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You searched for +publisher:"Rice University" +contributor:("Tezduyar, Tayfun E"). Showing records 1 – 30 of 36 total matches.

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Rice University

1. Zhang, Yutong. Computational Flow Analysis of a Cyclone Vacuum Cleaner.

Degree: MS, Mechanical Engineering, 2019, Rice University

 Computational flow analysis of a cyclone vacuum cleaner can provide valuable fluid mechanics information for efficient design and operation. The vacuum cleaner is made of… (more)

Subjects/Keywords: Fluid Mechanics; Computational Fluid Mechanics

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APA (6th Edition):

Zhang, Y. (2019). Computational Flow Analysis of a Cyclone Vacuum Cleaner. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/105403

Chicago Manual of Style (16th Edition):

Zhang, Yutong. “Computational Flow Analysis of a Cyclone Vacuum Cleaner.” 2019. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/105403.

MLA Handbook (7th Edition):

Zhang, Yutong. “Computational Flow Analysis of a Cyclone Vacuum Cleaner.” 2019. Web. 16 Apr 2021.

Vancouver:

Zhang Y. Computational Flow Analysis of a Cyclone Vacuum Cleaner. [Internet] [Masters thesis]. Rice University; 2019. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/105403.

Council of Science Editors:

Zhang Y. Computational Flow Analysis of a Cyclone Vacuum Cleaner. [Masters Thesis]. Rice University; 2019. Available from: http://hdl.handle.net/1911/105403


Rice University

2. Mei, Sen. Computational Analysis of Flow in a Turbocharger Turbine with Pulsating Inflow.

Degree: MS, Engineering, 2016, Rice University

 The turbine of an automobile turbocharger commonly operates under pulsating inflow, which leads to an undesired “hysteresis” performance. This study is to investigate this phenomenon… (more)

Subjects/Keywords: Turbocharger; Turbine; Pulsating inflow; Space–Time VMS method; Slip interfaces; ST-SI; Isogeometric Analysis; NURBS; weakly-imposed Dirichlet conditions

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APA (6th Edition):

Mei, S. (2016). Computational Analysis of Flow in a Turbocharger Turbine with Pulsating Inflow. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/95639

Chicago Manual of Style (16th Edition):

Mei, Sen. “Computational Analysis of Flow in a Turbocharger Turbine with Pulsating Inflow.” 2016. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/95639.

MLA Handbook (7th Edition):

Mei, Sen. “Computational Analysis of Flow in a Turbocharger Turbine with Pulsating Inflow.” 2016. Web. 16 Apr 2021.

Vancouver:

Mei S. Computational Analysis of Flow in a Turbocharger Turbine with Pulsating Inflow. [Internet] [Masters thesis]. Rice University; 2016. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/95639.

Council of Science Editors:

Mei S. Computational Analysis of Flow in a Turbocharger Turbine with Pulsating Inflow. [Masters Thesis]. Rice University; 2016. Available from: http://hdl.handle.net/1911/95639


Rice University

3. Yu, Yuxuan. Coronary Artery Computational Flow Analysis with Isogeometric Discretization.

Degree: MS, Engineering, 2017, Rice University

 Patient-specific computational flow analysis of the coronary artery can provide valuable information that the doctor can use in making treatment decisions. Reliable analysis requires addressing… (more)

Subjects/Keywords: Estimated element-based zero-stress state; Coronary artery flow; Time-dependent anatomical model; Isogeometric discretization; Space–Time VMS method

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APA (6th Edition):

Yu, Y. (2017). Coronary Artery Computational Flow Analysis with Isogeometric Discretization. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/105460

Chicago Manual of Style (16th Edition):

Yu, Yuxuan. “Coronary Artery Computational Flow Analysis with Isogeometric Discretization.” 2017. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/105460.

MLA Handbook (7th Edition):

Yu, Yuxuan. “Coronary Artery Computational Flow Analysis with Isogeometric Discretization.” 2017. Web. 16 Apr 2021.

Vancouver:

Yu Y. Coronary Artery Computational Flow Analysis with Isogeometric Discretization. [Internet] [Masters thesis]. Rice University; 2017. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/105460.

Council of Science Editors:

Yu Y. Coronary Artery Computational Flow Analysis with Isogeometric Discretization. [Masters Thesis]. Rice University; 2017. Available from: http://hdl.handle.net/1911/105460

4. Wright, Samuel E., III. Advanced fluid-structure interaction techniques for modeling ringsail parachutes.

Degree: MS, Engineering, 2010, Rice University

 The Team for Advanced Flow Simulation and Modeling (T☆FSM) at Rice University specializes in developing fluid-structure interaction (FSI) modeling techniques for several classes of challenging… (more)

Subjects/Keywords: Applied mechanics; Aerospace engineering; Mechanical engineering

…Grant CNS-0421109, and a partnership among Rice University, AMD and CRAY. Contents Abstract… …x29; [tafsm.org] at Rice University has extensive experience with FSI modeling of… 

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APA (6th Edition):

Wright, Samuel E., I. (2010). Advanced fluid-structure interaction techniques for modeling ringsail parachutes. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/62116

Chicago Manual of Style (16th Edition):

Wright, Samuel E., III. “Advanced fluid-structure interaction techniques for modeling ringsail parachutes.” 2010. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/62116.

