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You searched for +publisher:"Delft University of Technology" +contributor:("Veldhuis, L.L.M."). Showing records 1 – 28 of 28 total matches.

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Delft University of Technology

1. Van Egmond, J.J. Passive Flow Separation Control for High Lift: An Experimental Investigation on a Novel Vortex Generator:.

Degree: 2015, Delft University of Technology

 A current focus in the quest for improvement in fuel efficiency in aircraft design is the simplification of complex high lift systems. A simpler high… (more)

Subjects/Keywords: vortex generators; high lift system; passive flow control

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APA (6th Edition):

Van Egmond, J. J. (2015). Passive Flow Separation Control for High Lift: An Experimental Investigation on a Novel Vortex Generator:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b2328172-746b-4a0b-9937-f2e70f97c224

Chicago Manual of Style (16th Edition):

Van Egmond, J J. “Passive Flow Separation Control for High Lift: An Experimental Investigation on a Novel Vortex Generator:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:b2328172-746b-4a0b-9937-f2e70f97c224.

MLA Handbook (7th Edition):

Van Egmond, J J. “Passive Flow Separation Control for High Lift: An Experimental Investigation on a Novel Vortex Generator:.” 2015. Web. 15 Nov 2019.

Vancouver:

Van Egmond JJ. Passive Flow Separation Control for High Lift: An Experimental Investigation on a Novel Vortex Generator:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:b2328172-746b-4a0b-9937-f2e70f97c224.

Council of Science Editors:

Van Egmond JJ. Passive Flow Separation Control for High Lift: An Experimental Investigation on a Novel Vortex Generator:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:b2328172-746b-4a0b-9937-f2e70f97c224


Delft University of Technology

2. Sinnige, T. The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:.

Degree: 2013, Delft University of Technology

 Growing concerns about the environmental impact of aircraft operations and increasing fuel prices have led to the demand for more fuel-efficient aircraft. One of the… (more)

Subjects/Keywords: propeller; propeller noise; pylon blowing; aeroacoustics

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APA (6th Edition):

Sinnige, T. (2013). The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992

Chicago Manual of Style (16th Edition):

Sinnige, T. “The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:.” 2013. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992.

MLA Handbook (7th Edition):

Sinnige, T. “The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:.” 2013. Web. 15 Nov 2019.

Vancouver:

Sinnige T. The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992.

Council of Science Editors:

Sinnige T. The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:. [Masters Thesis]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992


Delft University of Technology

3. Sitter, M. Internal flow of fluidic oscillators: A numerical and experimental investigation:.

Degree: 2015, Delft University of Technology

 Fluidic oscillators are devices that generate a temporally oscillating jet when supplied with a fluid under pressure. In recent investigations fluidic oscillators have proven to… (more)

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APA (6th Edition):

Sitter, M. (2015). Internal flow of fluidic oscillators: A numerical and experimental investigation:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:88b7b720-7402-4e1a-85e6-7dc785a23b16

Chicago Manual of Style (16th Edition):

Sitter, M. “Internal flow of fluidic oscillators: A numerical and experimental investigation:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:88b7b720-7402-4e1a-85e6-7dc785a23b16.

MLA Handbook (7th Edition):

Sitter, M. “Internal flow of fluidic oscillators: A numerical and experimental investigation:.” 2015. Web. 15 Nov 2019.

Vancouver:

Sitter M. Internal flow of fluidic oscillators: A numerical and experimental investigation:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:88b7b720-7402-4e1a-85e6-7dc785a23b16.

Council of Science Editors:

Sitter M. Internal flow of fluidic oscillators: A numerical and experimental investigation:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:88b7b720-7402-4e1a-85e6-7dc785a23b16


Delft University of Technology

4. Bouquet, T. Modelling the Propeller Slipstream Effect on the Longitudinal Stability and Control:.

Degree: 2016, Delft University of Technology

 As the aviation industry continues to strive for improvements in fuel efficiency throughout the entire aircraft design, interest has been renewed in propeller engines. New… (more)

Subjects/Keywords: aircraft design; initiator; propeller slipstream; longitudinal stability and control

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APA (6th Edition):

Bouquet, T. (2016). Modelling the Propeller Slipstream Effect on the Longitudinal Stability and Control:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:7faf08f7-d16f-4836-b4ff-61ea060bd166

Chicago Manual of Style (16th Edition):

Bouquet, T. “Modelling the Propeller Slipstream Effect on the Longitudinal Stability and Control:.” 2016. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:7faf08f7-d16f-4836-b4ff-61ea060bd166.

MLA Handbook (7th Edition):

Bouquet, T. “Modelling the Propeller Slipstream Effect on the Longitudinal Stability and Control:.” 2016. Web. 15 Nov 2019.

Vancouver:

Bouquet T. Modelling the Propeller Slipstream Effect on the Longitudinal Stability and Control:. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:7faf08f7-d16f-4836-b4ff-61ea060bd166.

Council of Science Editors:

Bouquet T. Modelling the Propeller Slipstream Effect on the Longitudinal Stability and Control:. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:7faf08f7-d16f-4836-b4ff-61ea060bd166


Delft University of Technology

5. Channa, V.V. Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:.

Degree: 2015, Delft University of Technology

 Open rotors are considered to have the potential to improve the fuel economy of aircraft significantly by improving the propulsive efficiency compared to the current… (more)

Subjects/Keywords: propeller; performance; acoustics

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APA (6th Edition):

Channa, V. V. (2015). Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e32f84f1-21da-4a5a-a541-2f15b041ede5

Chicago Manual of Style (16th Edition):

Channa, V V. “Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:e32f84f1-21da-4a5a-a541-2f15b041ede5.

MLA Handbook (7th Edition):

Channa, V V. “Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:.” 2015. Web. 15 Nov 2019.

Vancouver:

Channa VV. Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:e32f84f1-21da-4a5a-a541-2f15b041ede5.

