. University of São Paulo; 2015. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-15112015-170422/ ;

10. 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 24, 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. 24 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 24]. 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


University of Washington

11. 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 24, 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. 24 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 24]. 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

12. 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 24, 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. 24 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 24]. 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

13. 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… …Unswept Open Flows with Swept Forward-Facing Steps . Swept-Wing Flows with Backward-Facing Steps… …Swept-Wing Flows with Forward-Facing Steps . . . . . . Current Experiments… …TRAVELING MODES . . . . . . . 120 xi LIST OF FIGURES FIGURE Page I.1 Swept-Wing Velocity… 

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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 24, 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. 24 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 24]. 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


University of Manchester

14. 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 (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 24, 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. 24 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 24]. 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


Virginia Tech

15. Orr, Matthew William. Aerodynamic Properties of the Inboard Wing Concept.

Degree: MS, Aerospace Engineering, 2003, Virginia Tech

 This investigation examines a new concept in airliner configurations from an experimental aerodynamics point of view. The concept proposes mounting the fuselages at the tips… (more)

Subjects/Keywords: configuration testing; aerodynamics; inboard wing

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APA (6th Edition):

Orr, M. W. (2003). Aerodynamic Properties of the Inboard Wing Concept. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/9708

Chicago Manual of Style (16th Edition):

Orr, Matthew William. “Aerodynamic Properties of the Inboard Wing Concept.” 2003. Masters Thesis, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/9708.

MLA Handbook (7th Edition):

Orr, Matthew William. “Aerodynamic Properties of the Inboard Wing Concept.” 2003. Web. 24 Jan 2021.

Vancouver:

Orr MW. Aerodynamic Properties of the Inboard Wing Concept. [Internet] [Masters thesis]. Virginia Tech; 2003. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/9708.

Council of Science Editors:

Orr MW. Aerodynamic Properties of the Inboard Wing Concept. [Masters Thesis]. Virginia Tech; 2003. Available from: http://hdl.handle.net/10919/9708


Delft University of Technology

16. Boersma, J.Y. (author). Business Jet Design Using Laminar Flow.

Degree: 2016, Delft University of Technology

For conceptual aircraft design to include accurate laminar flow prediction, a link between modern computational tools to determine laminar-to-turbulent boundary layer transition and fast sizing… (more)

Subjects/Keywords: drag; N-factor; boundary layer; skin friction; laminar; flow; transition; Reynolds; crossflow; aircraft; design; business; swept; wing; initiator; model

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APA (6th Edition):

Boersma, J. Y. (. (2016). Business Jet Design Using Laminar Flow. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4d1818ec-5842-47b0-b144-173aa77a3803

Chicago Manual of Style (16th Edition):

Boersma, J Y (author). “Business Jet Design Using Laminar Flow.” 2016. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:4d1818ec-5842-47b0-b144-173aa77a3803.

MLA Handbook (7th Edition):

Boersma, J Y (author). “Business Jet Design Using Laminar Flow.” 2016. Web. 24 Jan 2021.

Vancouver:

Boersma JY(. Business Jet Design Using Laminar Flow. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:4d1818ec-5842-47b0-b144-173aa77a3803.

Council of Science Editors:

Boersma JY(. Business Jet Design Using Laminar Flow. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:4d1818ec-5842-47b0-b144-173aa77a3803


Texas A&M University

17. Belisle, Michael Joseph. Aerodynamic Design for Swept-wing Laminar Flow.

Degree: PhD, Aerospace Engineering, 2013, Texas A&M University

 This work describes and compares processes for swept-wing laminar flow control (SWLFC) aerody-namic design. It focuses on results obtained during the preliminary outer-mold-line (OML) design… (more)

Subjects/Keywords: aircraft; aerodynamic design; boundary-layer stability; boundary-layer transition; crossflow instability; discrete roughness elements; drag reduction; flight test; laminar flow control; natural laminar flow; swept-wing laminar flow control; wing design; wing glove

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APA (6th Edition):

Belisle, M. J. (2013). Aerodynamic Design for Swept-wing Laminar Flow. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151655

Chicago Manual of Style (16th Edition):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Doctoral Dissertation, Texas A&M University. Accessed January 24, 2021. http://hdl.handle.net/1969.1/151655.