MLA Handbook (7th Edition):

Wright, Samuel E., III. “Advanced fluid-structure interaction techniques for modeling ringsail parachutes.” 2010. Web. 16 Apr 2021.

Vancouver:

Wright, Samuel E. I. Advanced fluid-structure interaction techniques for modeling ringsail parachutes. [Internet] [Masters thesis]. Rice University; 2010. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/62116.

Council of Science Editors:

Wright, Samuel E. I. Advanced fluid-structure interaction techniques for modeling ringsail parachutes. [Masters Thesis]. Rice University; 2010. Available from: http://hdl.handle.net/1911/62116

5. Pan, Linqi. A Study on Weakly-Imposed Dirichlet Boundary Conditions in Internal Flows.

Degree: MS, Engineering, 2016, Rice University

 This thesis is on weakly-imposed Dirichlet boundary conditions in incompressible and compressible flow. Our target is internal flows. The weakly-imposed conditions are compared with strongly-imposed… (more)

Subjects/Keywords: Weakly-imposed Dirichlet boundary condition

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APA (6th Edition):

Pan, L. (2016). A Study on Weakly-Imposed Dirichlet Boundary Conditions in Internal Flows. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/96612

Chicago Manual of Style (16th Edition):

Pan, Linqi. “A Study on Weakly-Imposed Dirichlet Boundary Conditions in Internal Flows.” 2016. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/96612.

MLA Handbook (7th Edition):

Pan, Linqi. “A Study on Weakly-Imposed Dirichlet Boundary Conditions in Internal Flows.” 2016. Web. 16 Apr 2021.

Vancouver:

Pan L. A Study on Weakly-Imposed Dirichlet Boundary Conditions in Internal Flows. [Internet] [Masters thesis]. Rice University; 2016. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/96612.

Council of Science Editors:

Pan L. A Study on Weakly-Imposed Dirichlet Boundary Conditions in Internal Flows. [Masters Thesis]. Rice University; 2016. Available from: http://hdl.handle.net/1911/96612

6. Zhang, Ruochun. Computation of Flapping-Wing Fluid–Structure Interaction.

Degree: MS, Engineering, 2016, Rice University

 This thesis is on computational fluid–structure interaction (FSI) analysis of bioinspired wing flapping, based on an actual locust in wind tunnel. The wing motion is… (more)

Subjects/Keywords: FSI; wing flapping; near topology changes; Space–Time Slip Interface method; ST-SI; Space–Time Variational Multiscale method; ST-VMS

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APA (6th Edition):

Zhang, R. (2016). Computation of Flapping-Wing Fluid–Structure Interaction. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/96611

Chicago Manual of Style (16th Edition):

Zhang, Ruochun. “Computation of Flapping-Wing Fluid–Structure Interaction.” 2016. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/96611.

MLA Handbook (7th Edition):

Zhang, Ruochun. “Computation of Flapping-Wing Fluid–Structure Interaction.” 2016. Web. 16 Apr 2021.

Vancouver:

Zhang R. Computation of Flapping-Wing Fluid–Structure Interaction. [Internet] [Masters thesis]. Rice University; 2016. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/96611.

Council of Science Editors:

Zhang R. Computation of Flapping-Wing Fluid–Structure Interaction. [Masters Thesis]. Rice University; 2016. Available from: http://hdl.handle.net/1911/96611

7. Fu, Mingyuan. Computational Analysis of a Diesel Engine Exhaust Manifold and Turbocharger Turbine.

Degree: MS, Engineering, 2018, Rice University

 The unsteady nature of the flow in turbocharges makes computational flow analysis challenging. The unsteadiness comes from the engine cycle and the flow in the… (more)

Subjects/Keywords: Turbocharger turbine; Space-time method

…Modeling (TFAFSM) at Rice University and Waseda University. The core technique is the… 

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APA (6th Edition):

Fu, M. (2018). Computational Analysis of a Diesel Engine Exhaust Manifold and Turbocharger Turbine. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/105781

Chicago Manual of Style (16th Edition):

Fu, Mingyuan. “Computational Analysis of a Diesel Engine Exhaust Manifold and Turbocharger Turbine.” 2018. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/105781.

MLA Handbook (7th Edition):

Fu, Mingyuan. “Computational Analysis of a Diesel Engine Exhaust Manifold and Turbocharger Turbine.” 2018. Web. 16 Apr 2021.

Vancouver:

Fu M. Computational Analysis of a Diesel Engine Exhaust Manifold and Turbocharger Turbine. [Internet] [Masters thesis]. Rice University; 2018. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/105781.