Council of Science Editors:

Channa VV. Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:e32f84f1-21da-4a5a-a541-2f15b041ede5

6. Janssen, R.F. The influence of laminar-turbulent transition on the perfomance of a propeller:.

Degree: 2015, Delft University of Technology

 The influence of laminar-turbulent transition on a propeller blade’s performance has been investigated in this study, both numerically and experimentally. The computational fluid dynamics (CFD)… (more)

Subjects/Keywords: propeller; transition; performance; CFD; computational; fluid; dynamics; infrared; numerical; experimental; RANS; BEMT

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APA (6th Edition):

Janssen, R. F. (2015). The influence of laminar-turbulent transition on the perfomance of a propeller:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ee2db063-a1c0-4f0c-b8a6-79f6f3acb749

Chicago Manual of Style (16th Edition):

Janssen, R F. “The influence of laminar-turbulent transition on the perfomance of a propeller:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:ee2db063-a1c0-4f0c-b8a6-79f6f3acb749.

MLA Handbook (7th Edition):

Janssen, R F. “The influence of laminar-turbulent transition on the perfomance of a propeller:.” 2015. Web. 15 Nov 2019.

Vancouver:

Janssen RF. The influence of laminar-turbulent transition on the perfomance of a propeller:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:ee2db063-a1c0-4f0c-b8a6-79f6f3acb749.

Council of Science Editors:

Janssen RF. The influence of laminar-turbulent transition on the perfomance of a propeller:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:ee2db063-a1c0-4f0c-b8a6-79f6f3acb749


Delft University of Technology

7. Windels, E.R.G. Formation Flight: analysis of wake sensitivity, drag and control in trimmed flight:.

Degree: 2015, Delft University of Technology

 A research simulation model was created to perform extended research into formation flight dynamic behaviour. The principle of aircraft flying in formation is to lower… (more)

Subjects/Keywords: formation flight; formation flight trim; induced drag saving; formation flight stability; wake vortex field; A330-300; fuel saving; formation flight control

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APA (6th Edition):

Windels, E. R. G. (2015). Formation Flight: analysis of wake sensitivity, drag and control in trimmed flight:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a65726f9-a873-442e-a186-b27202d9519a

Chicago Manual of Style (16th Edition):

Windels, E R G. “Formation Flight: analysis of wake sensitivity, drag and control in trimmed flight:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:a65726f9-a873-442e-a186-b27202d9519a.

MLA Handbook (7th Edition):

Windels, E R G. “Formation Flight: analysis of wake sensitivity, drag and control in trimmed flight:.” 2015. Web. 15 Nov 2019.

Vancouver:

Windels ERG. Formation Flight: analysis of wake sensitivity, drag and control in trimmed flight:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:a65726f9-a873-442e-a186-b27202d9519a.

Council of Science Editors:

Windels ERG. Formation Flight: analysis of wake sensitivity, drag and control in trimmed flight:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:a65726f9-a873-442e-a186-b27202d9519a


Delft University of Technology

8. Stokkermans, T.C.A. Design and Analysis of Swirl Recovery Vanes for an Isolated and a Wing Mounted Tractor Propeller:.

Degree: 2015, Delft University of Technology

 In light of the energy crisis of the early 1970's, NASA and industry gained a renewed interest in high-speed propellers for improved propulsive efficiency and… (more)

Subjects/Keywords: Swirl Recovery Vanes; SRV; propeller; APIAN; wing; Fokker 50; CFD; propulsive efficiency; slipstream

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APA (6th Edition):

Stokkermans, T. C. A. (2015). Design and Analysis of Swirl Recovery Vanes for an Isolated and a Wing Mounted Tractor Propeller:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4ef56c0f-1dbd-4edb-8b89-f672dd3597ec

Chicago Manual of Style (16th Edition):

Stokkermans, T C A. “Design and Analysis of Swirl Recovery Vanes for an Isolated and a Wing Mounted Tractor Propeller:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:4ef56c0f-1dbd-4edb-8b89-f672dd3597ec.

MLA Handbook (7th Edition):

Stokkermans, T C A. “Design and Analysis of Swirl Recovery Vanes for an Isolated and a Wing Mounted Tractor Propeller:.” 2015. Web. 15 Nov 2019.

Vancouver:

Stokkermans TCA. Design and Analysis of Swirl Recovery Vanes for an Isolated and a Wing Mounted Tractor Propeller:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:4ef56c0f-1dbd-4edb-8b89-f672dd3597ec.

Council of Science Editors:

Stokkermans TCA. Design and Analysis of Swirl Recovery Vanes for an Isolated and a Wing Mounted Tractor Propeller:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:4ef56c0f-1dbd-4edb-8b89-f672dd3597ec


Delft University of Technology

9. Van Arnhem, N. Design and Analysis of an Installed Pusher Propeller with Boundary Layer Inflow:.

Degree: 2015, Delft University of Technology

 Boundary Layer Ingestion is an integrated propulsion concept in which a propulsor operates in boundary layer flow instead of the free streamflow with the goal… (more)

Subjects/Keywords: Boundary Layer Ingestion; BLI; pusher propeller; CFD; interference effects; design optimisation; integrated propulsion

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APA (6th Edition):

Van Arnhem, N. (2015). Design and Analysis of an Installed Pusher Propeller with Boundary Layer Inflow:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:267beaa5-8b62-4e58-b1ad-ff94355c68f9

Chicago Manual of Style (16th Edition):

Van Arnhem, N. “Design and Analysis of an Installed Pusher Propeller with Boundary Layer Inflow:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:267beaa5-8b62-4e58-b1ad-ff94355c68f9.

MLA Handbook (7th Edition):

Van Arnhem, N. “Design and Analysis of an Installed Pusher Propeller with Boundary Layer Inflow:.” 2015. Web. 15 Nov 2019.

Vancouver:

Van Arnhem N. Design and Analysis of an Installed Pusher Propeller with Boundary Layer Inflow:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:267beaa5-8b62-4e58-b1ad-ff94355c68f9.