MLA Handbook (7th Edition):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Web. 24 Jan 2021.

Vancouver:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1969.1/151655.

Council of Science Editors:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151655


Brno University of Technology

18. Musil, Tomáš. Netradiční koncepce letadel: Non-Traditional Aircraft Conception.

Degree: 2018, Brno University of Technology

 This bachelor thesis is about concepts of aircraft that are non-traditional in structural design or unconventional in different aspects. The individual chapters describe selected concepts… (more)

Subjects/Keywords: Koncepce letadla; nekonvenční letoun; VTOL; negativní geometrie křídla; samokřídlo; tailsitter; konvertoplán; vektorování tahu; šikmé křídlo; vztlakové těleso; Aircraft conception; unconventional aircraft; VTOL; forward-swept wing; flying wing; tailsitter; convertiplane; thrust vectoring; oblique wing; lifting body

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APA (6th Edition):

Musil, T. (2018). Netradiční koncepce letadel: Non-Traditional Aircraft Conception. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/81578

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):

Musil, Tomáš. “Netradiční koncepce letadel: Non-Traditional Aircraft Conception.” 2018. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/81578.

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

MLA Handbook (7th Edition):

Musil, Tomáš. “Netradiční koncepce letadel: Non-Traditional Aircraft Conception.” 2018. Web. 24 Jan 2021.

Vancouver:

Musil T. Netradiční koncepce letadel: Non-Traditional Aircraft Conception. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/81578.

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

Council of Science Editors:

Musil T. Netradiční koncepce letadel: Non-Traditional Aircraft Conception. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/81578

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


University of Florida

19. Lacroix, Bradley W. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 This document details the research performed on applying piezoelectric macro fiber composite actuators on micro air vehicles. The research objective was to apply the minimum… (more)

Subjects/Keywords: Aircraft; Aircraft pitch; Aircraft roll; Aircraft wings; Carbon fibers; Design optimization; Geometry; Steels; Swept wings; Wind tunnels; composite  – fiber  – flying  – macro  – materials  – mav  – mfc  – morphing  – optimization  – piezoelectric  – smart  – uav  – wing

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APA (6th Edition):

Lacroix, B. W. (2013). On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0046212

Chicago Manual of Style (16th Edition):

Lacroix, Bradley W. “On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.” 2013. Doctoral Dissertation, University of Florida. Accessed January 24, 2021. https://ufdc.ufl.edu/UFE0046212.

MLA Handbook (7th Edition):

Lacroix, Bradley W. “On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.” 2013. Web. 24 Jan 2021.

Vancouver:

Lacroix BW. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2021 Jan 24]. Available from: https://ufdc.ufl.edu/UFE0046212.

Council of Science Editors:

Lacroix BW. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. [Doctoral Dissertation]. University of Florida; 2013. Available from: https://ufdc.ufl.edu/UFE0046212

20. Weissenfluh, Shawn Edward. Quantifying Seasonal Variation in Physiological Condition of Adult Franklin's Gull (Luecophaeus Pipixcan) during Nesting.

Degree: 2011, North Dakota State University

 Understanding seasonal variation in adult physiological condition is important for developing hypotheses on how nest initiation, adult condition, chick development and recruitment are related in… (more)

Subjects/Keywords: Franklin's gull  – Physiology.; Franklin's gull  – Reproduction.; Franklin's gull  – Nests.

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APA (6th Edition):

Weissenfluh, S. E. (2011). Quantifying Seasonal Variation in Physiological Condition of Adult Franklin's Gull (Luecophaeus Pipixcan) during Nesting. (Thesis). North Dakota State University. Retrieved from http://hdl.handle.net/10365/28844

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):

Weissenfluh, Shawn Edward. “Quantifying Seasonal Variation in Physiological Condition of Adult Franklin's Gull (Luecophaeus Pipixcan) during Nesting.” 2011. Thesis, North Dakota State University. Accessed January 24, 2021. http://hdl.handle.net/10365/28844.