Council of Science Editors:

Fu M. Computational Analysis of a Diesel Engine Exhaust Manifold and Turbocharger Turbine. [Masters Thesis]. Rice University; 2018. Available from: http://hdl.handle.net/1911/105781

8. Zhang, Yutong. Computational Flow Analysis of a Cyclone Vacuum Cleaner.

Degree: MS, Engineering, 2019, Rice University

 Computational flow analysis of a cyclone vacuum cleaner can provide valuable fluid mechanics information for efficient design and operation. The vacuum cleaner is made of… (more)

Subjects/Keywords: Fluid Mechanics; Computational Fluid Mechanics

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APA (6th Edition):

Zhang, Y. (2019). Computational Flow Analysis of a Cyclone Vacuum Cleaner. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/105402

Chicago Manual of Style (16th Edition):

Zhang, Yutong. “Computational Flow Analysis of a Cyclone Vacuum Cleaner.” 2019. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/105402.

MLA Handbook (7th Edition):

Zhang, Yutong. “Computational Flow Analysis of a Cyclone Vacuum Cleaner.” 2019. Web. 16 Apr 2021.

Vancouver:

Zhang Y. Computational Flow Analysis of a Cyclone Vacuum Cleaner. [Internet] [Masters thesis]. Rice University; 2019. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/105402.

Council of Science Editors:

Zhang Y. Computational Flow Analysis of a Cyclone Vacuum Cleaner. [Masters Thesis]. Rice University; 2019. Available from: http://hdl.handle.net/1911/105402


Rice University

9. Montel, Kenneth Keef. Fluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamics.

Degree: MS, Engineering, 2015, Rice University

 This thesis is on computational fluid-structure interaction (FSI) modeling of bioinspired flapping-wing aerodynamics of a micro aerial vehicle (MAV). The wing motion is prescribed partially,… (more)

Subjects/Keywords: Micro aerial vehicle; Bio-inspired flapping; Locust; Fluid – Structure Interaction; Space – time techniques; Block-Iterative Coupling

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APA (6th Edition):

Montel, K. K. (2015). Fluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamics. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/88237

Chicago Manual of Style (16th Edition):

Montel, Kenneth Keef. “Fluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamics.” 2015. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/88237.

MLA Handbook (7th Edition):

Montel, Kenneth Keef. “Fluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamics.” 2015. Web. 16 Apr 2021.

Vancouver:

Montel KK. Fluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamics. [Internet] [Masters thesis]. Rice University; 2015. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/88237.

Council of Science Editors:

Montel KK. Fluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamics. [Masters Thesis]. Rice University; 2015. Available from: http://hdl.handle.net/1911/88237


Rice University

10. Buscher, Austin J. Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces.

Degree: MS, Mechanical Engineering, 2014, Rice University

 To address the computational challenges associated with contact between moving solid surfaces, such as those in cardiovascular fluid–structure interaction (FSI), parachute FSI, and flapping-wing aerodynamics,… (more)

Subjects/Keywords: space – time; toplogy-change; MAV; heart valve

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APA (6th Edition):

Buscher, A. J. (2014). Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/87723

Chicago Manual of Style (16th Edition):

Buscher, Austin J. “Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces.” 2014. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/87723.

MLA Handbook (7th Edition):

Buscher, Austin J. “Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces.” 2014. Web. 16 Apr 2021.

Vancouver:

Buscher AJ. Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces. [Internet] [Masters thesis]. Rice University; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/87723.

Council of Science Editors:

Buscher AJ. Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/87723


Rice University

11. Buscher, Austin J. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.

Degree: MS, Mechanical Engineering, 2014, Rice University

 To address the computational challenges associated with contact between moving solid surfaces, such as those in cardiovascular fluid–structure interaction (FSI), parachute FSI, and flapping-wing aerodynamics,… (more)

Subjects/Keywords: space – time; toplogy-change; MAV; heart valve

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APA (6th Edition):

Buscher, A. J. (2014). Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/103780

Chicago Manual of Style (16th Edition):

Buscher, Austin J. “Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.” 2014. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/103780.

MLA Handbook (7th Edition):

Buscher, Austin J. “Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.” 2014. Web. 16 Apr 2021.

Vancouver:

Buscher AJ. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. [Internet] [Masters thesis]. Rice University; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/103780.

Council of Science Editors:

Buscher AJ. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/103780


Rice University

12. Buscher, Austin J. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.

Degree: MS, Engineering, 2014, Rice University

 To address the computational challenges associated with contact between moving solid surfaces, such as those in cardiovascular fluid–structure interaction (FSI), parachute FSI, and flapping-wing aerodynamics,… (more)

Subjects/Keywords: space – time; toplogy-change; MAV; heart valve

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APA (6th Edition):

Buscher, A. J. (2014). Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/103866

Chicago Manual of Style (16th Edition):

Buscher, Austin J. “Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.” 2014. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/103866.

MLA Handbook (7th Edition):

Buscher, Austin J. “Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.” 2014. Web. 16 Apr 2021.

Vancouver:

Buscher AJ. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. [Internet] [Masters thesis]. Rice University; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/103866.

