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

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Delft University of Technology

1. Kinderman, Hendrik Wisse (author). The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.

Degree: 2017, Delft University of Technology

 This research project aims at obtaining a better understanding of vertically translating the wing and the related wing-body interference effects on the drag and sonic… (more)

Subjects/Keywords: sonic boom; vertical wing placement; wave drag; drag; supersonic; pressure signature; lift; zero-lift; area ruling; area rule; Mach; cone

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APA (6th Edition):

Kinderman, H. W. (. (2017). The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef

Chicago Manual of Style (16th Edition):

Kinderman, Hendrik Wisse (author). “The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef.

MLA Handbook (7th Edition):

Kinderman, Hendrik Wisse (author). “The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.” 2017. Web. 23 Jan 2021.

Vancouver:

Kinderman HW(. The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef.

Council of Science Editors:

Kinderman HW(. The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef


Delft University of Technology

2. Gonon, Bastien (author). Evaluation of the One Variable Measured Boundary Condition Method WIN3VE.

Degree: 2012, Delft University of Technology

This thesis is an evaluation of a wall interference correction program called WIN3VE. This program was developed in the 1990s by the National Aerospace Laboratory… (more)

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APA (6th Edition):

Gonon, B. (. (2012). Evaluation of the One Variable Measured Boundary Condition Method WIN3VE. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:7c30200a-8742-4c82-bf84-f776626dc15e

Chicago Manual of Style (16th Edition):

Gonon, Bastien (author). “Evaluation of the One Variable Measured Boundary Condition Method WIN3VE.” 2012. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:7c30200a-8742-4c82-bf84-f776626dc15e.

MLA Handbook (7th Edition):

Gonon, Bastien (author). “Evaluation of the One Variable Measured Boundary Condition Method WIN3VE.” 2012. Web. 23 Jan 2021.

Vancouver:

Gonon B(. Evaluation of the One Variable Measured Boundary Condition Method WIN3VE. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:7c30200a-8742-4c82-bf84-f776626dc15e.

Council of Science Editors:

Gonon B(. Evaluation of the One Variable Measured Boundary Condition Method WIN3VE. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:7c30200a-8742-4c82-bf84-f776626dc15e


Delft University of Technology

3. Flinkerbusch, Arti (author). Oblique Shock Wave-Boundary Layer Interactions Over Porous Plates.

Degree: 2018, Delft University of Technology

 This report discusses an investigation into the effect of a porous plate covering a cavity, on an oblique shock wave-boundary layer interaction. Four porous plates… (more)

Subjects/Keywords: Supersonic; Shock wave boundary layer interaction; shock wave; Aerodynamics

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APA (6th Edition):

Flinkerbusch, A. (. (2018). Oblique Shock Wave-Boundary Layer Interactions Over Porous Plates. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4001ee80-f303-48a6-a9b9-e606fc12d740

Chicago Manual of Style (16th Edition):

Flinkerbusch, Arti (author). “Oblique Shock Wave-Boundary Layer Interactions Over Porous Plates.” 2018. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:4001ee80-f303-48a6-a9b9-e606fc12d740.

MLA Handbook (7th Edition):

Flinkerbusch, Arti (author). “Oblique Shock Wave-Boundary Layer Interactions Over Porous Plates.” 2018. Web. 23 Jan 2021.

Vancouver:

Flinkerbusch A(. Oblique Shock Wave-Boundary Layer Interactions Over Porous Plates. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:4001ee80-f303-48a6-a9b9-e606fc12d740.

Council of Science Editors:

Flinkerbusch A(. Oblique Shock Wave-Boundary Layer Interactions Over Porous Plates. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:4001ee80-f303-48a6-a9b9-e606fc12d740


Delft University of Technology

4. Voogt, Nick (author). Investigation on supersonic, large wall roughness elements using QIRT and PIV.

Degree: 2017, Delft University of Technology

In spaceflight, a launch vehicle is a rocket used to carry a payload from the Earth's surface into outer space. By traveling supersonically, launch vehicles… (more)

Subjects/Keywords: QIRT; supersonic; ribbed roughness; PIV; heat transfer

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APA (6th Edition):

Voogt, N. (. (2017). Investigation on supersonic, large wall roughness elements using QIRT and PIV. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:737e4a9d-75de-4699-88e2-b611f93a88b5

Chicago Manual of Style (16th Edition):

Voogt, Nick (author). “Investigation on supersonic, large wall roughness elements using QIRT and PIV.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:737e4a9d-75de-4699-88e2-b611f93a88b5.

MLA Handbook (7th Edition):

Voogt, Nick (author). “Investigation on supersonic, large wall roughness elements using QIRT and PIV.” 2017. Web. 23 Jan 2021.

Vancouver:

Voogt N(. Investigation on supersonic, large wall roughness elements using QIRT and PIV. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:737e4a9d-75de-4699-88e2-b611f93a88b5.

