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University: University of Southampton

You searched for subject:(Permanent Magnet Brushless DC Motor). Showing records 1 – 30 of 256 total matches.

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University of Southampton

1. Blandeau, Vincent. Aerodynamic broadband noise from contra-rotating open rotors.

Degree: PhD, 2011, University of Southampton

 In recent years, there has been growing interest in contra-rotating open rotors (CRORs) for use as the power plants on aircraft, since they are estimated… (more)

Subjects/Keywords: 629.13; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Blandeau, V. (2011). Aerodynamic broadband noise from contra-rotating open rotors. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/179853/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.533277

Chicago Manual of Style (16th Edition):

Blandeau, Vincent. “Aerodynamic broadband noise from contra-rotating open rotors.” 2011. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/179853/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.533277.

MLA Handbook (7th Edition):

Blandeau, Vincent. “Aerodynamic broadband noise from contra-rotating open rotors.” 2011. Web. 20 Nov 2019.

Vancouver:

Blandeau V. Aerodynamic broadband noise from contra-rotating open rotors. [Internet] [Doctoral dissertation]. University of Southampton; 2011. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/179853/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.533277.

Council of Science Editors:

Blandeau V. Aerodynamic broadband noise from contra-rotating open rotors. [Doctoral Dissertation]. University of Southampton; 2011. Available from: https://eprints.soton.ac.uk/179853/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.533277


University of Southampton

2. Balakrishnan, Shankar Kumar. A numerical study of some vortex ring phenomena using direct numerical simulation (DNS).

Degree: PhD, 2013, University of Southampton

 Direct numerical simulation (DNS) is used to study some aspects of the dynamics of vortex rings in viscous, incompressible ow at Reynolds numbers (defined as… (more)

Subjects/Keywords: 532.059; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Balakrishnan, S. K. (2013). A numerical study of some vortex ring phenomena using direct numerical simulation (DNS). (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/355700/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581531

Chicago Manual of Style (16th Edition):

Balakrishnan, Shankar Kumar. “A numerical study of some vortex ring phenomena using direct numerical simulation (DNS).” 2013. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/355700/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581531.

MLA Handbook (7th Edition):

Balakrishnan, Shankar Kumar. “A numerical study of some vortex ring phenomena using direct numerical simulation (DNS).” 2013. Web. 20 Nov 2019.

Vancouver:

Balakrishnan SK. A numerical study of some vortex ring phenomena using direct numerical simulation (DNS). [Internet] [Doctoral dissertation]. University of Southampton; 2013. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/355700/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581531.

Council of Science Editors:

Balakrishnan SK. A numerical study of some vortex ring phenomena using direct numerical simulation (DNS). [Doctoral Dissertation]. University of Southampton; 2013. Available from: https://eprints.soton.ac.uk/355700/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581531


University of Southampton

3. Bianchi, Gabriel. Structural performance of spacecraft honeycomb panels.

Degree: PhD, 2011, University of Southampton

 Honeycomb sandwich structures (commonly referred to as honeycomb sandwich panels) have found wide spread application in the aerospace industry thanks to their excellent properties, in… (more)

Subjects/Keywords: 620.112; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Bianchi, G. (2011). Structural performance of spacecraft honeycomb panels. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/333288/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.548222

Chicago Manual of Style (16th Edition):

Bianchi, Gabriel. “Structural performance of spacecraft honeycomb panels.” 2011. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/333288/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.548222.

MLA Handbook (7th Edition):

Bianchi, Gabriel. “Structural performance of spacecraft honeycomb panels.” 2011. Web. 20 Nov 2019.

Vancouver:

Bianchi G. Structural performance of spacecraft honeycomb panels. [Internet] [Doctoral dissertation]. University of Southampton; 2011. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/333288/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.548222.

Council of Science Editors:

Bianchi G. Structural performance of spacecraft honeycomb panels. [Doctoral Dissertation]. University of Southampton; 2011. Available from: https://eprints.soton.ac.uk/333288/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.548222


University of Southampton

4. Wang, Xin. Computational aeroacoustic study of aircraft slat tracks and cut-outs.

Degree: PhD, 2013, University of Southampton

 As one of the major contributors to aircraft noise, the noise generated by high-lift devices has been explored for many years. However, the noise related… (more)

Subjects/Keywords: 629.132; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Wang, X. (2013). Computational aeroacoustic study of aircraft slat tracks and cut-outs. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/372765/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.635452

Chicago Manual of Style (16th Edition):

Wang, Xin. “Computational aeroacoustic study of aircraft slat tracks and cut-outs.” 2013. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/372765/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.635452.

MLA Handbook (7th Edition):

Wang, Xin. “Computational aeroacoustic study of aircraft slat tracks and cut-outs.” 2013. Web. 20 Nov 2019.