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

MLA Handbook (7th Edition):

Weissenfluh, Shawn Edward. “Quantifying Seasonal Variation in Physiological Condition of Adult Franklin's Gull (Luecophaeus Pipixcan) during Nesting.” 2011. Web. 24 Jan 2021.

Vancouver:

Weissenfluh SE. Quantifying Seasonal Variation in Physiological Condition of Adult Franklin's Gull (Luecophaeus Pipixcan) during Nesting. [Internet] [Thesis]. North Dakota State University; 2011. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10365/28844.

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

Council of Science Editors:

Weissenfluh SE. Quantifying Seasonal Variation in Physiological Condition of Adult Franklin's Gull (Luecophaeus Pipixcan) during Nesting. [Thesis]. North Dakota State University; 2011. Available from: http://hdl.handle.net/10365/28844

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


Indian Institute of Science

21. Nathan, Vinay. Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail.

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

 This thesis deals with computing the pressure distribution around a swimming slender fish and the thrust generated by its flapping motion. The body of the… (more)

Subjects/Keywords: Swimming Slender Fish Flow Dynamics; Slender Body Flow Model; Swept Wing Model; Planar Wing Flow; Unsteady Flows; Vortex Dynamics; Swimming Propulsion; Unsteady Propulsion; Fishlike Swimmimg Hydrodynamics; Fish Near-Body Flow Dynamics; Marine Propulsion; Fluid Dynamics; Vortex Panel Method; Bernoulli Equation; Aerospace Engineering

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APA (6th Edition):

Nathan, V. (2018). Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3551

Chicago Manual of Style (16th Edition):

Nathan, Vinay. “Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail.” 2018. Masters Thesis, Indian Institute of Science. Accessed January 24, 2021. http://etd.iisc.ac.in/handle/2005/3551.

MLA Handbook (7th Edition):

Nathan, Vinay. “Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail.” 2018. Web. 24 Jan 2021.

Vancouver:

Nathan V. Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail. [Internet] [Masters thesis]. Indian Institute of Science; 2018. [cited 2021 Jan 24]. Available from: http://etd.iisc.ac.in/handle/2005/3551.

Council of Science Editors:

Nathan V. Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail. [Masters Thesis]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3551

22. Adegbindin, Moustaine Kolawole Agnide. Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft.

Degree: MS, Aerospace Engineering, 2017, Virginia Tech

 Many futuristic aircraft such as the Hybrid Wing Body have numerous control surfaces that can result in large hinge moments, high actuation power demands, and… (more)

Subjects/Keywords: Optimization; Artificial Intelligence; Neural Network; Genetic Algorithm; Forward Swept Wing; Hybrid Wing Body; Hinge Moment

…Forward Swept Wing GA : Genetic Algorithm HM : Hinge Moments xiv HWB : Hybrid Wing… …Forward Swept Wing (FSW) aircraft. 4 2 Aircraft Configurations Studied 2.1 Hybrid… …Wing Body (HWB) A Hybrid Wing Body aircraft is a configuration where the wing and… …Swept Wing (FSW) A Forward Swept Wing (FSW) aircraft was selected as a… …Laboratory have developed a Hybrid Wing Body aircraft concept: the X48 (see Fig. 1.1)… 

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APA (6th Edition):

Adegbindin, M. K. A. (2017). Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/74950

Chicago Manual of Style (16th Edition):

Adegbindin, Moustaine Kolawole Agnide. “Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft.” 2017. Masters Thesis, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/74950.

MLA Handbook (7th Edition):

Adegbindin, Moustaine Kolawole Agnide. “Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft.” 2017. Web. 24 Jan 2021.

Vancouver:

Adegbindin MKA. Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/74950.