Council of Science Editors:

Voogt N(. Investigation on supersonic, large wall roughness elements using QIRT and PIV. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:737e4a9d-75de-4699-88e2-b611f93a88b5


Delft University of Technology

5. Mercieca, Edward (author). Spray Characteristics in Gas / Liquid Pintle Injection.

Degree: 2017, Delft University of Technology

In Liquid Rocket Engine (LRE) design, knowledge of how the propellant atomization quality varies with respect to some injector design variables would be useful in… (more)

Subjects/Keywords: LIquid Rocket Engine; Pintle Injector; Drop size distribution; Sauter Mean Diameter; Atomization; Spray; Combustion; Cone Angle

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APA (6th Edition):

Mercieca, E. (. (2017). Spray Characteristics in Gas / Liquid Pintle Injection. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ffcc0e29-e9e7-4042-832b-5bc46e92ef0d

Chicago Manual of Style (16th Edition):

Mercieca, Edward (author). “Spray Characteristics in Gas / Liquid Pintle Injection.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:ffcc0e29-e9e7-4042-832b-5bc46e92ef0d.

MLA Handbook (7th Edition):

Mercieca, Edward (author). “Spray Characteristics in Gas / Liquid Pintle Injection.” 2017. Web. 23 Jan 2021.

Vancouver:

Mercieca E(. Spray Characteristics in Gas / Liquid Pintle Injection. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:ffcc0e29-e9e7-4042-832b-5bc46e92ef0d.

Council of Science Editors:

Mercieca E(. Spray Characteristics in Gas / Liquid Pintle Injection. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:ffcc0e29-e9e7-4042-832b-5bc46e92ef0d


Delft University of Technology

6. Yue, Yang (author). Mean flow analysis and pressure evaluation by means of PIV in transonic baseflow.

Degree: 2012, Delft University of Technology

During atmospheric ascent, flow separation at the base of launch vehicles gives rise to aerodynamic buffeting across the surface of the nozzle (baseflow buffeting). As… (more)

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APA (6th Edition):

Yue, Y. (. (2012). Mean flow analysis and pressure evaluation by means of PIV in transonic baseflow. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:74663a38-1cee-43d4-b805-e2018655c383

Chicago Manual of Style (16th Edition):

Yue, Yang (author). “Mean flow analysis and pressure evaluation by means of PIV in transonic baseflow.” 2012. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:74663a38-1cee-43d4-b805-e2018655c383.

MLA Handbook (7th Edition):

Yue, Yang (author). “Mean flow analysis and pressure evaluation by means of PIV in transonic baseflow.” 2012. Web. 23 Jan 2021.

Vancouver:

Yue Y(. Mean flow analysis and pressure evaluation by means of PIV in transonic baseflow. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:74663a38-1cee-43d4-b805-e2018655c383.

Council of Science Editors:

Yue Y(. Mean flow analysis and pressure evaluation by means of PIV in transonic baseflow. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:74663a38-1cee-43d4-b805-e2018655c383


Delft University of Technology

7. Payanda, Qais (author). The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.

Degree: 2017, Delft University of Technology

 A combined PIV and Schlieren measurements have been carried out in the transonic-supersonic wind tunnel (TST-27) to investigate the effect of exhaust plume and the… (more)

Subjects/Keywords: Space launcher base flow; Aerodynamics; experimental; PIV; Schlieren; buffet; shock wave; Transonic and supersonic wake; Base-nozzle flow interaction

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APA (6th Edition):

Payanda, Q. (. (2017). The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782

Chicago Manual of Style (16th Edition):

Payanda, Qais (author). “The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782.

MLA Handbook (7th Edition):

Payanda, Qais (author). “The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.” 2017. Web. 23 Jan 2021.

Vancouver:

Payanda Q(. The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782.

Council of Science Editors:

Payanda Q(. The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782


Delft University of Technology

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

Degree: 2019, Delft University of Technology

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Camps Pons, Carlos (author). “Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren.” 2019. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:c1a52829-0267-4211-bf93-109fba0db350.

MLA Handbook (7th Edition):

Camps Pons, Carlos (author). “Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren.” 2019. Web. 23 Jan 2021.

Vancouver:

Camps Pons C(. Experimental investigation of transonic buffet on swept wings: A comparative study between 2D and 3D flow and analysis of sweep angle influence using stereoscopic PIV and Background Oriented Schlieren. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:c1a52829-0267-4211-bf93-109fba0db350.

Council of Science Editors:

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


Delft University of Technology

9. van Wijk, Erwin (author). Submerged Ramjet Intake Modeling.