Vancouver:

Wang X. Computational aeroacoustic study of aircraft slat tracks and cut-outs. [Internet] [Doctoral dissertation]. University of Southampton; 2013. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/372765/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.635452.

Council of Science Editors:

Wang X. Computational aeroacoustic study of aircraft slat tracks and cut-outs. [Doctoral Dissertation]. University of Southampton; 2013. Available from: https://eprints.soton.ac.uk/372765/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.635452


University of Southampton

5. Schwarz, Benjamin Samuel. Fractionated satellites : a systems engineering analysis.

Degree: PhD, 2014, University of Southampton

 The current method of operating space-based assets involves the design and launch of large, monolithic spacecraft. These spacecraft are not responsive to failures or changes… (more)

Subjects/Keywords: 629.47; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Schwarz, B. S. (2014). Fractionated satellites : a systems engineering analysis. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/370544/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.628830

Chicago Manual of Style (16th Edition):

Schwarz, Benjamin Samuel. “Fractionated satellites : a systems engineering analysis.” 2014. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/370544/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.628830.

MLA Handbook (7th Edition):

Schwarz, Benjamin Samuel. “Fractionated satellites : a systems engineering analysis.” 2014. Web. 20 Nov 2019.

Vancouver:

Schwarz BS. Fractionated satellites : a systems engineering analysis. [Internet] [Doctoral dissertation]. University of Southampton; 2014. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/370544/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.628830.

Council of Science Editors:

Schwarz BS. Fractionated satellites : a systems engineering analysis. [Doctoral Dissertation]. University of Southampton; 2014. Available from: https://eprints.soton.ac.uk/370544/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.628830


University of Southampton

6. Deshpande, Aditya S. The use of geometric uncertainty data in aero engine structural analysis and design.

Degree: PhD, 2013, University of Southampton

 A gas turbine disc has three critical regions for which lifing calculations are essential: the assembly holes or weld areas, the hub region, and the… (more)

Subjects/Keywords: 629.134353; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Deshpande, A. S. (2013). The use of geometric uncertainty data in aero engine structural analysis and design. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/361705/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588918

Chicago Manual of Style (16th Edition):

Deshpande, Aditya S. “The use of geometric uncertainty data in aero engine structural analysis and design.” 2013. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/361705/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588918.

MLA Handbook (7th Edition):

Deshpande, Aditya S. “The use of geometric uncertainty data in aero engine structural analysis and design.” 2013. Web. 20 Nov 2019.

Vancouver:

Deshpande AS. The use of geometric uncertainty data in aero engine structural analysis and design. [Internet] [Doctoral dissertation]. University of Southampton; 2013. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/361705/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588918.

Council of Science Editors:

Deshpande AS. The use of geometric uncertainty data in aero engine structural analysis and design. [Doctoral Dissertation]. University of Southampton; 2013. Available from: https://eprints.soton.ac.uk/361705/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588918


University of Southampton

7. Chen, Peng. Identification and attenuation of slat noise.

Degree: PhD, 2012, University of Southampton

 In the case of civil transport aircraft, engines were the dominant noise source until the advent of the high-bypass ratio engines in the early 1970s.… (more)

Subjects/Keywords: 520.23; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Chen, P. (2012). Identification and attenuation of slat noise. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/348864/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560797

Chicago Manual of Style (16th Edition):

Chen, Peng. “Identification and attenuation of slat noise.” 2012. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/348864/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560797.

MLA Handbook (7th Edition):

Chen, Peng. “Identification and attenuation of slat noise.” 2012. Web. 20 Nov 2019.

Vancouver:

Chen P. Identification and attenuation of slat noise. [Internet] [Doctoral dissertation]. University of Southampton; 2012. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/348864/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560797.

Council of Science Editors:

Chen P. Identification and attenuation of slat noise. [Doctoral Dissertation]. University of Southampton; 2012. Available from: https://eprints.soton.ac.uk/348864/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560797


University of Southampton

8. Luo, Xinfu. Plasma based jet actuators for flow control.

Degree: PhD, 2012, University of Southampton

 A set of plasma based jet actuators were designed for flow control applications. The characteristics of these actuators and their flow control applications were studied… (more)

Subjects/Keywords: 533.62; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Luo, X. (2012). Plasma based jet actuators for flow control. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/348870/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560791

Chicago Manual of Style (16th Edition):

Luo, Xinfu. “Plasma based jet actuators for flow control.” 2012. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/348870/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560791.

MLA Handbook (7th Edition):

Luo, Xinfu. “Plasma based jet actuators for flow control.” 2012. Web. 20 Nov 2019.

