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You searched for +publisher:"Georgia Tech" +contributor:("Smith, Marilyn J."). Showing records 1 – 12 of 12 total matches.

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Georgia Tech

1. Cook, James Richard. Development of an aeroelastic methodology for surface morphing rotors.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 A Computational Fluid Dynamics/Computational Fluid Dynamics (CFD/CSD) coupling interface was developed to obtain aeroelastic solutions of a morphing rotor. The methodology was implemented in Fully… (more)

Subjects/Keywords: Aeroelasticity; Test facility; Recirculation; Turbulence model; Hrles; Rotorcraft; Rotor; CFD/CSD; Coupling; CFD; Camber; Actuation; Morphing; Rotors; Aeroelasticity; Structural dynamics; Computational fluid dynamics

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APA (6th Edition):

Cook, J. R. (2014). Development of an aeroelastic methodology for surface morphing rotors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51807

Chicago Manual of Style (16th Edition):

Cook, James Richard. “Development of an aeroelastic methodology for surface morphing rotors.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/51807.

MLA Handbook (7th Edition):

Cook, James Richard. “Development of an aeroelastic methodology for surface morphing rotors.” 2014. Web. 17 Oct 2019.

Vancouver:

Cook JR. Development of an aeroelastic methodology for surface morphing rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/51807.

Council of Science Editors:

Cook JR. Development of an aeroelastic methodology for surface morphing rotors. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51807


Georgia Tech

2. Kong, Yong Boon. Development of a finite state coaxial rotor dynamic inflow model.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Accurate modeling of rotor inflow dynamics in flight simulations is crucial for rotorcraft performance and handling qualities evaluations. Both Pitt-Peters and Peters-He inflow models are… (more)

Subjects/Keywords: Coaxial rotor; Dynamic inflow model; System identification

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APA (6th Edition):

Kong, Y. B. (2018). Development of a finite state coaxial rotor dynamic inflow model. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60258

Chicago Manual of Style (16th Edition):

Kong, Yong Boon. “Development of a finite state coaxial rotor dynamic inflow model.” 2018. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/60258.

MLA Handbook (7th Edition):

Kong, Yong Boon. “Development of a finite state coaxial rotor dynamic inflow model.” 2018. Web. 17 Oct 2019.

Vancouver:

Kong YB. Development of a finite state coaxial rotor dynamic inflow model. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/60258.

Council of Science Editors:

Kong YB. Development of a finite state coaxial rotor dynamic inflow model. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/60258


Georgia Tech

3. Clay, Matthew Paul. Strained turbulence and low-diffusivity turbulent mixing using high performance computing.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 In this thesis, turbulent flows are studied using the method of direct numerical simulation (DNS), whereby exact governing equations are computed without modeling. Beginning with… (more)

Subjects/Keywords: Turbulence; DNS; High performance computing

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APA (6th Edition):

Clay, M. P. (2017). Strained turbulence and low-diffusivity turbulent mixing using high performance computing. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60184

Chicago Manual of Style (16th Edition):

Clay, Matthew Paul. “Strained turbulence and low-diffusivity turbulent mixing using high performance computing.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/60184.

MLA Handbook (7th Edition):

Clay, Matthew Paul. “Strained turbulence and low-diffusivity turbulent mixing using high performance computing.” 2017. Web. 17 Oct 2019.

Vancouver:

Clay MP. Strained turbulence and low-diffusivity turbulent mixing using high performance computing. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/60184.

Council of Science Editors:

Clay MP. Strained turbulence and low-diffusivity turbulent mixing using high performance computing. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/60184


Georgia Tech

4. Bopp, Matthew Scott. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 The landing of the Mars Science Laboratory (MSL) in 2012 demonstrated the limits of supersonic planetary entry technology through the use of a disk-gap-band parachute… (more)

Subjects/Keywords: CFD; FSI; Cartesian; EDL; Aerodynamic decelerator; Fluid dynamics; Structural dynamics; Coupling; C++; Immersed boundary method

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APA (6th Edition):

Bopp, M. S. (2017). A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59257

Chicago Manual of Style (16th Edition):

Bopp, Matthew Scott. “A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/59257.

MLA Handbook (7th Edition):

Bopp, Matthew Scott. “A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.” 2017. Web. 17 Oct 2019.

Vancouver:

Bopp MS. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/59257.