Degree: 2017, Delft University of Technology

 To evaluate the performance of proposed submerged intakes in an early design phase, a performance analysis model able to evaluate a range of intake geometries… (more)

Subjects/Keywords: Ramjet; Intake; Shock wave boundary layer interaction; Modeling; intake performance

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APA (6th Edition):

van Wijk, E. (. (2017). Submerged Ramjet Intake Modeling. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1203a4cc-adae-45ef-abe2-afc7f735ca7a

Chicago Manual of Style (16th Edition):

van Wijk, Erwin (author). “Submerged Ramjet Intake Modeling.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:1203a4cc-adae-45ef-abe2-afc7f735ca7a.

MLA Handbook (7th Edition):

van Wijk, Erwin (author). “Submerged Ramjet Intake Modeling.” 2017. Web. 23 Jan 2021.

Vancouver:

van Wijk E(. Submerged Ramjet Intake Modeling. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:1203a4cc-adae-45ef-abe2-afc7f735ca7a.

Council of Science Editors:

van Wijk E(. Submerged Ramjet Intake Modeling. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:1203a4cc-adae-45ef-abe2-afc7f735ca7a


Delft University of Technology

10. van Weersch, Yorin (author). On the turbulent drag reduction of a dimpled surface under a pressure gradient.

Degree: 2017, Delft University of Technology

 Dimples are spherical indentations applied at a surface that have been found to yield a skin-friction drag reduction within a turbulent boundary layer. Shallow dimples… (more)

Subjects/Keywords: drag reduction; turbulent boundary layer; pressure gradient; dimples

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APA (6th Edition):

van Weersch, Y. (. (2017). On the turbulent drag reduction of a dimpled surface under a pressure gradient. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:cf0b3ec3-f018-4e39-9fd7-587eb75a6c47

Chicago Manual of Style (16th Edition):

van Weersch, Yorin (author). “On the turbulent drag reduction of a dimpled surface under a pressure gradient.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:cf0b3ec3-f018-4e39-9fd7-587eb75a6c47.

MLA Handbook (7th Edition):

van Weersch, Yorin (author). “On the turbulent drag reduction of a dimpled surface under a pressure gradient.” 2017. Web. 23 Jan 2021.

Vancouver:

van Weersch Y(. On the turbulent drag reduction of a dimpled surface under a pressure gradient. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:cf0b3ec3-f018-4e39-9fd7-587eb75a6c47.

Council of Science Editors:

van Weersch Y(. On the turbulent drag reduction of a dimpled surface under a pressure gradient. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:cf0b3ec3-f018-4e39-9fd7-587eb75a6c47


Delft University of Technology

11. Solana Perez, Roberto (author). On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization.

Degree: 2017, Delft University of Technology

This thesis presents an experimental study of the unsteady phenomenon known as transonic buffet. Completely developed in the High Speed Lab of the Aerospace Faculty… (more)

Subjects/Keywords: buffet; aerodynamics; experimental; PIV; Schlieren; shock wave

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APA (6th Edition):

Solana Perez, R. (. (2017). On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d412c786-067d-44cd-9d0e-2d7aea5a4505

Chicago Manual of Style (16th Edition):

Solana Perez, Roberto (author). “On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:d412c786-067d-44cd-9d0e-2d7aea5a4505.

MLA Handbook (7th Edition):

Solana Perez, Roberto (author). “On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization.” 2017. Web. 23 Jan 2021.

Vancouver:

Solana Perez R(. On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:d412c786-067d-44cd-9d0e-2d7aea5a4505.

Council of Science Editors:

Solana Perez R(. On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:d412c786-067d-44cd-9d0e-2d7aea5a4505


Delft University of Technology

12. Dubois, Wouter (author). Enhanced Radiation Cooling: Design of an active thermal protection system.

Degree: 2017, Delft University of Technology

 Current-day space vehicle are equipped with a passive Thermal Protection System (TPS), but these systems operate at the edge of their capabilities. The research into… (more)

Subjects/Keywords: Active thermal protection system; Enhanced radiation cooling; 6 Degree of Freedom modelling

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APA (6th Edition):

Dubois, W. (. (2017). Enhanced Radiation Cooling: Design of an active thermal protection system. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e7a4ba62-6949-41bd-99e7-07170b4c5979

Chicago Manual of Style (16th Edition):

Dubois, Wouter (author). “Enhanced Radiation Cooling: Design of an active thermal protection system.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:e7a4ba62-6949-41bd-99e7-07170b4c5979.

MLA Handbook (7th Edition):

Dubois, Wouter (author). “Enhanced Radiation Cooling: Design of an active thermal protection system.” 2017. Web. 23 Jan 2021.

Vancouver:

Dubois W(. Enhanced Radiation Cooling: Design of an active thermal protection system. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:e7a4ba62-6949-41bd-99e7-07170b4c5979.