Vancouver:

Luo X. Plasma based jet actuators for flow control. [Internet] [Doctoral dissertation]. University of Southampton; 2012. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/348870/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560791.

Council of Science Editors:

Luo X. Plasma based jet actuators for flow control. [Doctoral Dissertation]. University of Southampton; 2012. Available from: https://eprints.soton.ac.uk/348870/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560791


University of Southampton

9. Saunders, Arrun. An empirical model of long-term thermospheric density change.

Degree: PhD, 2012, University of Southampton

 Predicting the positions of satellites in Low Earth Orbit (LEO) requires a comprehensive understanding of the dynamic nature of the atmosphere. For objects in LEO… (more)

Subjects/Keywords: 551.51011; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Saunders, A. (2012). An empirical model of long-term thermospheric density change. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/348934/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560596

Chicago Manual of Style (16th Edition):

Saunders, Arrun. “An empirical model of long-term thermospheric density change.” 2012. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/348934/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560596.

MLA Handbook (7th Edition):

Saunders, Arrun. “An empirical model of long-term thermospheric density change.” 2012. Web. 20 Nov 2019.

Vancouver:

Saunders A. An empirical model of long-term thermospheric density change. [Internet] [Doctoral dissertation]. University of Southampton; 2012. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/348934/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560596.

Council of Science Editors:

Saunders A. An empirical model of long-term thermospheric density change. [Doctoral Dissertation]. University of Southampton; 2012. Available from: https://eprints.soton.ac.uk/348934/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560596


University of Southampton

10. Heyder-Bruckner, Jacques. The aerodynamics of an inverted wing and a rotating wheel in ground effect.

Degree: PhD, 2011, University of Southampton

 This study investigates the aerodynamics of nil inverted wing in ground effect, a race car wheel and the interaction between the two components, using numerical… (more)

Subjects/Keywords: 629.1323; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Heyder-Bruckner, J. (2011). The aerodynamics of an inverted wing and a rotating wheel in ground effect. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/207263/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561508

Chicago Manual of Style (16th Edition):

Heyder-Bruckner, Jacques. “The aerodynamics of an inverted wing and a rotating wheel in ground effect.” 2011. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/207263/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561508.

MLA Handbook (7th Edition):

Heyder-Bruckner, Jacques. “The aerodynamics of an inverted wing and a rotating wheel in ground effect.” 2011. Web. 20 Nov 2019.

Vancouver:

Heyder-Bruckner J. The aerodynamics of an inverted wing and a rotating wheel in ground effect. [Internet] [Doctoral dissertation]. University of Southampton; 2011. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/207263/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561508.

Council of Science Editors:

Heyder-Bruckner J. The aerodynamics of an inverted wing and a rotating wheel in ground effect. [Doctoral Dissertation]. University of Southampton; 2011. Available from: https://eprints.soton.ac.uk/207263/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561508


University of Southampton

11. Kim, Yusik. Wind turbine aerodynamics in freestream turbulence.

Degree: PhD, 2013, University of Southampton

 Topics in wind turbine aerodynamics are reviewed. These include the effect of freestrearn turbulence all the flows over wind turbine blades; dynamic stall phenomenon; and… (more)

Subjects/Keywords: 621.45; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Kim, Y. (2013). Wind turbine aerodynamics in freestream turbulence. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/360372/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588876

Chicago Manual of Style (16th Edition):

Kim, Yusik. “Wind turbine aerodynamics in freestream turbulence.” 2013. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/360372/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588876.

MLA Handbook (7th Edition):

Kim, Yusik. “Wind turbine aerodynamics in freestream turbulence.” 2013. Web. 20 Nov 2019.

Vancouver:

Kim Y. Wind turbine aerodynamics in freestream turbulence. [Internet] [Doctoral dissertation]. University of Southampton; 2013. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/360372/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588876.

Council of Science Editors:

Kim Y. Wind turbine aerodynamics in freestream turbulence. [Doctoral Dissertation]. University of Southampton; 2013. Available from: https://eprints.soton.ac.uk/360372/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588876


University of Southampton

12. De Tullio, Nicola. Receptivity and transition to turbulence of supersonic boundary layers with surface roughness.

Degree: PhD, 2013, University of Southampton

 A deeper understanding of the different factors that influence the laminar-turbulent transition in supersonic boundary layers will help the design of efficient high-speed vehicles. In… (more)

Subjects/Keywords: 533.62; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

De Tullio, N. (2013). Receptivity and transition to turbulence of supersonic boundary layers with surface roughness. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/348815/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.568952

Chicago Manual of Style (16th Edition):

De Tullio, Nicola. “Receptivity and transition to turbulence of supersonic boundary layers with surface roughness.” 2013. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/348815/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.568952.