Council of Science Editors:

Buscher AJ. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/103866


Rice University

13. Fritze, Matt. Fluid-Structure Interaction Modeling of Parachutes with Disreefing and Modified Geometric Porosity and Separation Aerodynamics of a Cover Jettisoned to the Spacecraft Wake.

Degree: MS, Engineering, 2012, Rice University

 Fluid – structure interaction (FSI) modeling of spacecraft parachutes involves a number of computational challenges. The canopy complexity created by the hundreds of gaps and slits… (more)

Subjects/Keywords: Fluid-structure interaction; SSTFSI method; Parachute modeling; Special FSI methods; Impulse ejection; Parachute extraction; Temporal NURBS representation; Parachute disreefing; Space-time techniques; Ringsail parachutes; Contact; Parachutes

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APA (6th Edition):

Fritze, M. (2012). Fluid-Structure Interaction Modeling of Parachutes with Disreefing and Modified Geometric Porosity and Separation Aerodynamics of a Cover Jettisoned to the Spacecraft Wake. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/77320

Chicago Manual of Style (16th Edition):

Fritze, Matt. “Fluid-Structure Interaction Modeling of Parachutes with Disreefing and Modified Geometric Porosity and Separation Aerodynamics of a Cover Jettisoned to the Spacecraft Wake.” 2012. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/77320.

MLA Handbook (7th Edition):

Fritze, Matt. “Fluid-Structure Interaction Modeling of Parachutes with Disreefing and Modified Geometric Porosity and Separation Aerodynamics of a Cover Jettisoned to the Spacecraft Wake.” 2012. Web. 16 Apr 2021.

Vancouver:

Fritze M. Fluid-Structure Interaction Modeling of Parachutes with Disreefing and Modified Geometric Porosity and Separation Aerodynamics of a Cover Jettisoned to the Spacecraft Wake. [Internet] [Masters thesis]. Rice University; 2012. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/77320.

Council of Science Editors:

Fritze M. Fluid-Structure Interaction Modeling of Parachutes with Disreefing and Modified Geometric Porosity and Separation Aerodynamics of a Cover Jettisoned to the Spacecraft Wake. [Masters Thesis]. Rice University; 2012. Available from: http://hdl.handle.net/1911/77320


Rice University

14. Montes, Darren. Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers.

Degree: MS, Engineering, 2012, Rice University

 A new version of the Deforming-Spatial-Domain/Stabilized Space – Time (DSD/SST) formulation of incompressible flows has been introduced recently to have additional subgrid-scale representation features. This is… (more)

Subjects/Keywords: High Reynolds numbers; Airfoil geometries; Incompressible flows; DSD/SST formulation; DSD/SST-VMST method; Space-time VMS method

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APA (6th Edition):

Montes, D. (2012). Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/77322

Chicago Manual of Style (16th Edition):

Montes, Darren. “Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers.” 2012. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/77322.

MLA Handbook (7th Edition):

Montes, Darren. “Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers.” 2012. Web. 16 Apr 2021.

Vancouver:

Montes D. Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers. [Internet] [Masters thesis]. Rice University; 2012. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/77322.

Council of Science Editors:

Montes D. Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers. [Masters Thesis]. Rice University; 2012. Available from: http://hdl.handle.net/1911/77322


Rice University

15. Sathe, Sunil Vijay. Enhanced-discretization and solution techniques in flow simulations and parachute fluid-structure interactions.

Degree: PhD, Engineering, 2004, Rice University

 We present three innovative approaches for simulations of parachute fluid-structure interactions (FSI), which otherwise tend to be unstable because of extreme sensitivity of thin membrane… (more)

Subjects/Keywords: Mechanical engineering

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APA (6th Edition):

Sathe, S. V. (2004). Enhanced-discretization and solution techniques in flow simulations and parachute fluid-structure interactions. (Doctoral Dissertation). Rice University. Retrieved from http://hdl.handle.net/1911/18695

Chicago Manual of Style (16th Edition):

Sathe, Sunil Vijay. “Enhanced-discretization and solution techniques in flow simulations and parachute fluid-structure interactions.” 2004. Doctoral Dissertation, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/18695.

MLA Handbook (7th Edition):

Sathe, Sunil Vijay. “Enhanced-discretization and solution techniques in flow simulations and parachute fluid-structure interactions.” 2004. Web. 16 Apr 2021.

Vancouver:

Sathe SV. Enhanced-discretization and solution techniques in flow simulations and parachute fluid-structure interactions. [Internet] [Doctoral dissertation]. Rice University; 2004. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/18695.

Council of Science Editors:

Sathe SV. Enhanced-discretization and solution techniques in flow simulations and parachute fluid-structure interactions. [Doctoral Dissertation]. Rice University; 2004. Available from: http://hdl.handle.net/1911/18695


Rice University

16. Brummer, Tyler Matthew. A Comparative Study Based on Patient-Specific Fluid-Structure Interaction Modeling of Cerebral Aneurysms.