Council of Science Editors:

Dubois W(. Enhanced Radiation Cooling: Design of an active thermal protection system. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:e7a4ba62-6949-41bd-99e7-07170b4c5979


Delft University of Technology

13. Ramaswamy, Deepak Prem (author). Investigation of the Effect of a Surface Protuberance on a High Speed Boundary Layer.

Degree: 2017, Delft University of Technology

 One of the major challenges that engineers face when designing a high speed vehicle is aerodynamics heating. While ideally the external surfaces are expected to… (more)

Subjects/Keywords: Infrared Thermometry; protuberance; Transition; Boundary Layer; shock wave

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APA (6th Edition):

Ramaswamy, D. P. (. (2017). Investigation of the Effect of a Surface Protuberance on a High Speed Boundary Layer. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f68ba044-79c6-441e-84de-12029d1650f6

Chicago Manual of Style (16th Edition):

Ramaswamy, Deepak Prem (author). “Investigation of the Effect of a Surface Protuberance on a High Speed Boundary Layer.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:f68ba044-79c6-441e-84de-12029d1650f6.

MLA Handbook (7th Edition):

Ramaswamy, Deepak Prem (author). “Investigation of the Effect of a Surface Protuberance on a High Speed Boundary Layer.” 2017. Web. 23 Jan 2021.

Vancouver:

Ramaswamy DP(. Investigation of the Effect of a Surface Protuberance on a High Speed Boundary Layer. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:f68ba044-79c6-441e-84de-12029d1650f6.

Council of Science Editors:

Ramaswamy DP(. Investigation of the Effect of a Surface Protuberance on a High Speed Boundary Layer. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:f68ba044-79c6-441e-84de-12029d1650f6


Delft University of Technology

14. Srivastava, A. (author). Experimental Characterization of a Micro-ramp Wake and its Flow Mixing Properties in Supersonic Flow.

Degree: 2014, Delft University of Technology

Micro-ramps are currently being investigated as a means of reducing negative effects of shock wave-turbulent boundary layer interactions. A micro-ramp enhances the mixing of the… (more)

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APA (6th Edition):

Srivastava, A. (. (2014). Experimental Characterization of a Micro-ramp Wake and its Flow Mixing Properties in Supersonic Flow. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:084f2da6-d554-4b51-b605-e10a0f1d1785

Chicago Manual of Style (16th Edition):

Srivastava, A (author). “Experimental Characterization of a Micro-ramp Wake and its Flow Mixing Properties in Supersonic Flow.” 2014. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:084f2da6-d554-4b51-b605-e10a0f1d1785.

MLA Handbook (7th Edition):

Srivastava, A (author). “Experimental Characterization of a Micro-ramp Wake and its Flow Mixing Properties in Supersonic Flow.” 2014. Web. 23 Jan 2021.

Vancouver:

Srivastava A(. Experimental Characterization of a Micro-ramp Wake and its Flow Mixing Properties in Supersonic Flow. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:084f2da6-d554-4b51-b605-e10a0f1d1785.

Council of Science Editors:

Srivastava A(. Experimental Characterization of a Micro-ramp Wake and its Flow Mixing Properties in Supersonic Flow. [Masters Thesis]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:084f2da6-d554-4b51-b605-e10a0f1d1785


Delft University of Technology

15. Krishna, Swathi (author). Characterization of the flow-field in circular subsonic impinging jets: Investigation of surface pressure fluctuations and far-field noise emissions through pressure sensor measurements.

Degree: 2012, Delft University of Technology

Impinging jets are relevant ow configurations in many technological developments. For example, on some short take-off and landing aircraft the high speed exhaust from the… (more)

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APA (6th Edition):

Krishna, S. (. (2012). Characterization of the flow-field in circular subsonic impinging jets: Investigation of surface pressure fluctuations and far-field noise emissions through pressure sensor measurements. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5e842ec6-8da8-411c-b04b-ab0df1343558

Chicago Manual of Style (16th Edition):

Krishna, Swathi (author). “Characterization of the flow-field in circular subsonic impinging jets: Investigation of surface pressure fluctuations and far-field noise emissions through pressure sensor measurements.” 2012. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:5e842ec6-8da8-411c-b04b-ab0df1343558.

MLA Handbook (7th Edition):

Krishna, Swathi (author). “Characterization of the flow-field in circular subsonic impinging jets: Investigation of surface pressure fluctuations and far-field noise emissions through pressure sensor measurements.” 2012. Web. 23 Jan 2021.

Vancouver:

Krishna S(. Characterization of the flow-field in circular subsonic impinging jets: Investigation of surface pressure fluctuations and far-field noise emissions through pressure sensor measurements. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:5e842ec6-8da8-411c-b04b-ab0df1343558.

Council of Science Editors:

Krishna S(. Characterization of the flow-field in circular subsonic impinging jets: Investigation of surface pressure fluctuations and far-field noise emissions through pressure sensor measurements. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:5e842ec6-8da8-411c-b04b-ab0df1343558


Delft University of Technology

16. van Pelt, Hilbert (author). Flow modelling in supersonic flows over surfaces with large roughness heights.