MLA Handbook (7th Edition):

De Tullio, Nicola. “Receptivity and transition to turbulence of supersonic boundary layers with surface roughness.” 2013. Web. 20 Nov 2019.

Vancouver:

De Tullio N. Receptivity and transition to turbulence of supersonic boundary layers with surface roughness. [Internet] [Doctoral dissertation]. University of Southampton; 2013. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/348815/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.568952.

Council of Science Editors:

De Tullio N. Receptivity and transition to turbulence of supersonic boundary layers with surface roughness. [Doctoral Dissertation]. University of Southampton; 2013. Available from: https://eprints.soton.ac.uk/348815/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.568952


University of Southampton

13. Salimi, Pejwaak. Quadrature error cancellation for micro-machined vibratory gyroscope embedded in high order electromechanical sigma delta modulator.

Degree: PhD, 2013, University of Southampton

 Vibratory micro-machined gyroscopes utilize Coriolis force to detect the rotation rate. Recently it has been proved that embedding the gyroscope in an electromechanical ΣΔ modulator… (more)

Subjects/Keywords: 681.753; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Salimi, P. (2013). Quadrature error cancellation for micro-machined vibratory gyroscope embedded in high order electromechanical sigma delta modulator. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/361723/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588923

Chicago Manual of Style (16th Edition):

Salimi, Pejwaak. “Quadrature error cancellation for micro-machined vibratory gyroscope embedded in high order electromechanical sigma delta modulator.” 2013. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/361723/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588923.

MLA Handbook (7th Edition):

Salimi, Pejwaak. “Quadrature error cancellation for micro-machined vibratory gyroscope embedded in high order electromechanical sigma delta modulator.” 2013. Web. 20 Nov 2019.

Vancouver:

Salimi P. Quadrature error cancellation for micro-machined vibratory gyroscope embedded in high order electromechanical sigma delta modulator. [Internet] [Doctoral dissertation]. University of Southampton; 2013. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/361723/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588923.

Council of Science Editors:

Salimi P. Quadrature error cancellation for micro-machined vibratory gyroscope embedded in high order electromechanical sigma delta modulator. [Doctoral Dissertation]. University of Southampton; 2013. Available from: https://eprints.soton.ac.uk/361723/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588923


University of Southampton

14. Windiate, Sarah. An experimental and numerical study of bluff body.

Degree: PhD, 2014, University of Southampton

 An experimental and numerical investigation was performed in order to firstly establish the aerodynamics and aeroacoustics of a landing gear torque link configuration, and secondly… (more)

Subjects/Keywords: 629.132; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Windiate, S. (2014). An experimental and numerical study of bluff body. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/365194/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.605769

Chicago Manual of Style (16th Edition):

Windiate, Sarah. “An experimental and numerical study of bluff body.” 2014. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/365194/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.605769.

MLA Handbook (7th Edition):

Windiate, Sarah. “An experimental and numerical study of bluff body.” 2014. Web. 20 Nov 2019.

Vancouver:

Windiate S. An experimental and numerical study of bluff body. [Internet] [Doctoral dissertation]. University of Southampton; 2014. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/365194/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.605769.

Council of Science Editors:

Windiate S. An experimental and numerical study of bluff body. [Doctoral Dissertation]. University of Southampton; 2014. Available from: https://eprints.soton.ac.uk/365194/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.605769


University of Southampton

15. Palmer, Matthew James. Experimental evaluation of hydrogen peroxide catalysts for monopropellant attitude control thrusters.

Degree: PhD, 2014, University of Southampton

 Currently the space community relies on propellants such as hydrazine and its derivatives in propulsion systems aboard satellites and spacecraft. However their highly toxic and… (more)

Subjects/Keywords: 629.13; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Palmer, M. J. (2014). Experimental evaluation of hydrogen peroxide catalysts for monopropellant attitude control thrusters. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/385352/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.678123

Chicago Manual of Style (16th Edition):

Palmer, Matthew James. “Experimental evaluation of hydrogen peroxide catalysts for monopropellant attitude control thrusters.” 2014. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/385352/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.678123.

MLA Handbook (7th Edition):

Palmer, Matthew James. “Experimental evaluation of hydrogen peroxide catalysts for monopropellant attitude control thrusters.” 2014. Web. 20 Nov 2019.

Vancouver:

Palmer MJ. Experimental evaluation of hydrogen peroxide catalysts for monopropellant attitude control thrusters. [Internet] [Doctoral dissertation]. University of Southampton; 2014. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/385352/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.678123.