Council of Science Editors:

Van Arnhem N. Design and Analysis of an Installed Pusher Propeller with Boundary Layer Inflow:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:267beaa5-8b62-4e58-b1ad-ff94355c68f9

10. Florjancic, D. Improved Design of a High Lift System for General Aviation Aircraft:.

Degree: 2015, Delft University of Technology

 Relatively high wing loading leads to increase in fuel efficiency in commercial as well as in small general aviation aircraft, but requires sophisticated high lift… (more)

Subjects/Keywords: high lift system; flap; payload; general aviation aircraft

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APA (6th Edition):

Florjancic, D. (2015). Improved Design of a High Lift System for General Aviation Aircraft:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a0bcdbba-3ccc-4622-ab8d-6ac2e4a1e598

Chicago Manual of Style (16th Edition):

Florjancic, D. “Improved Design of a High Lift System for General Aviation Aircraft:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:a0bcdbba-3ccc-4622-ab8d-6ac2e4a1e598.

MLA Handbook (7th Edition):

Florjancic, D. “Improved Design of a High Lift System for General Aviation Aircraft:.” 2015. Web. 15 Nov 2019.

Vancouver:

Florjancic D. Improved Design of a High Lift System for General Aviation Aircraft:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:a0bcdbba-3ccc-4622-ab8d-6ac2e4a1e598.

Council of Science Editors:

Florjancic D. Improved Design of a High Lift System for General Aviation Aircraft:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:a0bcdbba-3ccc-4622-ab8d-6ac2e4a1e598


Delft University of Technology

11. Candade, A.A. Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:.

Degree: 2015, Delft University of Technology

 Advanced propeller propulsion systems potentially provide a significant reduction in fuel burn compared to traditional turbofans. An alternative to the conventional aft-fuselage mounted pusher layout… (more)

Subjects/Keywords: propeller; propulsion integration; vortex interactions; aeroacoustics

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APA (6th Edition):

Candade, A. A. (2015). Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135

Chicago Manual of Style (16th Edition):

Candade, A A. “Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135.

MLA Handbook (7th Edition):

Candade, A A. “Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:.” 2015. Web. 15 Nov 2019.

Vancouver:

Candade AA. Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135.

Council of Science Editors:

Candade AA. Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135


Delft University of Technology

12. Fokker, A.D. Investigating the drag sensitivity parameters and lateral dynamic response of a road vehicle in cross-wind flow:.

Degree: 2015, Delft University of Technology

 Recent trends in the automobile industry focus towards enhancing the operating efficiency of the road vehicle. One can achieve this by a combination of increasing… (more)

Subjects/Keywords: vehicle aerodynamics drag reduction vehicle dynamics

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APA (6th Edition):

Fokker, A. D. (2015). Investigating the drag sensitivity parameters and lateral dynamic response of a road vehicle in cross-wind flow:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:bb871e9d-2596-49a4-9bf2-cbed4c6a9446

Chicago Manual of Style (16th Edition):

Fokker, A D. “Investigating the drag sensitivity parameters and lateral dynamic response of a road vehicle in cross-wind flow:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:bb871e9d-2596-49a4-9bf2-cbed4c6a9446.

MLA Handbook (7th Edition):

Fokker, A D. “Investigating the drag sensitivity parameters and lateral dynamic response of a road vehicle in cross-wind flow:.” 2015. Web. 15 Nov 2019.

Vancouver:

Fokker AD. Investigating the drag sensitivity parameters and lateral dynamic response of a road vehicle in cross-wind flow:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:bb871e9d-2596-49a4-9bf2-cbed4c6a9446.

Council of Science Editors:

Fokker AD. Investigating the drag sensitivity parameters and lateral dynamic response of a road vehicle in cross-wind flow:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:bb871e9d-2596-49a4-9bf2-cbed4c6a9446


Delft University of Technology

13. Moerland, E. Development of an aeroelastic analysis tool for structural sizing of high-lift devices during preliminary design:.

Degree: 2011, Delft University of Technology

 The design of complex aircraft elements such as high-lift devices has large influence on the performance of modern transport airplanes. At the cost of increased… (more)

Subjects/Keywords: aeroelastic analysis; high-lift devices; parametric modeling; rapid load estimation; vortex-lattice method; structural sizing; preliminary design

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APA (6th Edition):

Moerland, E. (2011). Development of an aeroelastic analysis tool for structural sizing of high-lift devices during preliminary design:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:feca38a2-e2f4-4249-9b73-5bcc4171ca9d

Chicago Manual of Style (16th Edition):

Moerland, E. “Development of an aeroelastic analysis tool for structural sizing of high-lift devices during preliminary design:.” 2011. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:feca38a2-e2f4-4249-9b73-5bcc4171ca9d.

MLA Handbook (7th Edition):

Moerland, E. “Development of an aeroelastic analysis tool for structural sizing of high-lift devices during preliminary design:.” 2011. Web. 15 Nov 2019.

Vancouver:

Moerland E. Development of an aeroelastic analysis tool for structural sizing of high-lift devices during preliminary design:. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:feca38a2-e2f4-4249-9b73-5bcc4171ca9d.

Council of Science Editors:

Moerland E. Development of an aeroelastic analysis tool for structural sizing of high-lift devices during preliminary design:. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:feca38a2-e2f4-4249-9b73-5bcc4171ca9d


Delft University of Technology

14. Koning, J.H. Development of a KBE application to support aerodynamic design and analysis: Towards a next-generation multi-model generator:.