Degree: 2013, Delft University of Technology

Flow over smooth surfaces has been studied ever since the start of aerodynamic research. Non-smooth irregularities in rough walled surfaces will impact on the flow… (more)

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APA (6th Edition):

van Pelt, H. (. (2013). Flow modelling in supersonic flows over surfaces with large roughness heights. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:af468b85-ef8e-44f3-aad6-4b6821418db5

Chicago Manual of Style (16th Edition):

van Pelt, Hilbert (author). “Flow modelling in supersonic flows over surfaces with large roughness heights.” 2013. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:af468b85-ef8e-44f3-aad6-4b6821418db5.

MLA Handbook (7th Edition):

van Pelt, Hilbert (author). “Flow modelling in supersonic flows over surfaces with large roughness heights.” 2013. Web. 23 Jan 2021.

Vancouver:

van Pelt H(. Flow modelling in supersonic flows over surfaces with large roughness heights. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:af468b85-ef8e-44f3-aad6-4b6821418db5.

Council of Science Editors:

van Pelt H(. Flow modelling in supersonic flows over surfaces with large roughness heights. [Masters Thesis]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:af468b85-ef8e-44f3-aad6-4b6821418db5


Delft University of Technology

17. Benjamin, Leroy (author). Investigation of instability growth in a hypersonic boundary layer using schlieren visualization.

Degree: 2017, Delft University of Technology

Hypersonic boundary layer transition plays a significant role in the design of hypersonic vehicles as a turbulent boundary layer has higher heat transfer compared to… (more)

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APA (6th Edition):

Benjamin, L. (. (2017). Investigation of instability growth in a hypersonic boundary layer using schlieren visualization. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:2453a50f-891d-40b2-881d-8ac797d91123

Chicago Manual of Style (16th Edition):

Benjamin, Leroy (author). “Investigation of instability growth in a hypersonic boundary layer using schlieren visualization.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:2453a50f-891d-40b2-881d-8ac797d91123.

MLA Handbook (7th Edition):

Benjamin, Leroy (author). “Investigation of instability growth in a hypersonic boundary layer using schlieren visualization.” 2017. Web. 23 Jan 2021.

Vancouver:

Benjamin L(. Investigation of instability growth in a hypersonic boundary layer using schlieren visualization. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:2453a50f-891d-40b2-881d-8ac797d91123.

Council of Science Editors:

Benjamin L(. Investigation of instability growth in a hypersonic boundary layer using schlieren visualization. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:2453a50f-891d-40b2-881d-8ac797d91123


Delft University of Technology

18. Louman, Renee (author). The effect of tripping devices on a shock wave - boundary layer interaction.

Degree: 2015, Delft University of Technology

Shock Wave Boundary Layer Interactions (SWBLIs) occur frequently in supersonic and hypersonic flows and, depending on the strength of the shock wave and the state… (more)

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APA (6th Edition):

Louman, R. (. (2015). The effect of tripping devices on a shock wave - boundary layer interaction. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:742ec2a1-708e-41d8-95ea-27a2c0160045

Chicago Manual of Style (16th Edition):

Louman, Renee (author). “The effect of tripping devices on a shock wave - boundary layer interaction.” 2015. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:742ec2a1-708e-41d8-95ea-27a2c0160045.

MLA Handbook (7th Edition):

Louman, Renee (author). “The effect of tripping devices on a shock wave - boundary layer interaction.” 2015. Web. 23 Jan 2021.

Vancouver:

Louman R(. The effect of tripping devices on a shock wave - boundary layer interaction. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:742ec2a1-708e-41d8-95ea-27a2c0160045.

Council of Science Editors:

Louman R(. The effect of tripping devices on a shock wave - boundary layer interaction. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:742ec2a1-708e-41d8-95ea-27a2c0160045


Delft University of Technology

19. van Nesselrooij, Michiel (author). On the drag reduction of dimpled surfaces in turbulent boundary layers: Proof of concept and identification of flow structure.

Degree: 2015, Delft University of Technology

The drag characteristics and flows structures over flat surfaces with a pattern of shallow rounded spherical dimples were studied. Such dimpled surfaces have been investigated… (more)

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APA (6th Edition):

van Nesselrooij, M. (. (2015). On the drag reduction of dimpled surfaces in turbulent boundary layers: Proof of concept and identification of flow structure. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:dee8edc0-fd9a-4398-b35a-a1b6f7a45315

Chicago Manual of Style (16th Edition):

van Nesselrooij, Michiel (author). “On the drag reduction of dimpled surfaces in turbulent boundary layers: Proof of concept and identification of flow structure.” 2015. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:dee8edc0-fd9a-4398-b35a-a1b6f7a45315.