Council of Science Editors:

Palmer MJ. Experimental evaluation of hydrogen peroxide catalysts for monopropellant attitude control thrusters. [Doctoral Dissertation]. University of Southampton; 2014. Available from: https://eprints.soton.ac.uk/385352/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.678123


University of Southampton

16. White, Adam Edward. An adaptive strategy to control the space debris population.

Degree: PhD, 2014, University of Southampton

 As a result of the last 60 years of satellite launches, a significant amount of space debris has been generated in Earth orbit. Growing consensus… (more)

Subjects/Keywords: 629.4; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

White, A. E. (2014). An adaptive strategy to control the space debris population. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/377012/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.655359

Chicago Manual of Style (16th Edition):

White, Adam Edward. “An adaptive strategy to control the space debris population.” 2014. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/377012/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.655359.

MLA Handbook (7th Edition):

White, Adam Edward. “An adaptive strategy to control the space debris population.” 2014. Web. 20 Nov 2019.

Vancouver:

White AE. An adaptive strategy to control the space debris population. [Internet] [Doctoral dissertation]. University of Southampton; 2014. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/377012/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.655359.

Council of Science Editors:

White AE. An adaptive strategy to control the space debris population. [Doctoral Dissertation]. University of Southampton; 2014. Available from: https://eprints.soton.ac.uk/377012/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.655359


University of Southampton

17. Touber, Emile. Unsteadiness in shock-wave/boundary layer interactions.

Degree: PhD, 2010, University of Southampton

 The need for better understanding of the low-frequency unsteadiness observed in shock wave/turbulent boundary layer interactions has been driving research in this area for several… (more)

Subjects/Keywords: 629.13; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Touber, E. (2010). Unsteadiness in shock-wave/boundary layer interactions. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/161073/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.523451

Chicago Manual of Style (16th Edition):

Touber, Emile. “Unsteadiness in shock-wave/boundary layer interactions.” 2010. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/161073/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.523451.

MLA Handbook (7th Edition):

Touber, Emile. “Unsteadiness in shock-wave/boundary layer interactions.” 2010. Web. 20 Nov 2019.

Vancouver:

Touber E. Unsteadiness in shock-wave/boundary layer interactions. [Internet] [Doctoral dissertation]. University of Southampton; 2010. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/161073/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.523451.

Council of Science Editors:

Touber E. Unsteadiness in shock-wave/boundary layer interactions. [Doctoral Dissertation]. University of Southampton; 2010. Available from: https://eprints.soton.ac.uk/161073/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.523451


University of Southampton

18. Wong, J. S. Whole life cost methods for aero-engine design.

Degree: PhD, 2012, University of Southampton

 This research was motivated by the move of aero-engine manufacturers to provide services as well as products. With leasing arrangements such as TotalCare©, the aero-engine… (more)

Subjects/Keywords: 629.13435; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Wong, J. S. (2012). Whole life cost methods for aero-engine design. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/360369/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588801

Chicago Manual of Style (16th Edition):

Wong, J S. “Whole life cost methods for aero-engine design.” 2012. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/360369/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588801.

MLA Handbook (7th Edition):

Wong, J S. “Whole life cost methods for aero-engine design.” 2012. Web. 20 Nov 2019.

Vancouver:

Wong JS. Whole life cost methods for aero-engine design. [Internet] [Doctoral dissertation]. University of Southampton; 2012. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/360369/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588801.

Council of Science Editors:

Wong JS. Whole life cost methods for aero-engine design. [Doctoral Dissertation]. University of Southampton; 2012. Available from: https://eprints.soton.ac.uk/360369/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588801


University of Southampton

19. Grubisic, Angelo Niko. Microthrusters based on the T5 and T6 hollow cathodes.

Degree: PhD, 2011, University of Southampton

 Small spacecraft with limited on-board resources would benefit greatly from the development of a low power, low cost microthruster able to offer propellant savings over… (more)

Subjects/Keywords: 621.31042; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Grubisic, A. N. (2011). Microthrusters based on the T5 and T6 hollow cathodes. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/181509/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561538

Chicago Manual of Style (16th Edition):

Grubisic, Angelo Niko. “Microthrusters based on the T5 and T6 hollow cathodes.” 2011. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/181509/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561538.

MLA Handbook (7th Edition):

Grubisic, Angelo Niko. “Microthrusters based on the T5 and T6 hollow cathodes.” 2011. Web. 20 Nov 2019.

Vancouver:

Grubisic AN. Microthrusters based on the T5 and T6 hollow cathodes. [Internet] [Doctoral dissertation]. University of Southampton; 2011. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/181509/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561538.