Degree: MS, Engineering, 2011, Rice University

 The Team for Advanced Flow Simulation and Modeling (T*AFSM) at Rice University has been developing techniques to address the computational challenges involved in fluid-structure interaction… (more)

Subjects/Keywords: Mechanical engineering; Materials science

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APA (6th Edition):

Brummer, T. M. (2011). A Comparative Study Based on Patient-Specific Fluid-Structure Interaction Modeling of Cerebral Aneurysms. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/64393

Chicago Manual of Style (16th Edition):

Brummer, Tyler Matthew. “A Comparative Study Based on Patient-Specific Fluid-Structure Interaction Modeling of Cerebral Aneurysms.” 2011. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/64393.

MLA Handbook (7th Edition):

Brummer, Tyler Matthew. “A Comparative Study Based on Patient-Specific Fluid-Structure Interaction Modeling of Cerebral Aneurysms.” 2011. Web. 16 Apr 2021.

Vancouver:

Brummer TM. A Comparative Study Based on Patient-Specific Fluid-Structure Interaction Modeling of Cerebral Aneurysms. [Internet] [Masters thesis]. Rice University; 2011. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/64393.

Council of Science Editors:

Brummer TM. A Comparative Study Based on Patient-Specific Fluid-Structure Interaction Modeling of Cerebral Aneurysms. [Masters Thesis]. Rice University; 2011. Available from: http://hdl.handle.net/1911/64393


Rice University

17. Curlett, Tracee Lee. Investigation of the Stabilization Parameters of the Stabilized Finite Element Formulations.

Degree: MS, Engineering, 2011, Rice University

 The Team for Advanced Flow Simulation and Modeling at Rice University specializes in finite element computation of complex problems, relying on stabilized formulations such as… (more)

Subjects/Keywords: Mechanical engineering; Materials science

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APA (6th Edition):

Curlett, T. L. (2011). Investigation of the Stabilization Parameters of the Stabilized Finite Element Formulations. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/64412

Chicago Manual of Style (16th Edition):

Curlett, Tracee Lee. “Investigation of the Stabilization Parameters of the Stabilized Finite Element Formulations.” 2011. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/64412.

MLA Handbook (7th Edition):

Curlett, Tracee Lee. “Investigation of the Stabilization Parameters of the Stabilized Finite Element Formulations.” 2011. Web. 16 Apr 2021.

Vancouver:

Curlett TL. Investigation of the Stabilization Parameters of the Stabilized Finite Element Formulations. [Internet] [Masters thesis]. Rice University; 2011. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/64412.

Council of Science Editors:

Curlett TL. Investigation of the Stabilization Parameters of the Stabilized Finite Element Formulations. [Masters Thesis]. Rice University; 2011. Available from: http://hdl.handle.net/1911/64412

18. Wood, Jeffre. A Penalty Method Approach to Experimental Data Coupling in the Sequentially Optimized Meshfree Approximation.

Degree: MS, Engineering, 2014, Rice University

 This thesis presents an overview of recent changes that have been made to the Sequentially Optimized Meshfree Approximation (SOMA) and provides a proof of concept… (more)

Subjects/Keywords: Meshfree; CFD; Data coupling; Data assimilation; Penalty method

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APA (6th Edition):

Wood, J. (2014). A Penalty Method Approach to Experimental Data Coupling in the Sequentially Optimized Meshfree Approximation. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/77570

Chicago Manual of Style (16th Edition):

Wood, Jeffre. “A Penalty Method Approach to Experimental Data Coupling in the Sequentially Optimized Meshfree Approximation.” 2014. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/77570.

MLA Handbook (7th Edition):

Wood, Jeffre. “A Penalty Method Approach to Experimental Data Coupling in the Sequentially Optimized Meshfree Approximation.” 2014. Web. 16 Apr 2021.

Vancouver:

Wood J. A Penalty Method Approach to Experimental Data Coupling in the Sequentially Optimized Meshfree Approximation. [Internet] [Masters thesis]. Rice University; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/77570.

Council of Science Editors:

Wood J. A Penalty Method Approach to Experimental Data Coupling in the Sequentially Optimized Meshfree Approximation. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/77570


Rice University

19. Keedy, Ryan M. Special methods for fluid-object interactions and space-time computations.

Degree: MS, Engineering, 2004, Rice University

 Simulations of complex fluid-object interactions problems in aeronautics demand robust and sophisticated numerical techniques. The proposed B-FOIST is an efficient library-lookup method for predicting the… (more)

Subjects/Keywords: Mechanical engineering

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APA (6th Edition):

Keedy, R. M. (2004). Special methods for fluid-object interactions and space-time computations. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/17695

Chicago Manual of Style (16th Edition):

Keedy, Ryan M. “Special methods for fluid-object interactions and space-time computations.” 2004. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/17695.

MLA Handbook (7th Edition):

Keedy, Ryan M. “Special methods for fluid-object interactions and space-time computations.” 2004. Web. 16 Apr 2021.