MLA Handbook (7th Edition):

van Nesselrooij, Michiel (author). “On the drag reduction of dimpled surfaces in turbulent boundary layers: Proof of concept and identification of flow structure.” 2015. Web. 23 Jan 2021.

Vancouver:

van Nesselrooij M(. On the drag reduction of dimpled surfaces in turbulent boundary layers: Proof of concept and identification of flow structure. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:dee8edc0-fd9a-4398-b35a-a1b6f7a45315.

Council of Science Editors:

van Nesselrooij M(. On the drag reduction of dimpled surfaces in turbulent boundary layers: Proof of concept and identification of flow structure. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:dee8edc0-fd9a-4398-b35a-a1b6f7a45315


Delft University of Technology

20. Theuns, Lieselotte (author). Characterization of off-stagnation point pyrolysis in plasma flows using optical measurement techniques.

Degree: 2015, Delft University of Technology

After the invention of the rocket mankind saw a new possibility to study the universe and other planets than Earth by space travel. Since then… (more)

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APA (6th Edition):

Theuns, L. (. (2015). Characterization of off-stagnation point pyrolysis in plasma flows using optical measurement techniques. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:05c96802-1a35-40ff-a760-092c725d9069

Chicago Manual of Style (16th Edition):

Theuns, Lieselotte (author). “Characterization of off-stagnation point pyrolysis in plasma flows using optical measurement techniques.” 2015. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:05c96802-1a35-40ff-a760-092c725d9069.

MLA Handbook (7th Edition):

Theuns, Lieselotte (author). “Characterization of off-stagnation point pyrolysis in plasma flows using optical measurement techniques.” 2015. Web. 23 Jan 2021.

Vancouver:

Theuns L(. Characterization of off-stagnation point pyrolysis in plasma flows using optical measurement techniques. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:05c96802-1a35-40ff-a760-092c725d9069.

Council of Science Editors:

Theuns L(. Characterization of off-stagnation point pyrolysis in plasma flows using optical measurement techniques. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:05c96802-1a35-40ff-a760-092c725d9069


Delft University of Technology

21. Zhang, Quan (author). Development of a data fusion framework for the aerodynamic analysis of launchers.

Degree: 2017, Delft University of Technology

During the launching vehicles design and their optimization process, the implementing of aerodynamic characteristics (AC) database is quite important. Accuracy of such database determines quality… (more)

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APA (6th Edition):

Zhang, Q. (. (2017). Development of a data fusion framework for the aerodynamic analysis of launchers. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:bc5caa33-e99e-4c2a-8d1c-be3ead860452

Chicago Manual of Style (16th Edition):

Zhang, Quan (author). “Development of a data fusion framework for the aerodynamic analysis of launchers.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:bc5caa33-e99e-4c2a-8d1c-be3ead860452.

MLA Handbook (7th Edition):

Zhang, Quan (author). “Development of a data fusion framework for the aerodynamic analysis of launchers.” 2017. Web. 23 Jan 2021.

Vancouver:

Zhang Q(. Development of a data fusion framework for the aerodynamic analysis of launchers. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:bc5caa33-e99e-4c2a-8d1c-be3ead860452.

Council of Science Editors:

Zhang Q(. Development of a data fusion framework for the aerodynamic analysis of launchers. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:bc5caa33-e99e-4c2a-8d1c-be3ead860452


Delft University of Technology

22. Ekelschot, Dirk (author). Investigation of Gortler vortices in hypersonic flow using Quantitative Infrared Thermography (QIRT) and Tomographic Particle Image Velocimetry (Tomo-PIV).

Degree: 2012, Delft University of Technology

Aerodynamic heating is one of the driving aspects in hypersonic vehicle design. During take-off and re-entry, high heat loads are encountered for which the appropriate… (more)

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APA (6th Edition):

Ekelschot, D. (. (2012). Investigation of Gortler vortices in hypersonic flow using Quantitative Infrared Thermography (QIRT) and Tomographic Particle Image Velocimetry (Tomo-PIV). (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1e304e24-dfc1-4145-bbcf-2c47cafa699d

Chicago Manual of Style (16th Edition):

Ekelschot, Dirk (author). “Investigation of Gortler vortices in hypersonic flow using Quantitative Infrared Thermography (QIRT) and Tomographic Particle Image Velocimetry (Tomo-PIV).” 2012. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:1e304e24-dfc1-4145-bbcf-2c47cafa699d.

MLA Handbook (7th Edition):

Ekelschot, Dirk (author). “Investigation of Gortler vortices in hypersonic flow using Quantitative Infrared Thermography (QIRT) and Tomographic Particle Image Velocimetry (Tomo-PIV).” 2012. Web. 23 Jan 2021.