Council of Science Editors:

Grubisic AN. Microthrusters based on the T5 and T6 hollow cathodes. [Doctoral Dissertation]. University of Southampton; 2011. Available from: https://eprints.soton.ac.uk/181509/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561538


University of Southampton

20. Rind, Elad. Turbulent wakes in turbulent streams.

Degree: PhD, 2011, University of Southampton

 Direct numerical simulation and wind tunnel experiments have been used to study the effects of free-stream turbulence on axisymmetric wakes. In both cases the wake… (more)

Subjects/Keywords: 629.13; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Rind, E. (2011). Turbulent wakes in turbulent streams. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/193955/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.536338

Chicago Manual of Style (16th Edition):

Rind, Elad. “Turbulent wakes in turbulent streams.” 2011. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/193955/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.536338.

MLA Handbook (7th Edition):

Rind, Elad. “Turbulent wakes in turbulent streams.” 2011. Web. 20 Nov 2019.

Vancouver:

Rind E. Turbulent wakes in turbulent streams. [Internet] [Doctoral dissertation]. University of Southampton; 2011. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/193955/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.536338.

Council of Science Editors:

Rind E. Turbulent wakes in turbulent streams. [Doctoral Dissertation]. University of Southampton; 2011. Available from: https://eprints.soton.ac.uk/193955/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.536338


University of Southampton

21. Jasion, G. Toward a physics based entrainment model for simulation of helicopter brownout.

Degree: PhD, 2013, University of Southampton

 Brownout is the name given to the degraded visual environment that can develop around a helicopter as it operates in dusty conditions. The dust cloud… (more)

Subjects/Keywords: 620; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Jasion, G. (2013). Toward a physics based entrainment model for simulation of helicopter brownout. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/355705/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581534

Chicago Manual of Style (16th Edition):

Jasion, G. “Toward a physics based entrainment model for simulation of helicopter brownout.” 2013. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/355705/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581534.

MLA Handbook (7th Edition):

Jasion, G. “Toward a physics based entrainment model for simulation of helicopter brownout.” 2013. Web. 20 Nov 2019.

Vancouver:

Jasion G. Toward a physics based entrainment model for simulation of helicopter brownout. [Internet] [Doctoral dissertation]. University of Southampton; 2013. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/355705/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581534.

Council of Science Editors:

Jasion G. Toward a physics based entrainment model for simulation of helicopter brownout. [Doctoral Dissertation]. University of Southampton; 2013. Available from: https://eprints.soton.ac.uk/355705/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581534


University of Southampton

22. Lau, Alex Siu Hong. High-order computations on aerofoil-gust interaction noise and the effects of wavy leading edges.

Degree: PhD, 2012, University of Southampton

 High-order accurate numerical simulations are performed to investigate the effects of wavy leading edges on aerofoil gust interaction (AGI) noise. The present study is based… (more)

Subjects/Keywords: 629.13432; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Lau, A. S. H. (2012). High-order computations on aerofoil-gust interaction noise and the effects of wavy leading edges. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/355961/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581486

Chicago Manual of Style (16th Edition):

Lau, Alex Siu Hong. “High-order computations on aerofoil-gust interaction noise and the effects of wavy leading edges.” 2012. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/355961/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581486.

MLA Handbook (7th Edition):

Lau, Alex Siu Hong. “High-order computations on aerofoil-gust interaction noise and the effects of wavy leading edges.” 2012. Web. 20 Nov 2019.

Vancouver:

Lau ASH. High-order computations on aerofoil-gust interaction noise and the effects of wavy leading edges. [Internet] [Doctoral dissertation]. University of Southampton; 2012. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/355961/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581486.

Council of Science Editors:

Lau ASH. High-order computations on aerofoil-gust interaction noise and the effects of wavy leading edges. [Doctoral Dissertation]. University of Southampton; 2012. Available from: https://eprints.soton.ac.uk/355961/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581486


University of Southampton

23. Everitt, Stewart. Developments in advanced high temperature disc and blade materials for aero-engine gas turbine applications.

Degree: PhD, 2012, University of Southampton

 The research carried out as part of this EngD is aimed at understanding the high temperature materials used in modern gas turbine applications and providing… (more)

Subjects/Keywords: 621.4330153205; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Everitt, S. (2012). Developments in advanced high temperature disc and blade materials for aero-engine gas turbine applications. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/348897/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560587

Chicago Manual of Style (16th Edition):

Everitt, Stewart. “Developments in advanced high temperature disc and blade materials for aero-engine gas turbine applications.” 2012. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/348897/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560587.

MLA Handbook (7th Edition):

Everitt, Stewart. “Developments in advanced high temperature disc and blade materials for aero-engine gas turbine applications.” 2012. Web. 20 Nov 2019.

Vancouver:

Everitt S. Developments in advanced high temperature disc and blade materials for aero-engine gas turbine applications. [Internet] [Doctoral dissertation]. University of Southampton; 2012. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/348897/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560587.