Vancouver:

Keedy RM. Special methods for fluid-object interactions and space-time computations. [Internet] [Masters thesis]. Rice University; 2004. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/17695.

Council of Science Editors:

Keedy RM. Special methods for fluid-object interactions and space-time computations. [Masters Thesis]. Rice University; 2004. Available from: http://hdl.handle.net/1911/17695


Rice University

20. Spielman, Timothy R. Space-Time FSI Modeling and Dynamical Analysis of Spacecraft Parachutes and Parachute Clusters.

Degree: MS, Engineering, 2011, Rice University

 The Team for Advanced Flow Simulation and Modeling (T*AFSM) at Rice University has been developing fluid-structure interaction (FSI) modeling techniques using Stabilized Space-Time FSI (SSTFSI)… (more)

Subjects/Keywords: Applied sciences; Aerospace engineering; Mechanical engineering

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APA (6th Edition):

Spielman, T. R. (2011). Space-Time FSI Modeling and Dynamical Analysis of Spacecraft Parachutes and Parachute Clusters. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/70449

Chicago Manual of Style (16th Edition):

Spielman, Timothy R. “Space-Time FSI Modeling and Dynamical Analysis of Spacecraft Parachutes and Parachute Clusters.” 2011. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/70449.

MLA Handbook (7th Edition):

Spielman, Timothy R. “Space-Time FSI Modeling and Dynamical Analysis of Spacecraft Parachutes and Parachute Clusters.” 2011. Web. 16 Apr 2021.

Vancouver:

Spielman TR. Space-Time FSI Modeling and Dynamical Analysis of Spacecraft Parachutes and Parachute Clusters. [Internet] [Masters thesis]. Rice University; 2011. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/70449.

Council of Science Editors:

Spielman TR. Space-Time FSI Modeling and Dynamical Analysis of Spacecraft Parachutes and Parachute Clusters. [Masters Thesis]. Rice University; 2011. Available from: http://hdl.handle.net/1911/70449


Rice University

21. Christopher, Jason Daniel. Computational aerodynamics modeling of the reefed stages of ringsail parachutes.

Degree: MS, Engineering, 2009, Rice University

 The Team for Advanced Flow Simulation and Modeling (T*AFSM) at Rice University has been using the Stabilized Space-Time Fluid-Structure Interaction (SSTFSI) they developed to model… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering

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APA (6th Edition):

Christopher, J. D. (2009). Computational aerodynamics modeling of the reefed stages of ringsail parachutes. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/61798

Chicago Manual of Style (16th Edition):

Christopher, Jason Daniel. “Computational aerodynamics modeling of the reefed stages of ringsail parachutes.” 2009. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/61798.

MLA Handbook (7th Edition):

Christopher, Jason Daniel. “Computational aerodynamics modeling of the reefed stages of ringsail parachutes.” 2009. Web. 16 Apr 2021.

Vancouver:

Christopher JD. Computational aerodynamics modeling of the reefed stages of ringsail parachutes. [Internet] [Masters thesis]. Rice University; 2009. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/61798.

Council of Science Editors:

Christopher JD. Computational aerodynamics modeling of the reefed stages of ringsail parachutes. [Masters Thesis]. Rice University; 2009. Available from: http://hdl.handle.net/1911/61798


Rice University

22. Henicke, Bradley J. Space – Time Finite Element Computation of the Aerodynamics of Flapping Wings.

Degree: MS, Engineering, 2011, Rice University

 The details of the aerodynamics of flapping flight continue to pose a considerable challenge to a complete understanding of flight. Advanced computational fluid mechanics technology… (more)

Subjects/Keywords: Applied sciences; Mechanical engineering

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APA (6th Edition):

Henicke, B. J. (2011). Space – Time Finite Element Computation of the Aerodynamics of Flapping Wings. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/70259

Chicago Manual of Style (16th Edition):

Henicke, Bradley J. “Space – Time Finite Element Computation of the Aerodynamics of Flapping Wings.” 2011. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/70259.

MLA Handbook (7th Edition):

Henicke, Bradley J. “Space – Time Finite Element Computation of the Aerodynamics of Flapping Wings.” 2011. Web. 16 Apr 2021.

Vancouver:

Henicke BJ. Space – Time Finite Element Computation of the Aerodynamics of Flapping Wings. [Internet] [Masters thesis]. Rice University; 2011. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/70259.

Council of Science Editors:

Henicke BJ. Space – Time Finite Element Computation of the Aerodynamics of Flapping Wings. [Masters Thesis]. Rice University; 2011. Available from: http://hdl.handle.net/1911/70259


Rice University

23. Moorman, Creighton J. Fluid-structure interaction modeling of the Orion spacecraft parachutes.

Degree: MS, Engineering, 2010, Rice University

 The Team for Advanced Flow Simulation and Modeling (T☆AFSM) at Rice University has been developing the Stabilized Space – Time Fluid – Structure Interaction core technologies in… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering

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APA (6th Edition):

Moorman, C. J. (2010). Fluid-structure interaction modeling of the Orion spacecraft parachutes. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/61979

Chicago Manual of Style (16th Edition):

Moorman, Creighton J. “Fluid-structure interaction modeling of the Orion spacecraft parachutes.” 2010. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/61979.