Degree: 2010, Delft University of Technology

 The aviation industry faces a number of challenges: it needs to produce safer, quieter and more efficient aircraft to meet the demands of the airlines… (more)

Subjects/Keywords: KBE; Multi-model generator; MMG; VSaero; Aerodynamics; Knowledge-Based Engineering

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APA (6th Edition):

Koning, J. H. (2010). Development of a KBE application to support aerodynamic design and analysis: Towards a next-generation multi-model generator:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e7d206a5-2e1f-4287-a8b6-27258316bf79

Chicago Manual of Style (16th Edition):

Koning, J H. “Development of a KBE application to support aerodynamic design and analysis: Towards a next-generation multi-model generator:.” 2010. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:e7d206a5-2e1f-4287-a8b6-27258316bf79.

MLA Handbook (7th Edition):

Koning, J H. “Development of a KBE application to support aerodynamic design and analysis: Towards a next-generation multi-model generator:.” 2010. Web. 15 Nov 2019.

Vancouver:

Koning JH. Development of a KBE application to support aerodynamic design and analysis: Towards a next-generation multi-model generator:. [Internet] [Masters thesis]. Delft University of Technology; 2010. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:e7d206a5-2e1f-4287-a8b6-27258316bf79.

Council of Science Editors:

Koning JH. Development of a KBE application to support aerodynamic design and analysis: Towards a next-generation multi-model generator:. [Masters Thesis]. Delft University of Technology; 2010. Available from: http://resolver.tudelft.nl/uuid:e7d206a5-2e1f-4287-a8b6-27258316bf79

15. Michelis, T. On the Interaction of NS-DBD Plasma Actuation with Flat Plate Boundary Layers:.

Degree: 2013, Delft University of Technology

 Flow control is a never ending strive to achieve the desired flow conditions for an application. As requirements become more demanding, new techniques of flow… (more)

Subjects/Keywords: ns-dbd; plasma actuator

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APA (6th Edition):

Michelis, T. (2013). On the Interaction of NS-DBD Plasma Actuation with Flat Plate Boundary Layers:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a7d697ed-05d4-450c-8b0c-d283329e2b31

Chicago Manual of Style (16th Edition):

Michelis, T. “On the Interaction of NS-DBD Plasma Actuation with Flat Plate Boundary Layers:.” 2013. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:a7d697ed-05d4-450c-8b0c-d283329e2b31.

MLA Handbook (7th Edition):

Michelis, T. “On the Interaction of NS-DBD Plasma Actuation with Flat Plate Boundary Layers:.” 2013. Web. 15 Nov 2019.

Vancouver:

Michelis T. On the Interaction of NS-DBD Plasma Actuation with Flat Plate Boundary Layers:. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:a7d697ed-05d4-450c-8b0c-d283329e2b31.

Council of Science Editors:

Michelis T. On the Interaction of NS-DBD Plasma Actuation with Flat Plate Boundary Layers:. [Masters Thesis]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:a7d697ed-05d4-450c-8b0c-d283329e2b31

16. Van Kuijk, J.J.A. Analysis of Swirl Recovery Vanes: Propulsion system performance and slipstream-wing interaction:.

Degree: 2015, Delft University of Technology

Subjects/Keywords: swirl recovery vanes; propulsion

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APA (6th Edition):

Van Kuijk, J. J. A. (2015). Analysis of Swirl Recovery Vanes: Propulsion system performance and slipstream-wing interaction:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:33cc26ac-2e9b-4bd5-a5dc-55756db1f863

Chicago Manual of Style (16th Edition):

Van Kuijk, J J A. “Analysis of Swirl Recovery Vanes: Propulsion system performance and slipstream-wing interaction:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:33cc26ac-2e9b-4bd5-a5dc-55756db1f863.

MLA Handbook (7th Edition):

Van Kuijk, J J A. “Analysis of Swirl Recovery Vanes: Propulsion system performance and slipstream-wing interaction:.” 2015. Web. 15 Nov 2019.

Vancouver:

Van Kuijk JJA. Analysis of Swirl Recovery Vanes: Propulsion system performance and slipstream-wing interaction:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:33cc26ac-2e9b-4bd5-a5dc-55756db1f863.

Council of Science Editors:

Van Kuijk JJA. Analysis of Swirl Recovery Vanes: Propulsion system performance and slipstream-wing interaction:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:33cc26ac-2e9b-4bd5-a5dc-55756db1f863

17. Crepain, T.P. Flap Side-Edge Noise Reduction:.

Degree: 2015, Delft University of Technology

Subjects/Keywords: Aeroacoustics; CFD; Beamforming; Flap noise

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APA (6th Edition):

Crepain, T. P. (2015). Flap Side-Edge Noise Reduction:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:11de9007-cb02-4540-bb42-3b537d86ef7e

Chicago Manual of Style (16th Edition):

Crepain, T P. “Flap Side-Edge Noise Reduction:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:11de9007-cb02-4540-bb42-3b537d86ef7e.

MLA Handbook (7th Edition):

Crepain, T P. “Flap Side-Edge Noise Reduction:.” 2015. Web. 15 Nov 2019.

Vancouver:

Crepain TP. Flap Side-Edge Noise Reduction:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:11de9007-cb02-4540-bb42-3b537d86ef7e.

Council of Science Editors:

Crepain TP. Flap Side-Edge Noise Reduction:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:11de9007-cb02-4540-bb42-3b537d86ef7e

18. Hoogreef, M.F.M. The Oval Fuselage: A New Structural Design Concept for Blended Wing Body Cabins:.

Degree: 2012, Delft University of Technology

 Faced with the decreasing fossil fuel reserves and the need to decrease its environmental footprint, the aviation industry is searching for alternative fuels and more… (more)

Subjects/Keywords: Blended Wing Body; Aircraft Weight Estimation; Conceptual Design; Fuselage Concept; Aircraft Cabin

…Faculty of Aerospace Engineering of the Delft University of Technology. It is the result of a 10… 

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APA (6th Edition):

Hoogreef, M. F. M. (2012). The Oval Fuselage: A New Structural Design Concept for Blended Wing Body Cabins:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:726c4d37-e9c3-48f7-a2c2-55511e52f1c9

Chicago Manual of Style (16th Edition):

Hoogreef, M F M. “The Oval Fuselage: A New Structural Design Concept for Blended Wing Body Cabins:.” 2012. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:726c4d37-e9c3-48f7-a2c2-55511e52f1c9.