Vancouver:

Ekelschot D(. Investigation of Gortler vortices in hypersonic flow using Quantitative Infrared Thermography (QIRT) and Tomographic Particle Image Velocimetry (Tomo-PIV). [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:1e304e24-dfc1-4145-bbcf-2c47cafa699d.

Council of Science Editors:

Ekelschot D(. Investigation of Gortler vortices in hypersonic flow using Quantitative Infrared Thermography (QIRT) and Tomographic Particle Image Velocimetry (Tomo-PIV). [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:1e304e24-dfc1-4145-bbcf-2c47cafa699d


Delft University of Technology

23. Santiago Patterson, Jaime (author). Experimental Study of Shock-Shock Interactions with Variable Inflow Mach Number.

Degree: 2019, Delft University of Technology

An experimental investigation on shock-shock interactions has been conducted with the aim of studying the transition between Regular (RI) and Mach interactions (MI) under the… (more)

Subjects/Keywords: Supersonic; Shockwave; Interaction; Transition; Schlieren; Focusing Schlieren; Aerodynamics

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APA (6th Edition):

Santiago Patterson, J. (. (2019). Experimental Study of Shock-Shock Interactions with Variable Inflow Mach Number. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:da9bfc58-7b4e-4de6-81ef-1941856566d6

Chicago Manual of Style (16th Edition):

Santiago Patterson, Jaime (author). “Experimental Study of Shock-Shock Interactions with Variable Inflow Mach Number.” 2019. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:da9bfc58-7b4e-4de6-81ef-1941856566d6.

MLA Handbook (7th Edition):

Santiago Patterson, Jaime (author). “Experimental Study of Shock-Shock Interactions with Variable Inflow Mach Number.” 2019. Web. 23 Jan 2021.

Vancouver:

Santiago Patterson J(. Experimental Study of Shock-Shock Interactions with Variable Inflow Mach Number. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:da9bfc58-7b4e-4de6-81ef-1941856566d6.

Council of Science Editors:

Santiago Patterson J(. Experimental Study of Shock-Shock Interactions with Variable Inflow Mach Number. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:da9bfc58-7b4e-4de6-81ef-1941856566d6


Delft University of Technology

24. Kwakman, Koen (author). Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance.

Degree: 2019, Delft University of Technology

 Since ramjet propulsion eliminates the need for oxidizers, it provides an alternative to classic rocket engines for missiles and projectiles. However, to capture free-stream air,… (more)

Subjects/Keywords: Submerged; Supersonic; Intake; Inlet; Flush; Ramjet; Propulsion; Missile; Airbreathing

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APA (6th Edition):

Kwakman, K. (. (2019). Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:671fa0bd-d6e5-4159-b29d-6f09dda6dcce

Chicago Manual of Style (16th Edition):

Kwakman, Koen (author). “Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance.” 2019. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:671fa0bd-d6e5-4159-b29d-6f09dda6dcce.

MLA Handbook (7th Edition):

Kwakman, Koen (author). “Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance.” 2019. Web. 23 Jan 2021.

Vancouver:

Kwakman K(. Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:671fa0bd-d6e5-4159-b29d-6f09dda6dcce.

Council of Science Editors:

Kwakman K(. Submerged Supersonic Air Intakes: An experimental investigation and inviscid study into their preformance. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:671fa0bd-d6e5-4159-b29d-6f09dda6dcce


Delft University of Technology

25. Pfeifle, Ole (author). Aerodynamic Investigation of an Exit Guide Vane Followed by a Curved Duct: A Numerical Study.

Degree: 2017, Delft University of Technology

 Curved exhaust ducts are used in aero engine applications for different purposes, including thrust vectoring, shielding of parts from the exhaust or improving stealth properties.… (more)

Subjects/Keywords: CFD; turbulent flow; 90° elbow bend; flow separation; sensitivity study; Exit Guide Vane

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APA (6th Edition):

Pfeifle, O. (. (2017). Aerodynamic Investigation of an Exit Guide Vane Followed by a Curved Duct: A Numerical Study. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:09dc7b81-d268-4e93-be17-b6f0c683c361

Chicago Manual of Style (16th Edition):

Pfeifle, Ole (author). “Aerodynamic Investigation of an Exit Guide Vane Followed by a Curved Duct: A Numerical Study.” 2017. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:09dc7b81-d268-4e93-be17-b6f0c683c361.

MLA Handbook (7th Edition):

Pfeifle, Ole (author). “Aerodynamic Investigation of an Exit Guide Vane Followed by a Curved Duct: A Numerical Study.” 2017. Web. 23 Jan 2021.

Vancouver:

Pfeifle O(. Aerodynamic Investigation of an Exit Guide Vane Followed by a Curved Duct: A Numerical Study. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:09dc7b81-d268-4e93-be17-b6f0c683c361.