MLA Handbook (7th Edition):

Moorman, Creighton J. “Fluid-structure interaction modeling of the Orion spacecraft parachutes.” 2010. Web. 16 Apr 2021.

Vancouver:

Moorman CJ. Fluid-structure interaction modeling of the Orion spacecraft parachutes. [Internet] [Masters thesis]. Rice University; 2010. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/61979.

Council of Science Editors:

Moorman CJ. Fluid-structure interaction modeling of the Orion spacecraft parachutes. [Masters Thesis]. Rice University; 2010. Available from: http://hdl.handle.net/1911/61979


Rice University

24. Cragin, Timothy L. Stabilized space-time fluid-structure interaction techniques with the continuum element.

Degree: MS, Engineering, 2007, Rice University

 We present the methods used to add continuum element functionality to the structure side of our Fluid-Structure Interaction (FSI) solver. The FSI solver, already capable… (more)

Subjects/Keywords: Applied mechanics; Biomedical engineering; Mechanical engineering

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APA (6th Edition):

Cragin, T. L. (2007). Stabilized space-time fluid-structure interaction techniques with the continuum element. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/20497

Chicago Manual of Style (16th Edition):

Cragin, Timothy L. “Stabilized space-time fluid-structure interaction techniques with the continuum element.” 2007. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/20497.

MLA Handbook (7th Edition):

Cragin, Timothy L. “Stabilized space-time fluid-structure interaction techniques with the continuum element.” 2007. Web. 16 Apr 2021.

Vancouver:

Cragin TL. Stabilized space-time fluid-structure interaction techniques with the continuum element. [Internet] [Masters thesis]. Rice University; 2007. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/20497.

Council of Science Editors:

Cragin TL. Stabilized space-time fluid-structure interaction techniques with the continuum element. [Masters Thesis]. Rice University; 2007. Available from: http://hdl.handle.net/1911/20497


Rice University

25. Senga, Masayoshi. Improved SUPG formulations for compressible flows.

Degree: PhD, Engineering, 2006, Rice University

 Stabilization and shock-capturing parameters introduced recently for the StreamlineUpwind/Petrov-Galerkin (SUPG) formulation of compressible flows based on conservation variables are assessed in test computations with inviscid… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering

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APA (6th Edition):

Senga, M. (2006). Improved SUPG formulations for compressible flows. (Doctoral Dissertation). Rice University. Retrieved from http://hdl.handle.net/1911/18974

Chicago Manual of Style (16th Edition):

Senga, Masayoshi. “Improved SUPG formulations for compressible flows.” 2006. Doctoral Dissertation, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/18974.

MLA Handbook (7th Edition):

Senga, Masayoshi. “Improved SUPG formulations for compressible flows.” 2006. Web. 16 Apr 2021.

Vancouver:

Senga M. Improved SUPG formulations for compressible flows. [Internet] [Doctoral dissertation]. Rice University; 2006. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/18974.

Council of Science Editors:

Senga M. Improved SUPG formulations for compressible flows. [Doctoral Dissertation]. Rice University; 2006. Available from: http://hdl.handle.net/1911/18974


Rice University

26. Nanna, W. L. Bryan. Arterial fluid mechanics computations with the stabilized space-time fluid-structure interaction techniques.

Degree: MS, Engineering, 2007, Rice University

 The stabilized space-time fluid-structure interaction (SSTFSI) techniques developed by the Team for Advanced Flow Simulation and Modeling (T☆AFSM) are applied to the field of arterial… (more)

Subjects/Keywords: Applied mechanics; Biomedical engineering; Mechanical engineering

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APA (6th Edition):

Nanna, W. L. B. (2007). Arterial fluid mechanics computations with the stabilized space-time fluid-structure interaction techniques. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/20565

Chicago Manual of Style (16th Edition):

Nanna, W L Bryan. “Arterial fluid mechanics computations with the stabilized space-time fluid-structure interaction techniques.” 2007. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/20565.

MLA Handbook (7th Edition):

Nanna, W L Bryan. “Arterial fluid mechanics computations with the stabilized space-time fluid-structure interaction techniques.” 2007. Web. 16 Apr 2021.

Vancouver:

Nanna WLB. Arterial fluid mechanics computations with the stabilized space-time fluid-structure interaction techniques. [Internet] [Masters thesis]. Rice University; 2007. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/20565.