MLA Handbook (7th Edition):

Hoogreef, M F M. “The Oval Fuselage: A New Structural Design Concept for Blended Wing Body Cabins:.” 2012. Web. 15 Nov 2019.

Vancouver:

Hoogreef MFM. The Oval Fuselage: A New Structural Design Concept for Blended Wing Body Cabins:. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:726c4d37-e9c3-48f7-a2c2-55511e52f1c9.

Council of Science Editors:

Hoogreef MFM. The Oval Fuselage: A New Structural Design Concept for Blended Wing Body Cabins:. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:726c4d37-e9c3-48f7-a2c2-55511e52f1c9


Delft University of Technology

19. Tian, F.N. An Integrated Knowledge Based Engineering Mechatronics Modeling Approach to Support the Design of Unstable and Unmanned Aircraft.

Degree: 2015, Delft University of Technology

 The commercial transport aircraft industry is currently developing new “more electric aircraft” (MEA) designs in which various conventional mechanical, hydraulic and pneumatic power systems are… (more)

Subjects/Keywords: multiphysics simulation model; electronic control system; knowledge based engineering; unmanned aerial vehicle; multidisciplinary design optimization

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APA (6th Edition):

Tian, F. N. (2015). An Integrated Knowledge Based Engineering Mechatronics Modeling Approach to Support the Design of Unstable and Unmanned Aircraft. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; urn:NBN:nl:ui:24-uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; urn:NBN:nl:ui:24-uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; http://resolver.tudelft.nl/uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726

Chicago Manual of Style (16th Edition):

Tian, F N. “An Integrated Knowledge Based Engineering Mechatronics Modeling Approach to Support the Design of Unstable and Unmanned Aircraft.” 2015. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; urn:NBN:nl:ui:24-uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; urn:NBN:nl:ui:24-uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; http://resolver.tudelft.nl/uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726.

MLA Handbook (7th Edition):

Tian, F N. “An Integrated Knowledge Based Engineering Mechatronics Modeling Approach to Support the Design of Unstable and Unmanned Aircraft.” 2015. Web. 15 Nov 2019.

Vancouver:

Tian FN. An Integrated Knowledge Based Engineering Mechatronics Modeling Approach to Support the Design of Unstable and Unmanned Aircraft. [Internet] [Doctoral dissertation]. Delft University of Technology; 2015. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; urn:NBN:nl:ui:24-uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; urn:NBN:nl:ui:24-uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; http://resolver.tudelft.nl/uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726.

Council of Science Editors:

Tian FN. An Integrated Knowledge Based Engineering Mechatronics Modeling Approach to Support the Design of Unstable and Unmanned Aircraft. [Doctoral Dissertation]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; urn:NBN:nl:ui:24-uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; urn:NBN:nl:ui:24-uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726 ; http://resolver.tudelft.nl/uuid:0a18a5e5-7109-4fab-97fb-b2a99d9f3726


Delft University of Technology

20. Yang, Y. Aerodynamic Interaction between Propeller and Vortex.

Degree: 2017, Delft University of Technology

Subjects/Keywords: Propeller; Vortex; ground vortex; Blade vortex interaction

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APA (6th Edition):

Yang, Y. (2017). Aerodynamic Interaction between Propeller and Vortex. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; urn:NBN:nl:ui:24-uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; 9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; 10.4233/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; urn:isbn:9789462335806 ; urn:NBN:nl:ui:24-uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; http://resolver.tudelft.nl/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6

Chicago Manual of Style (16th Edition):

Yang, Y. “Aerodynamic Interaction between Propeller and Vortex.” 2017. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; urn:NBN:nl:ui:24-uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; 9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; 10.4233/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; urn:isbn:9789462335806 ; urn:NBN:nl:ui:24-uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; http://resolver.tudelft.nl/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6.

MLA Handbook (7th Edition):

Yang, Y. “Aerodynamic Interaction between Propeller and Vortex.” 2017. Web. 15 Nov 2019.

Vancouver:

Yang Y. Aerodynamic Interaction between Propeller and Vortex. [Internet] [Doctoral dissertation]. Delft University of Technology; 2017. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; urn:NBN:nl:ui:24-uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; 9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; 10.4233/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; urn:isbn:9789462335806 ; urn:NBN:nl:ui:24-uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; http://resolver.tudelft.nl/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6.

Council of Science Editors:

Yang Y. Aerodynamic Interaction between Propeller and Vortex. [Doctoral Dissertation]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; urn:NBN:nl:ui:24-uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; 9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; 10.4233/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; urn:isbn:9789462335806 ; urn:NBN:nl:ui:24-uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6 ; http://resolver.tudelft.nl/uuid:9efb571c-0441-4690-84ca-7c5d5e8bfea6


Delft University of Technology

21. Kotsonis, M. Dielectric Barrier Discharge Actuators for Flow Control: Diagnostics, Modeling, Application.

Degree: 2012, Delft University of Technology

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APA (6th Edition):

Kotsonis, M. (2012). Dielectric Barrier Discharge Actuators for Flow Control: Diagnostics, Modeling, Application. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; urn:NBN:nl:ui:24-uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; urn:NBN:nl:ui:24-uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; http://resolver.tudelft.nl/uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025

Chicago Manual of Style (16th Edition):

Kotsonis, M. “Dielectric Barrier Discharge Actuators for Flow Control: Diagnostics, Modeling, Application.” 2012. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; urn:NBN:nl:ui:24-uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; urn:NBN:nl:ui:24-uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; http://resolver.tudelft.nl/uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025.

MLA Handbook (7th Edition):

Kotsonis, M. “Dielectric Barrier Discharge Actuators for Flow Control: Diagnostics, Modeling, Application.” 2012. Web. 15 Nov 2019.