Council of Science Editors:

Bopp MS. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59257


Georgia Tech

5. Jacobson, Kevin Edward. Adjoint-based Aeroelastic Optimization with High-fidelity Time-accurate Analysis.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 A methodology is proposed for adjoint-based sensitivities of steady and time-accurate aeroelastic analysis with high-fidelity models based on computational fluid dynamics and structural finite element… (more)

Subjects/Keywords: Aeroelasticity; Flutter; Gust response; Optimization; Adjoint-based sensitivities

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APA (6th Edition):

Jacobson, K. E. (2018). Adjoint-based Aeroelastic Optimization with High-fidelity Time-accurate Analysis. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61189

Chicago Manual of Style (16th Edition):

Jacobson, Kevin Edward. “Adjoint-based Aeroelastic Optimization with High-fidelity Time-accurate Analysis.” 2018. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/61189.

MLA Handbook (7th Edition):

Jacobson, Kevin Edward. “Adjoint-based Aeroelastic Optimization with High-fidelity Time-accurate Analysis.” 2018. Web. 17 Oct 2019.

Vancouver:

Jacobson KE. Adjoint-based Aeroelastic Optimization with High-fidelity Time-accurate Analysis. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/61189.

Council of Science Editors:

Jacobson KE. Adjoint-based Aeroelastic Optimization with High-fidelity Time-accurate Analysis. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/61189


Georgia Tech

6. Patterson, Michael Dobson. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 The maturation of electric propulsion technologies presents intriguing new degrees of freedom for aircraft designers including the ability to distribute many small propellers upstream of… (more)

Subjects/Keywords: distributed electric propulsion; high-lift propellers; aircraft design; aircraft performance; design method; propeller design

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APA (6th Edition):

Patterson, M. D. (2016). Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55569

Chicago Manual of Style (16th Edition):

Patterson, Michael Dobson. “Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/55569.

MLA Handbook (7th Edition):

Patterson, Michael Dobson. “Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.” 2016. Web. 17 Oct 2019.

Vancouver:

Patterson MD. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/55569.

Council of Science Editors:

Patterson MD. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55569

7. Reveles, Nicolas. Advanced methods for dynamic aeroelastic analysis of rotors.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Simulations play an integral role in the understanding and development of rotor- craft aeromechanics. Computational Fluid Dynamics coupled with Computational Structural Dynamics (CFD/CSD) offers an… (more)

Subjects/Keywords: Aeroelasticity; Tight coupling; Loose coupling; CFD/CSD; Hybrid; Free-wake; URANS; Trim; Aeroelasticity; Rotors; Computational fluid dynamics; Structural dynamics

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APA (6th Edition):

Reveles, N. (2014). Advanced methods for dynamic aeroelastic analysis of rotors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51904

Chicago Manual of Style (16th Edition):

Reveles, Nicolas. “Advanced methods for dynamic aeroelastic analysis of rotors.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/51904.

MLA Handbook (7th Edition):

Reveles, Nicolas. “Advanced methods for dynamic aeroelastic analysis of rotors.” 2014. Web. 17 Oct 2019.

Vancouver:

Reveles N. Advanced methods for dynamic aeroelastic analysis of rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/51904.

Council of Science Editors:

Reveles N. Advanced methods for dynamic aeroelastic analysis of rotors. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51904

8. Hodara, Joachim. Hybrid RANS-LES closure for separated flows in the transitional regime.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 The aerodynamics of modern rotorcraft is highly complex and has proven to be an arduous challenge for computational fluid dynamics (CFD). Flow features such as… (more)

Subjects/Keywords: CFD; Turbulence modeling; Transition to turbulence; Numerical methods; Reverse flow; Aerodynamics; Hybrid RANS-LES

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APA (6th Edition):

Hodara, J. (2016). Hybrid RANS-LES closure for separated flows in the transitional regime. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54995

Chicago Manual of Style (16th Edition):

Hodara, Joachim. “Hybrid RANS-LES closure for separated flows in the transitional regime.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/54995.

MLA Handbook (7th Edition):

Hodara, Joachim. “Hybrid RANS-LES closure for separated flows in the transitional regime.” 2016. Web. 17 Oct 2019.

Vancouver:

Hodara J. Hybrid RANS-LES closure for separated flows in the transitional regime. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/54995.

Council of Science Editors:

Hodara J. Hybrid RANS-LES closure for separated flows in the transitional regime. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/54995

9. Heo, Seun Do. Parallel computation algorithms for multibody dynamics simulations.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 Flexible multibody dynamics simulations have been performed sequentially on a single processor because the problem sizes for the simulations were not large. How-ever, advanced designs… (more)

Subjects/Keywords: Flexible multibody dynamics; Finite element method; Parallel computing; Domain decomposition; Lagrange multiplier; Kinematic constraints

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APA (6th Edition):

Heo, S. D. (2017). Parallel computation algorithms for multibody dynamics simulations. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/58659

Chicago Manual of Style (16th Edition):

Heo, Seun Do. “Parallel computation algorithms for multibody dynamics simulations.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/58659.