Council of Science Editors:

Nanna WLB. Arterial fluid mechanics computations with the stabilized space-time fluid-structure interaction techniques. [Masters Thesis]. Rice University; 2007. Available from: http://hdl.handle.net/1911/20565

27. Baskici, Gokhan. A Computational Analysis of Novel Non-circular Nozzles.

Degree: MS, Engineering, 2014, Rice University

 This thesis presents a computational analysis for determining the flow properties of novel non-circular nozzles. In last few decades, non-circular nozzles have been investigated intensively… (more)

Subjects/Keywords: Non-circular; Nozzle; Mass entrainment; Star CCM+; Jet flows; CFD

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APA (6th Edition):

Baskici, G. (2014). A Computational Analysis of Novel Non-circular Nozzles. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/76343

Chicago Manual of Style (16th Edition):

Baskici, Gokhan. “A Computational Analysis of Novel Non-circular Nozzles.” 2014. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/76343.

MLA Handbook (7th Edition):

Baskici, Gokhan. “A Computational Analysis of Novel Non-circular Nozzles.” 2014. Web. 16 Apr 2021.

Vancouver:

Baskici G. A Computational Analysis of Novel Non-circular Nozzles. [Internet] [Masters thesis]. Rice University; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/76343.

Council of Science Editors:

Baskici G. A Computational Analysis of Novel Non-circular Nozzles. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/76343

28. Montes, Darren. Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers.

Degree: MS, Engineering, 2013, Rice University

 A new version of the Deforming-Spatial-Domain/Stabilized Space – Time (DSD/SST) formulation of incompressible flows has been introduced recently to have additional subgrid-scale representation features. This is… (more)

Subjects/Keywords: Incompressible flows; DSD/SST formulation; DSD/SST-VMST method; Space-time VMS method; High Reynolds numbers; Airfoil geometries

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APA (6th Edition):

Montes, D. (2013). Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/71298

Chicago Manual of Style (16th Edition):

Montes, Darren. “Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers.” 2013. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/71298.

MLA Handbook (7th Edition):

Montes, Darren. “Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers.” 2013. Web. 16 Apr 2021.

Vancouver:

Montes D. Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers. [Internet] [Masters thesis]. Rice University; 2013. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/71298.

Council of Science Editors:

Montes D. Space – Time VMS Computation of Incompressible Flows With Airfoil Geometries and High Reynolds Numbers. [Masters Thesis]. Rice University; 2013. Available from: http://hdl.handle.net/1911/71298

29. Boswell, Cody W. Fluid-Structure Interaction Modeling of the Reefed Stages of the Orion Spacecraft Main Parachutes.

Degree: MS, Engineering, 2014, Rice University

 Spacecraft parachutes are typically used in multiple stages, starting with a "reefed" stage where a cable along the parachute skirt constrains the diameter to be… (more)

Subjects/Keywords: Fluid-structure interaction; Parachutes; Parachute clusters; Disreefing; Space-time techniques

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APA (6th Edition):

Boswell, C. W. (2014). Fluid-Structure Interaction Modeling of the Reefed Stages of the Orion Spacecraft Main Parachutes. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/76363

Chicago Manual of Style (16th Edition):

Boswell, Cody W. “Fluid-Structure Interaction Modeling of the Reefed Stages of the Orion Spacecraft Main Parachutes.” 2014. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/76363.

MLA Handbook (7th Edition):

Boswell, Cody W. “Fluid-Structure Interaction Modeling of the Reefed Stages of the Orion Spacecraft Main Parachutes.” 2014. Web. 16 Apr 2021.

Vancouver:

Boswell CW. Fluid-Structure Interaction Modeling of the Reefed Stages of the Orion Spacecraft Main Parachutes. [Internet] [Masters thesis]. Rice University; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/76363.

Council of Science Editors:

Boswell CW. Fluid-Structure Interaction Modeling of the Reefed Stages of the Orion Spacecraft Main Parachutes. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/76363

30. Kolesar, Ryan. Fluid–Structure Interaction Modeling of the Orion Spacecraft Drogue Parachutes.

Degree: MS, Engineering, 2014, Rice University

 At higher altitudes, prior to the deployment of the main parachutes, the Orion spacecraft descent to Earth will rely on deceleration by drogue parachutes. These… (more)

Subjects/Keywords: Fluid-structure interaction; Spacecraft parachutes

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APA (6th Edition):

Kolesar, R. (2014). Fluid–Structure Interaction Modeling of the Orion Spacecraft Drogue Parachutes. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/77193

Chicago Manual of Style (16th Edition):

Kolesar, Ryan. “Fluid–Structure Interaction Modeling of the Orion Spacecraft Drogue Parachutes.” 2014. Masters Thesis, Rice University. Accessed April 16, 2021. http://hdl.handle.net/1911/77193.

MLA Handbook (7th Edition):

Kolesar, Ryan. “Fluid–Structure Interaction Modeling of the Orion Spacecraft Drogue Parachutes.” 2014. Web. 16 Apr 2021.

Vancouver:

Kolesar R. Fluid–Structure Interaction Modeling of the Orion Spacecraft Drogue Parachutes. [Internet] [Masters thesis]. Rice University; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/1911/77193.

Council of Science Editors:

Kolesar R. Fluid–Structure Interaction Modeling of the Orion Spacecraft Drogue Parachutes. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/77193

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