Vancouver:

Kotsonis M. Dielectric Barrier Discharge Actuators for Flow Control: Diagnostics, Modeling, Application. [Internet] [Doctoral dissertation]. Delft University of Technology; 2012. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; urn:NBN:nl:ui:24-uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; urn:NBN:nl:ui:24-uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; http://resolver.tudelft.nl/uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025.

Council of Science Editors:

Kotsonis M. Dielectric Barrier Discharge Actuators for Flow Control: Diagnostics, Modeling, Application. [Doctoral Dissertation]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; urn:NBN:nl:ui:24-uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; urn:NBN:nl:ui:24-uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025 ; http://resolver.tudelft.nl/uuid:e10f65c8-0d3e-4d2c-953b-cf460beca025


Delft University of Technology

22. Mo, L. Conceptual Design Study for In-flight Refueling of Passenger Aircraft.

Degree: 2017, Delft University of Technology

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APA (6th Edition):

Mo, L. (2017). Conceptual Design Study for In-flight Refueling of Passenger Aircraft. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5657a63d-1549-4080-8805-a122679cb707 ; urn:NBN:nl:ui:24-uuid:5657a63d-1549-4080-8805-a122679cb707 ; 5657a63d-1549-4080-8805-a122679cb707 ; 10.4233/uuid:5657a63d-1549-4080-8805-a122679cb707 ; urn:isbn:978-94-6295-630-8 ; urn:NBN:nl:ui:24-uuid:5657a63d-1549-4080-8805-a122679cb707 ; http://resolver.tudelft.nl/uuid:5657a63d-1549-4080-8805-a122679cb707

Chicago Manual of Style (16th Edition):

Mo, L. “Conceptual Design Study for In-flight Refueling of Passenger Aircraft.” 2017. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:5657a63d-1549-4080-8805-a122679cb707 ; urn:NBN:nl:ui:24-uuid:5657a63d-1549-4080-8805-a122679cb707 ; 5657a63d-1549-4080-8805-a122679cb707 ; 10.4233/uuid:5657a63d-1549-4080-8805-a122679cb707 ; urn:isbn:978-94-6295-630-8 ; urn:NBN:nl:ui:24-uuid:5657a63d-1549-4080-8805-a122679cb707 ; http://resolver.tudelft.nl/uuid:5657a63d-1549-4080-8805-a122679cb707.

MLA Handbook (7th Edition):

Mo, L. “Conceptual Design Study for In-flight Refueling of Passenger Aircraft.” 2017. Web. 15 Nov 2019.

Vancouver:

Mo L. Conceptual Design Study for In-flight Refueling of Passenger Aircraft. [Internet] [Doctoral dissertation]. Delft University of Technology; 2017. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:5657a63d-1549-4080-8805-a122679cb707 ; urn:NBN:nl:ui:24-uuid:5657a63d-1549-4080-8805-a122679cb707 ; 5657a63d-1549-4080-8805-a122679cb707 ; 10.4233/uuid:5657a63d-1549-4080-8805-a122679cb707 ; urn:isbn:978-94-6295-630-8 ; urn:NBN:nl:ui:24-uuid:5657a63d-1549-4080-8805-a122679cb707 ; http://resolver.tudelft.nl/uuid:5657a63d-1549-4080-8805-a122679cb707.

Council of Science Editors:

Mo L. Conceptual Design Study for In-flight Refueling of Passenger Aircraft. [Doctoral Dissertation]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:5657a63d-1549-4080-8805-a122679cb707 ; urn:NBN:nl:ui:24-uuid:5657a63d-1549-4080-8805-a122679cb707 ; 5657a63d-1549-4080-8805-a122679cb707 ; 10.4233/uuid:5657a63d-1549-4080-8805-a122679cb707 ; urn:isbn:978-94-6295-630-8 ; urn:NBN:nl:ui:24-uuid:5657a63d-1549-4080-8805-a122679cb707 ; http://resolver.tudelft.nl/uuid:5657a63d-1549-4080-8805-a122679cb707


Delft University of Technology

23. Kerklaan, R.A.G. Design tools for the virtual wind tunnel: Setting up the geometry for CFD calculations:.

Degree: 2006, Delft University of Technology

 Momenteel kan de windbelasting op gebouwen op twee manieren worden bepaald: met behulp van de norm (NEN 6702, Eurocode) of door middel van windtunnelproeven. De… (more)

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APA (6th Edition):

Kerklaan, R. A. G. (2006). Design tools for the virtual wind tunnel: Setting up the geometry for CFD calculations:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b81191e8-d955-4942-9dda-fe36348161e1

Chicago Manual of Style (16th Edition):

Kerklaan, R A G. “Design tools for the virtual wind tunnel: Setting up the geometry for CFD calculations:.” 2006. Masters Thesis, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:b81191e8-d955-4942-9dda-fe36348161e1.

MLA Handbook (7th Edition):

Kerklaan, R A G. “Design tools for the virtual wind tunnel: Setting up the geometry for CFD calculations:.” 2006. Web. 15 Nov 2019.

Vancouver:

Kerklaan RAG. Design tools for the virtual wind tunnel: Setting up the geometry for CFD calculations:. [Internet] [Masters thesis]. Delft University of Technology; 2006. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:b81191e8-d955-4942-9dda-fe36348161e1.