MLA Handbook (7th Edition):

Heo, Seun Do. “Parallel computation algorithms for multibody dynamics simulations.” 2017. Web. 17 Oct 2019.

Vancouver:

Heo SD. Parallel computation algorithms for multibody dynamics simulations. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/58659.

Council of Science Editors:

Heo SD. Parallel computation algorithms for multibody dynamics simulations. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/58659

10. Woo, Tak Kwong. Transitory control of separated shear layer using impulsive jet actuation.

Degree: PhD, Mechanical Engineering, 2014, Georgia Tech

 The dynamics of controlled transitory 2- and 3-D attachment of the separated flow over a 2-D airfoil model are investigated in wind tunnel experiments. Pulsed… (more)

Subjects/Keywords: Aerodynamics; Fluid mechanics; Flow control; Wind tunnel; Combustion actuators

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APA (6th Edition):

Woo, T. K. (2014). Transitory control of separated shear layer using impulsive jet actuation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/52980

Chicago Manual of Style (16th Edition):

Woo, Tak Kwong. “Transitory control of separated shear layer using impulsive jet actuation.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/52980.

MLA Handbook (7th Edition):

Woo, Tak Kwong. “Transitory control of separated shear layer using impulsive jet actuation.” 2014. Web. 17 Oct 2019.

Vancouver:

Woo TK. Transitory control of separated shear layer using impulsive jet actuation. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/52980.

Council of Science Editors:

Woo TK. Transitory control of separated shear layer using impulsive jet actuation. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/52980

11. Quon, Eliot. Data transfer strategies for overset and hybrid computational methods.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Modern computational science permits the accurate solution of nonlinear partial differential equations (PDEs) on overlapping computational domains, known as an overset approach. The complex grid… (more)

Subjects/Keywords: Computational fluid dynamics; Overset grids; Hybrid methods; Data transfer; Radial basis function interpolation

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APA (6th Edition):

Quon, E. (2014). Data transfer strategies for overset and hybrid computational methods. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53024

Chicago Manual of Style (16th Edition):

Quon, Eliot. “Data transfer strategies for overset and hybrid computational methods.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/53024.

MLA Handbook (7th Edition):

Quon, Eliot. “Data transfer strategies for overset and hybrid computational methods.” 2014. Web. 17 Oct 2019.

Vancouver:

Quon E. Data transfer strategies for overset and hybrid computational methods. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/53024.

Council of Science Editors:

Quon E. Data transfer strategies for overset and hybrid computational methods. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53024

12. Sánchez Rocha, Martín. Wall-models for large eddy simulation based on a generic additive-filter formulation.

Degree: PhD, Aerospace Engineering, 2008, Georgia Tech

 In this work, the mathematical implications of merging two different turbulence modeling approaches are addressed by deriving the exact hybrid RANS/LES Navier-Stokes equations. These equations… (more)

Subjects/Keywords: Near-wall models for LES; Turbulence modeling; Derivation of governing equations; Compressible TLS formulation; Hybrid RANS/LES governing equations; Eddies; Computer simulation; Turbulence; Mathematical models

…days at Georgia Tech, when my inexperience made me felt incapable to succeed at CCL. Thanks… …dissertation reading committee. I would like to express my gratitude to all the Georgia Tech… 

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APA (6th Edition):

Sánchez Rocha, M. (2008). Wall-models for large eddy simulation based on a generic additive-filter formulation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28086

Chicago Manual of Style (16th Edition):

Sánchez Rocha, Martín. “Wall-models for large eddy simulation based on a generic additive-filter formulation.” 2008. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/28086.

MLA Handbook (7th Edition):

Sánchez Rocha, Martín. “Wall-models for large eddy simulation based on a generic additive-filter formulation.” 2008. Web. 17 Oct 2019.

Vancouver:

Sánchez Rocha M. Wall-models for large eddy simulation based on a generic additive-filter formulation. [Internet] [Doctoral dissertation]. Georgia Tech; 2008. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/28086.

Council of Science Editors:

Sánchez Rocha M. Wall-models for large eddy simulation based on a generic additive-filter formulation. [Doctoral Dissertation]. Georgia Tech; 2008. Available from: http://hdl.handle.net/1853/28086

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