Council of Science Editors:

Adegbindin MKA. Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/74950

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

Degree: 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: Leading edge blowing; Swept wing; Flow control; Fluidic control; Tangential blowing; Leading edge separation; Delta wing; UCAV

…x28;61)....... 91 Figure 53: TLEB configuration on the Buccaneer Mark 1 swept wing (… …Figure 12: Leading edge separation bubble on a moderately swept wing (flow in direction of… …50 Figure 13: Upper surface attached pressure distribution on a swept wing. Taken from… …swept wing. Taken from (30)… …52 Figure 16: Leading edge vortex flow on a moderately swept wing (flow in direction… 

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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 http://www.manchester.ac.uk/escholar/uk-ac-man-scw:314613

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 24, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:314613.

MLA Handbook (7th Edition):

Chard, James. “Tangential leading edge blowing for flow control on non-slender delta wings.” 2018. Web. 24 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 24]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:314613.

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: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:314613


Michigan State University

24. Smith, William John. Movements of Michigan herring gulls.

Degree: MS, 1958, Michigan State University

Subjects/Keywords: Herring gull

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APA (6th Edition):

Smith, W. J. (1958). Movements of Michigan herring gulls. (Masters Thesis). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:13101

Chicago Manual of Style (16th Edition):

Smith, William John. “Movements of Michigan herring gulls.” 1958. Masters Thesis, Michigan State University. Accessed January 24, 2021. http://etd.lib.msu.edu/islandora/object/etd:13101.

MLA Handbook (7th Edition):

Smith, William John. “Movements of Michigan herring gulls.” 1958. Web. 24 Jan 2021.

Vancouver:

Smith WJ. Movements of Michigan herring gulls. [Internet] [Masters thesis]. Michigan State University; 1958. [cited 2021 Jan 24]. Available from: http://etd.lib.msu.edu/islandora/object/etd:13101.

Council of Science Editors:

Smith WJ. Movements of Michigan herring gulls. [Masters Thesis]. Michigan State University; 1958. Available from: http://etd.lib.msu.edu/islandora/object/etd:13101

25. Woodruff, Matthew Jeffery. Receptivity Studies on a Swept-Wing Model.

Degree: MS, Aerospace Engineering, 2012, Texas A&M University

 A series of flight tests was performed using a swept-wing model mounted on a Cessna O-2 aircraft. The crossflow waves on the airfoil were excited… (more)

Subjects/Keywords: laminar flow control; laminar to turbulent transition; swept wing flow control

…the last major hurdle in swept-wing laminar flow control (SWLFC) (Saric… …work relevant to the current experiment. The Swept-Wing In Flight Testing (SWIFT)… …The Swept-Wing In Flight Testing (SWIFT) model is an airfoil that has been… …with the flight crew during flight operations. TEST AIRFOIL The Swept Wing In Flight Testing… …x28;SWIFT) model used for these series of tests is a 30° swept wing with a laminar flow… 

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APA (6th Edition):

Woodruff, M. J. (2012). Receptivity Studies on a Swept-Wing Model. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9119

Chicago Manual of Style (16th Edition):

Woodruff, Matthew Jeffery. “Receptivity Studies on a Swept-Wing Model.” 2012. Masters Thesis, Texas A&M University. Accessed January 24, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9119.

MLA Handbook (7th Edition):

Woodruff, Matthew Jeffery. “Receptivity Studies on a Swept-Wing Model.” 2012. Web. 24 Jan 2021.

Vancouver:

Woodruff MJ. Receptivity Studies on a Swept-Wing Model. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9119.

Council of Science Editors:

Woodruff MJ. Receptivity Studies on a Swept-Wing Model. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9119


Delft University of Technology

26. Groot, K.J. BiGlobal Stability of Shear Flows: Spanwise & Streamwise Analyses.

Degree: 2018, Delft University of Technology

 Laminar-turbulent transition dictates an increase in skin friction. The resulting turbulent skin friction contributes to approximately 40% of the total drag of commercial aircraft. Reducing… (more)

Subjects/Keywords: Flow instability; measured base flows; Micro-ramp; Swept-wing boundary layer; Crossflow instability; Streamwise BiGlobal problem

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APA (6th Edition):

Groot, K. J. (2018). BiGlobal Stability of Shear Flows: Spanwise & Streamwise Analyses. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; urn:NBN:nl:ui:24-uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; 60ef07b2-00db-418b-9495-5a9baf6105df ; 10.4233/uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; urn:isbn:978-94-6366-115-7 ; urn:NBN:nl:ui:24-uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df

Chicago Manual of Style (16th Edition):

Groot, K J. “BiGlobal Stability of Shear Flows: Spanwise & Streamwise Analyses.” 2018. Doctoral Dissertation, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; urn:NBN:nl:ui:24-uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; 60ef07b2-00db-418b-9495-5a9baf6105df ; 10.4233/uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; urn:isbn:978-94-6366-115-7 ; urn:NBN:nl:ui:24-uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df.