Council of Science Editors:

Pfeifle O(. Aerodynamic Investigation of an Exit Guide Vane Followed by a Curved Duct: A Numerical Study. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:09dc7b81-d268-4e93-be17-b6f0c683c361


Delft University of Technology

26. Huijts, Melchior (author). An experimental and numerical investigation of the aerodynamic characteristics of a flameless combustor.

Degree: 2018, Delft University of Technology

 NOx emissions cause harm to the human body, the world around us and our atmosphere, both directly and indirectly. Flameless combustion is a combustion regime… (more)

Subjects/Keywords: Flameless Combustion; PIV; RANS; CFD; Recirculation; Entrainment; Experimental; Numerical

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APA (6th Edition):

Huijts, M. (. (2018). An experimental and numerical investigation of the aerodynamic characteristics of a flameless combustor. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:acf41200-c4f4-4004-8d24-dcc5f8d6dd7c

Chicago Manual of Style (16th Edition):

Huijts, Melchior (author). “An experimental and numerical investigation of the aerodynamic characteristics of a flameless combustor.” 2018. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:acf41200-c4f4-4004-8d24-dcc5f8d6dd7c.

MLA Handbook (7th Edition):

Huijts, Melchior (author). “An experimental and numerical investigation of the aerodynamic characteristics of a flameless combustor.” 2018. Web. 23 Jan 2021.

Vancouver:

Huijts M(. An experimental and numerical investigation of the aerodynamic characteristics of a flameless combustor. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:acf41200-c4f4-4004-8d24-dcc5f8d6dd7c.

Council of Science Editors:

Huijts M(. An experimental and numerical investigation of the aerodynamic characteristics of a flameless combustor. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:acf41200-c4f4-4004-8d24-dcc5f8d6dd7c


Delft University of Technology

27. Deka, Antaran (author). Manipulation of particles in a Hele-Shaw cell using sources and sinks.

Degree: 2018, Delft University of Technology

The interest in manipulating particles, droplets and bubbles have garnered significant attention in recent years, owing to the advantages offered by micro-fluidics and the advancement… (more)

Subjects/Keywords: Hele-Shaw cell; sources and sinks; Volume illuminated PIV; Particle manipulation

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APA (6th Edition):

Deka, A. (. (2018). Manipulation of particles in a Hele-Shaw cell using sources and sinks. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:fe2ef1cc-836a-4ad0-bbe8-c60bed1dd592

Chicago Manual of Style (16th Edition):

Deka, Antaran (author). “Manipulation of particles in a Hele-Shaw cell using sources and sinks.” 2018. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:fe2ef1cc-836a-4ad0-bbe8-c60bed1dd592.

MLA Handbook (7th Edition):

Deka, Antaran (author). “Manipulation of particles in a Hele-Shaw cell using sources and sinks.” 2018. Web. 23 Jan 2021.

Vancouver:

Deka A(. Manipulation of particles in a Hele-Shaw cell using sources and sinks. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:fe2ef1cc-836a-4ad0-bbe8-c60bed1dd592.

Council of Science Editors:

Deka A(. Manipulation of particles in a Hele-Shaw cell using sources and sinks. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:fe2ef1cc-836a-4ad0-bbe8-c60bed1dd592


Delft University of Technology

28. Mertens, Christoph (author). Unsteady Boundary Layer Transition Measurements with Infrared Thermography: Development of Improved Measurement Schemes.

Degree: 2018, Delft University of Technology

 The boundary layer transition location is a crucial design parameter in aerodynamics. The computational prediction of boundary layer transition in engineering applications is typically based… (more)

Subjects/Keywords: Boundary Layer Transition; Unsteady Aerodynamics; Pitching Airfoil; Wind Tunnel Experiment; Measurement Technique

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APA (6th Edition):

Mertens, C. (. (2018). Unsteady Boundary Layer Transition Measurements with Infrared Thermography: Development of Improved Measurement Schemes. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c9ef5823-c258-4c11-82b3-b7aaae78fa7d

Chicago Manual of Style (16th Edition):

Mertens, Christoph (author). “Unsteady Boundary Layer Transition Measurements with Infrared Thermography: Development of Improved Measurement Schemes.” 2018. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:c9ef5823-c258-4c11-82b3-b7aaae78fa7d.

MLA Handbook (7th Edition):

Mertens, Christoph (author). “Unsteady Boundary Layer Transition Measurements with Infrared Thermography: Development of Improved Measurement Schemes.” 2018. Web. 23 Jan 2021.

Vancouver:

Mertens C(. Unsteady Boundary Layer Transition Measurements with Infrared Thermography: Development of Improved Measurement Schemes. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:c9ef5823-c258-4c11-82b3-b7aaae78fa7d.

Council of Science Editors:

Mertens C(. Unsteady Boundary Layer Transition Measurements with Infrared Thermography: Development of Improved Measurement Schemes. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:c9ef5823-c258-4c11-82b3-b7aaae78fa7d

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