Council of Science Editors:

Kerklaan RAG. Design tools for the virtual wind tunnel: Setting up the geometry for CFD calculations:. [Masters Thesis]. Delft University of Technology; 2006. Available from: http://resolver.tudelft.nl/uuid:b81191e8-d955-4942-9dda-fe36348161e1


Delft University of Technology

24. Hoogreef, M.F.M. Advise, Formalize and Integrate MDO Architectures: A Methodology and Implementation.

Degree: 2017, Delft University of Technology

Subjects/Keywords: MDO architectures; semantic web; Multidisciplinary Design Optimization (MDO); ontology; simulation workflows

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APA (6th Edition):

Hoogreef, M. F. M. (2017). Advise, Formalize and Integrate MDO Architectures: A Methodology and Implementation. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; urn:NBN:nl:ui:24-uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; cc2af611-6d78-4439-9b10-7e62ae579029 ; 10.4233/uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; urn:isbn:978-94-028-0682-3 ; urn:NBN:nl:ui:24-uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; http://resolver.tudelft.nl/uuid:cc2af611-6d78-4439-9b10-7e62ae579029

Chicago Manual of Style (16th Edition):

Hoogreef, M F M. “Advise, Formalize and Integrate MDO Architectures: A Methodology and Implementation.” 2017. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; urn:NBN:nl:ui:24-uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; cc2af611-6d78-4439-9b10-7e62ae579029 ; 10.4233/uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; urn:isbn:978-94-028-0682-3 ; urn:NBN:nl:ui:24-uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; http://resolver.tudelft.nl/uuid:cc2af611-6d78-4439-9b10-7e62ae579029.

MLA Handbook (7th Edition):

Hoogreef, M F M. “Advise, Formalize and Integrate MDO Architectures: A Methodology and Implementation.” 2017. Web. 15 Nov 2019.

Vancouver:

Hoogreef MFM. Advise, Formalize and Integrate MDO Architectures: A Methodology and Implementation. [Internet] [Doctoral dissertation]. Delft University of Technology; 2017. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; urn:NBN:nl:ui:24-uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; cc2af611-6d78-4439-9b10-7e62ae579029 ; 10.4233/uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; urn:isbn:978-94-028-0682-3 ; urn:NBN:nl:ui:24-uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; http://resolver.tudelft.nl/uuid:cc2af611-6d78-4439-9b10-7e62ae579029.

Council of Science Editors:

Hoogreef MFM. Advise, Formalize and Integrate MDO Architectures: A Methodology and Implementation. [Doctoral Dissertation]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; urn:NBN:nl:ui:24-uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; cc2af611-6d78-4439-9b10-7e62ae579029 ; 10.4233/uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; urn:isbn:978-94-028-0682-3 ; urn:NBN:nl:ui:24-uuid:cc2af611-6d78-4439-9b10-7e62ae579029 ; http://resolver.tudelft.nl/uuid:cc2af611-6d78-4439-9b10-7e62ae579029


Delft University of Technology

25. Li, Q. Towards optimum swirl recovery for propeller propulsion systems.

Degree: 2019, Delft University of Technology

 In a propeller propulsion system, due to the torque working on the propeller, a rotational motion of the fluid is generated. This rotational motion, expressed… (more)

Subjects/Keywords: propeller; swirl recovery vane; propeller integration

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

APA (6th Edition):

Li, Q. (2019). Towards optimum swirl recovery for propeller propulsion systems. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; ef966464-6b76-434d-b147-81ec247b023c ; 10.4233/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:isbn:978-94-6323-805-2 ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c

Chicago Manual of Style (16th Edition):

Li, Q. “Towards optimum swirl recovery for propeller propulsion systems.” 2019. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; ef966464-6b76-434d-b147-81ec247b023c ; 10.4233/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:isbn:978-94-6323-805-2 ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c.

MLA Handbook (7th Edition):

Li, Q. “Towards optimum swirl recovery for propeller propulsion systems.” 2019. Web. 15 Nov 2019.

Vancouver:

Li Q. Towards optimum swirl recovery for propeller propulsion systems. [Internet] [Doctoral dissertation]. Delft University of Technology; 2019. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; ef966464-6b76-434d-b147-81ec247b023c ; 10.4233/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:isbn:978-94-6323-805-2 ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c.

Council of Science Editors:

Li Q. Towards optimum swirl recovery for propeller propulsion systems. [Doctoral Dissertation]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; ef966464-6b76-434d-b147-81ec247b023c ; 10.4233/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:isbn:978-94-6323-805-2 ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c


Delft University of Technology

26. Sinnige, T. Aerodynamic and Aeroacoustic Interaction Effects for Tip-Mounted Propellers: An Experimental Study.

Degree: 2018, Delft University of Technology

 Propellers can enable a significant reduction in energy use of future aircraft by offering a higher propulsive efficiency than turbofan engines. This is especially relevant… (more)

Subjects/Keywords: Propeller–airframe interactions; propeller aeroacoustics; propeller aerodynamics; propeller slipstream characteristics; tip-mounted propellers; wind-tunnel testing

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

APA (6th Edition):

Sinnige, T. (2018). Aerodynamic and Aeroacoustic Interaction Effects for Tip-Mounted Propellers: An Experimental Study. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; urn:NBN:nl:ui:24-uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; 214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; 10.4233/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; urn:isbn:978-94-9301-446-6 ; urn:NBN:nl:ui:24-uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; http://resolver.tudelft.nl/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b

Chicago Manual of Style (16th Edition):

Sinnige, T. “Aerodynamic and Aeroacoustic Interaction Effects for Tip-Mounted Propellers: An Experimental Study.” 2018. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; urn:NBN:nl:ui:24-uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; 214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; 10.4233/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; urn:isbn:978-94-9301-446-6 ; urn:NBN:nl:ui:24-uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; http://resolver.tudelft.nl/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b.

MLA Handbook (7th Edition):

Sinnige, T. “Aerodynamic and Aeroacoustic Interaction Effects for Tip-Mounted Propellers: An Experimental Study.” 2018. Web. 15 Nov 2019.

Vancouver:

Sinnige T. Aerodynamic and Aeroacoustic Interaction Effects for Tip-Mounted Propellers: An Experimental Study. [Internet] [Doctoral dissertation]. Delft University of Technology; 2018. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; urn:NBN:nl:ui:24-uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; 214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; 10.4233/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; urn:isbn:978-94-9301-446-6 ; urn:NBN:nl:ui:24-uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; http://resolver.tudelft.nl/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b.