MLA Handbook (7th Edition):

Groot, K J. “BiGlobal Stability of Shear Flows: Spanwise & Streamwise Analyses.” 2018. Web. 24 Jan 2021.

Vancouver:

Groot KJ. BiGlobal Stability of Shear Flows: Spanwise & Streamwise Analyses. [Internet] [Doctoral dissertation]. Delft University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; urn:NBN:nl:ui:24-uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; 60ef07b2-00db-418b-9495-5a9baf6105df ; 10.4233/uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; urn:isbn:978-94-6366-115-7 ; urn:NBN:nl:ui:24-uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df.

Council of Science Editors:

Groot KJ. BiGlobal Stability of Shear Flows: Spanwise & Streamwise Analyses. [Doctoral Dissertation]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; urn:NBN:nl:ui:24-uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; 60ef07b2-00db-418b-9495-5a9baf6105df ; 10.4233/uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; urn:isbn:978-94-6366-115-7 ; urn:NBN:nl:ui:24-uuid:60ef07b2-00db-418b-9495-5a9baf6105df ; http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df

27. Carpenter, Andrew L. In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements.

Degree: PhD, Aerospace Engineering, 2010, Texas A&M University

 One of the last remaining challenges preventing the laminarization of sweptwings is the control of unstable crossflow vortices. In low-disturbance environments the transition from laminar… (more)

Subjects/Keywords: Receptivity; Laminar Flow; Boundary Layer; Swept-Wing; Roughness; Hotfilms; Infrared Thermography; Flight Test

…element us Velocity tangential to swept-wing streamline ut Velocity normal to swept-wing… …velocity at swept-wing leading edge Vne Never-exceed speed Vno Top speed in turbulent… …conditions ws Velocity normal to swept-wing streamline wt Spanwise velocity parallel to swept… …wing leading edge zs Spanwise distance along the swept leading edge αt Streamwise… …wavenumber, tangential to swept-wing streamline αto First calculated streamwise growth rate βt… 

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

APA (6th Edition):

Carpenter, A. L. (2010). In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728

Chicago Manual of Style (16th Edition):

Carpenter, Andrew L. “In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements.” 2010. Doctoral Dissertation, Texas A&M University. Accessed January 24, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728.

MLA Handbook (7th Edition):

Carpenter, Andrew L. “In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements.” 2010. Web. 24 Jan 2021.

Vancouver:

Carpenter AL. In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements. [Internet] [Doctoral dissertation]. Texas A&M University; 2010. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728.

Council of Science Editors:

Carpenter AL. In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements. [Doctoral Dissertation]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-728

28. Hussain, Ali. The Effect of Spanwise Location of an Active Boundary Layer Fence on Swept Wing Performance.

Degree: MS, Aero/Astro Engineering, 2019, The Ohio State University

 Active flow control (AFC) in the form of a wall normal slot was investigated on a NACA 643-618 laminar wing model. The wing model has… (more)

Subjects/Keywords: Aerospace Engineering; aerodynamics; active flow control; boundary layer fence; swept wing; experimental; wind tunnel

…control. 1.2 Background Swept wing flow control presents additional challenges when considering… …dimensional wing will stall relatively uniformly along the spanwise direction. In contrast, a swept… …Queijo et al [14] tested numerous wing fence designs on a swept wing (Λ = 35… …investigation into the differences in lift and stability enhancement on a swept wing. To characterize… …which is crucial to studying swept wing aerodynamics [22]. The geometric chord of… 

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

APA (6th Edition):

Hussain, A. (2019). The Effect of Spanwise Location of an Active Boundary Layer Fence on Swept Wing Performance. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1555516043121521

Chicago Manual of Style (16th Edition):

Hussain, Ali. “The Effect of Spanwise Location of an Active Boundary Layer Fence on Swept Wing Performance.” 2019. Masters Thesis, The Ohio State University. Accessed January 24, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=osu1555516043121521.