Council of Science Editors:

Everitt S. Developments in advanced high temperature disc and blade materials for aero-engine gas turbine applications. [Doctoral Dissertation]. University of Southampton; 2012. Available from: https://eprints.soton.ac.uk/348897/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560587


University of Southampton

24. Kuya, Yuichi. Aerodynamics and multi-fidelity surrogate modelling of an inverted wing with vortex generators in ground effect.

Degree: PhD, 2009, University of Southampton

 A study of an inverted single-element wing with vortex denerators in ground effect is presented. Counter-rotating and co-rotating rectangular-vane type vortex generators with different device… (more)

Subjects/Keywords: 629.2; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Kuya, Y. (2009). Aerodynamics and multi-fidelity surrogate modelling of an inverted wing with vortex generators in ground effect. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/73331/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.523199

Chicago Manual of Style (16th Edition):

Kuya, Yuichi. “Aerodynamics and multi-fidelity surrogate modelling of an inverted wing with vortex generators in ground effect.” 2009. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/73331/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.523199.

MLA Handbook (7th Edition):

Kuya, Yuichi. “Aerodynamics and multi-fidelity surrogate modelling of an inverted wing with vortex generators in ground effect.” 2009. Web. 20 Nov 2019.

Vancouver:

Kuya Y. Aerodynamics and multi-fidelity surrogate modelling of an inverted wing with vortex generators in ground effect. [Internet] [Doctoral dissertation]. University of Southampton; 2009. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/73331/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.523199.

Council of Science Editors:

Kuya Y. Aerodynamics and multi-fidelity surrogate modelling of an inverted wing with vortex generators in ground effect. [Doctoral Dissertation]. University of Southampton; 2009. Available from: https://eprints.soton.ac.uk/73331/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.523199


University of Southampton

25. Schumann, Benjamin. Aeronautical life-cycle mission modelling framework for conceptual design.

Degree: PhD, 2014, University of Southampton

 This thesis introduces a novel framework for life cycle mission modelling during conceptual aeronautical design. The framework supports object-oriented mission definition using Geographical Information System… (more)

Subjects/Keywords: 629.13; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Schumann, B. (2014). Aeronautical life-cycle mission modelling framework for conceptual design. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/366537/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.628710

Chicago Manual of Style (16th Edition):

Schumann, Benjamin. “Aeronautical life-cycle mission modelling framework for conceptual design.” 2014. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/366537/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.628710.

MLA Handbook (7th Edition):

Schumann, Benjamin. “Aeronautical life-cycle mission modelling framework for conceptual design.” 2014. Web. 20 Nov 2019.

Vancouver:

Schumann B. Aeronautical life-cycle mission modelling framework for conceptual design. [Internet] [Doctoral dissertation]. University of Southampton; 2014. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/366537/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.628710.

Council of Science Editors:

Schumann B. Aeronautical life-cycle mission modelling framework for conceptual design. [Doctoral Dissertation]. University of Southampton; 2014. Available from: https://eprints.soton.ac.uk/366537/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.628710


University of Southampton

26. Collingwood, Cheryl. Investigation of a miniature differential ion thruster.

Degree: PhD, 2011, University of Southampton

 Complex space missions involving formation flying or drag compensation are driving the need for spacecraft propulsion systems capable of providing low but also highly accurate… (more)

Subjects/Keywords: 629.13; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Collingwood, C. (2011). Investigation of a miniature differential ion thruster. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/334166/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.543429

Chicago Manual of Style (16th Edition):

Collingwood, Cheryl. “Investigation of a miniature differential ion thruster.” 2011. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/334166/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.543429.

MLA Handbook (7th Edition):

Collingwood, Cheryl. “Investigation of a miniature differential ion thruster.” 2011. Web. 20 Nov 2019.

Vancouver:

Collingwood C. Investigation of a miniature differential ion thruster. [Internet] [Doctoral dissertation]. University of Southampton; 2011. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/334166/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.543429.

Council of Science Editors:

Collingwood C. Investigation of a miniature differential ion thruster. [Doctoral Dissertation]. University of Southampton; 2011. Available from: https://eprints.soton.ac.uk/334166/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.543429


University of Southampton

27. Chappell, S. Active control with dielectric barrier discharge actuators applied to high-lift devices.

Degree: PhD, 2013, University of Southampton

 An experimental investigation examined the capability of dielectric barrier discharge (DBD) actuators to control a high-lift device system. Aerodynamic tests investigated the potential of utilising… (more)

Subjects/Keywords: 621.313; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Chappell, S. (2013). Active control with dielectric barrier discharge actuators applied to high-lift devices. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/359742/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588851

Chicago Manual of Style (16th Edition):

Chappell, S. “Active control with dielectric barrier discharge actuators applied to high-lift devices.” 2013. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/359742/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588851.