Council of Science Editors:

Sinnige T. Aerodynamic and Aeroacoustic Interaction Effects for Tip-Mounted Propellers: An Experimental Study. [Doctoral Dissertation]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; urn:NBN:nl:ui:24-uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; 214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; 10.4233/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; urn:isbn:978-94-9301-446-6 ; urn:NBN:nl:ui:24-uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b ; http://resolver.tudelft.nl/uuid:214e1e9a-c53e-47c7-a12c-b1eb3ec8293b


Delft University of Technology

27. Wu, P. A Physics-based Approach to Assess Critical Load Cases for Landing Gears within Aircraft Conceptual Design.

Degree: 2019, Delft University of Technology

 The European Union and the United States are proposing to bring in more strict flight vehicle emission criteria in their reports of the high‐level groups… (more)

Subjects/Keywords: Flight Dynamics and Loads; Landing Gear; Load Cases; Multidisciplinary Design; Analysis and Optimization

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

APA (6th Edition):

Wu, P. (2019). A Physics-based Approach to Assess Critical Load Cases for Landing Gears within Aircraft Conceptual Design. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; urn:NBN:nl:ui:24-uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; 193f6664-0f19-488f-af6a-21b17ba75be0 ; 10.4233/uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; urn:isbn:978‐94‐6384‐039‐2 ; urn:NBN:nl:ui:24-uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; http://resolver.tudelft.nl/uuid:193f6664-0f19-488f-af6a-21b17ba75be0

Chicago Manual of Style (16th Edition):

Wu, P. “A Physics-based Approach to Assess Critical Load Cases for Landing Gears within Aircraft Conceptual Design.” 2019. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; urn:NBN:nl:ui:24-uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; 193f6664-0f19-488f-af6a-21b17ba75be0 ; 10.4233/uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; urn:isbn:978‐94‐6384‐039‐2 ; urn:NBN:nl:ui:24-uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; http://resolver.tudelft.nl/uuid:193f6664-0f19-488f-af6a-21b17ba75be0.

MLA Handbook (7th Edition):

Wu, P. “A Physics-based Approach to Assess Critical Load Cases for Landing Gears within Aircraft Conceptual Design.” 2019. Web. 15 Nov 2019.

Vancouver:

Wu P. A Physics-based Approach to Assess Critical Load Cases for Landing Gears within Aircraft Conceptual Design. [Internet] [Doctoral dissertation]. Delft University of Technology; 2019. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; urn:NBN:nl:ui:24-uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; 193f6664-0f19-488f-af6a-21b17ba75be0 ; 10.4233/uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; urn:isbn:978‐94‐6384‐039‐2 ; urn:NBN:nl:ui:24-uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; http://resolver.tudelft.nl/uuid:193f6664-0f19-488f-af6a-21b17ba75be0.

Council of Science Editors:

Wu P. A Physics-based Approach to Assess Critical Load Cases for Landing Gears within Aircraft Conceptual Design. [Doctoral Dissertation]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; urn:NBN:nl:ui:24-uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; 193f6664-0f19-488f-af6a-21b17ba75be0 ; 10.4233/uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; urn:isbn:978‐94‐6384‐039‐2 ; urn:NBN:nl:ui:24-uuid:193f6664-0f19-488f-af6a-21b17ba75be0 ; http://resolver.tudelft.nl/uuid:193f6664-0f19-488f-af6a-21b17ba75be0


Delft University of Technology

28. van Gent, I. Agile MDAO Systems: A Graph-based Methodology to Enhance Collaborative Multidisciplinary Design.

Degree: 2019, Delft University of Technology

 The need to continuously design better aircraft is challenging on multiple fronts: the existing tube-and-wing aircraft are difficult to improve further, while more creative configurations… (more)

Subjects/Keywords: MDAO; MDO; Collaborative design

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

APA (6th Edition):

van Gent, I. (2019). Agile MDAO Systems: A Graph-based Methodology to Enhance Collaborative Multidisciplinary Design. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; urn:NBN:nl:ui:24-uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; 10.4233/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; urn:isbn:978-94-6384-067-5 ; urn:NBN:nl:ui:24-uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; http://resolver.tudelft.nl/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af

Chicago Manual of Style (16th Edition):

van Gent, I. “Agile MDAO Systems: A Graph-based Methodology to Enhance Collaborative Multidisciplinary Design.” 2019. Doctoral Dissertation, Delft University of Technology. Accessed November 15, 2019. http://resolver.tudelft.nl/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; urn:NBN:nl:ui:24-uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; 10.4233/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; urn:isbn:978-94-6384-067-5 ; urn:NBN:nl:ui:24-uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; http://resolver.tudelft.nl/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af.

MLA Handbook (7th Edition):

van Gent, I. “Agile MDAO Systems: A Graph-based Methodology to Enhance Collaborative Multidisciplinary Design.” 2019. Web. 15 Nov 2019.

Vancouver:

van Gent I. Agile MDAO Systems: A Graph-based Methodology to Enhance Collaborative Multidisciplinary Design. [Internet] [Doctoral dissertation]. Delft University of Technology; 2019. [cited 2019 Nov 15]. Available from: http://resolver.tudelft.nl/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; urn:NBN:nl:ui:24-uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; 10.4233/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; urn:isbn:978-94-6384-067-5 ; urn:NBN:nl:ui:24-uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; http://resolver.tudelft.nl/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af.

Council of Science Editors:

van Gent I. Agile MDAO Systems: A Graph-based Methodology to Enhance Collaborative Multidisciplinary Design. [Doctoral Dissertation]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; urn:NBN:nl:ui:24-uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; 10.4233/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; urn:isbn:978-94-6384-067-5 ; urn:NBN:nl:ui:24-uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af ; http://resolver.tudelft.nl/uuid:c42b30ba-2ba7-4fff-bf1c-f81f85e890af

.