MLA Handbook (7th Edition):

Hussain, Ali. “The Effect of Spanwise Location of an Active Boundary Layer Fence on Swept Wing Performance.” 2019. Web. 24 Jan 2021.

Vancouver:

Hussain A. The Effect of Spanwise Location of an Active Boundary Layer Fence on Swept Wing Performance. [Internet] [Masters thesis]. The Ohio State University; 2019. [cited 2021 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1555516043121521.

Council of Science Editors:

Hussain A. The Effect of Spanwise Location of an Active Boundary Layer Fence on Swept Wing Performance. [Masters Thesis]. The Ohio State University; 2019. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1555516043121521


RMIT University

29. Guo, D. Modelling and experimental investigations of a bi-modal unmanned underwater/air system.

Degree: 2019, RMIT University

 The ability to perform underwater and coastal area monitoring missions without surfacing would increase submarine's safety and its combat ability. An innovative bi-modal unmanned/underwater air… (more)

Subjects/Keywords: Fields of Research; BUUAS; Transition propulsion system; Hybrid propulsion system; Variable sweep wing configuration; Wind tunnel test; Numerical simulation; Composite materials; Stability analysis

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

APA (6th Edition):

Guo, D. (2019). Modelling and experimental investigations of a bi-modal unmanned underwater/air system. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:162852

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):

Guo, D. “Modelling and experimental investigations of a bi-modal unmanned underwater/air system.” 2019. Thesis, RMIT University. Accessed January 24, 2021. http://researchbank.rmit.edu.au/view/rmit:162852.

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

MLA Handbook (7th Edition):

Guo, D. “Modelling and experimental investigations of a bi-modal unmanned underwater/air system.” 2019. Web. 24 Jan 2021.

Vancouver:

Guo D. Modelling and experimental investigations of a bi-modal unmanned underwater/air system. [Internet] [Thesis]. RMIT University; 2019. [cited 2021 Jan 24]. Available from: http://researchbank.rmit.edu.au/view/rmit:162852.

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

Council of Science Editors:

Guo D. Modelling and experimental investigations of a bi-modal unmanned underwater/air system. [Thesis]. RMIT University; 2019. Available from: http://researchbank.rmit.edu.au/view/rmit:162852

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


Luleå University of Technology

30. Khan, Fahad Aman. Preliminary aerodynamic investigation of box-wing configurations using low fidelity codes.

Degree: 2010, Luleå University of Technology

This work outlines the different aerodynamic aspects of box-wing design i.e. an unconventional aircraft design configuration exhibiting the capability of reducing induced drag. Being… (more)

Subjects/Keywords: Technology; Non planar configuration; induced drag reduction; box-wing; aircraft performance; Teknik

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

APA (6th Edition):

Khan, F. A. (2010). Preliminary aerodynamic investigation of box-wing configurations using low fidelity codes. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-55530

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):

Khan, Fahad Aman. “Preliminary aerodynamic investigation of box-wing configurations using low fidelity codes.” 2010. Thesis, Luleå University of Technology. Accessed January 24, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-55530.

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

MLA Handbook (7th Edition):

Khan, Fahad Aman. “Preliminary aerodynamic investigation of box-wing configurations using low fidelity codes.” 2010. Web. 24 Jan 2021.

Vancouver:

Khan FA. Preliminary aerodynamic investigation of box-wing configurations using low fidelity codes. [Internet] [Thesis]. Luleå University of Technology; 2010. [cited 2021 Jan 24]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-55530.

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

Council of Science Editors:

Khan FA. Preliminary aerodynamic investigation of box-wing configurations using low fidelity codes. [Thesis]. Luleå University of Technology; 2010. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-55530

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

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