MLA Handbook (7th Edition):

Chappell, S. “Active control with dielectric barrier discharge actuators applied to high-lift devices.” 2013. Web. 20 Nov 2019.

Vancouver:

Chappell S. Active control with dielectric barrier discharge actuators applied to high-lift devices. [Internet] [Doctoral dissertation]. University of Southampton; 2013. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/359742/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588851.

Council of Science Editors:

Chappell S. Active control with dielectric barrier discharge actuators applied to high-lift devices. [Doctoral Dissertation]. University of Southampton; 2013. Available from: https://eprints.soton.ac.uk/359742/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588851


University of Southampton

28. Powell, Stephen. Applications and enhancements of aircraft design optimization techniques.

Degree: PhD, 2012, University of Southampton

 The aircraft industry has been at the forefront in developing design optimization strategies ever since the advent of high performance computing. Thanks to the large… (more)

Subjects/Keywords: 621.1341; TL Motor vehicles. Aeronautics. Astronautics

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APA (6th Edition):

Powell, S. (2012). Applications and enhancements of aircraft design optimization techniques. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/348869/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560787

Chicago Manual of Style (16th Edition):

Powell, Stephen. “Applications and enhancements of aircraft design optimization techniques.” 2012. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/348869/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560787.

MLA Handbook (7th Edition):

Powell, Stephen. “Applications and enhancements of aircraft design optimization techniques.” 2012. Web. 20 Nov 2019.

Vancouver:

Powell S. Applications and enhancements of aircraft design optimization techniques. [Internet] [Doctoral dissertation]. University of Southampton; 2012. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/348869/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560787.

Council of Science Editors:

Powell S. Applications and enhancements of aircraft design optimization techniques. [Doctoral Dissertation]. University of Southampton; 2012. Available from: https://eprints.soton.ac.uk/348869/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560787


University of Southampton

29. Weinmann, Markus. Simulation strategies for complex turbulent flows.

Degree: PhD, 2011, University of Southampton

 Computational fluid dynamics in conjunction with the Reynolds-Averaged Navier-Stokes approach is nowadays routinely employed in a large variety of engineering and industrial applications despite some… (more)

Subjects/Keywords: 502.85; TL Motor vehicles. Aeronautics. Astronautics

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

APA (6th Edition):

Weinmann, M. (2011). Simulation strategies for complex turbulent flows. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/334174/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.543419

Chicago Manual of Style (16th Edition):

Weinmann, Markus. “Simulation strategies for complex turbulent flows.” 2011. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/334174/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.543419.

MLA Handbook (7th Edition):

Weinmann, Markus. “Simulation strategies for complex turbulent flows.” 2011. Web. 20 Nov 2019.

Vancouver:

Weinmann M. Simulation strategies for complex turbulent flows. [Internet] [Doctoral dissertation]. University of Southampton; 2011. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/334174/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.543419.

Council of Science Editors:

Weinmann M. Simulation strategies for complex turbulent flows. [Doctoral Dissertation]. University of Southampton; 2011. Available from: https://eprints.soton.ac.uk/334174/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.543419


University of Southampton

30. Spiteri, Matthew. Aerodynamic control of bluff body noise.

Degree: PhD, 2011, University of Southampton

 The main aim of this study was to investigate noise reduction techniques for bluff body noise. Three methods were investigated, using a splitter plate on… (more)

Subjects/Keywords: 629.1323; TL Motor vehicles. Aeronautics. Astronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Spiteri, M. (2011). Aerodynamic control of bluff body noise. (Doctoral Dissertation). University of Southampton. Retrieved from https://eprints.soton.ac.uk/181529/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560546

Chicago Manual of Style (16th Edition):

Spiteri, Matthew. “Aerodynamic control of bluff body noise.” 2011. Doctoral Dissertation, University of Southampton. Accessed November 20, 2019. https://eprints.soton.ac.uk/181529/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560546.

MLA Handbook (7th Edition):

Spiteri, Matthew. “Aerodynamic control of bluff body noise.” 2011. Web. 20 Nov 2019.

Vancouver:

Spiteri M. Aerodynamic control of bluff body noise. [Internet] [Doctoral dissertation]. University of Southampton; 2011. [cited 2019 Nov 20]. Available from: https://eprints.soton.ac.uk/181529/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560546.

Council of Science Editors:

Spiteri M. Aerodynamic control of bluff body noise. [Doctoral Dissertation]. University of Southampton; 2011. Available from: https://eprints.soton.ac.uk/181529/ ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.560546

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