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You searched for +publisher:"Georgia Tech" +contributor:("Smith, Marilyn"). Showing records 1 – 30 of 33 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 July 24, 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. 24 Jul 2019.

Vancouver:

Cook JR. Development of an aeroelastic methodology for surface morphing rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Jul 24]. 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. Prosser, Daniel T. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Interactions between the aerodynamics and dynamics of bluff bodies are important in many engineering applications, including suspension bridges, tall buildings, oil platforms, wind turbine towers,… (more)

Subjects/Keywords: Computational fluid dynamics; Reduced-order modeling; Tethered loads; Rotorcraft; Bluff bodies

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APA (6th Edition):

Prosser, D. T. (2015). Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53899

Chicago Manual of Style (16th Edition):

Prosser, Daniel T. “Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.” 2015. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/53899.

MLA Handbook (7th Edition):

Prosser, Daniel T. “Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.” 2015. Web. 24 Jul 2019.

Vancouver:

Prosser DT. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/53899.

Council of Science Editors:

Prosser DT. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53899


Georgia Tech

3. Lambert, Thomas John. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.

Degree: PhD, Mechanical Engineering, 2016, Georgia Tech

 This research focuses on the unsteady flow mechanisms of using aerodynamic flow control at the aft end flow boundary of a bluff body to modify… (more)

Subjects/Keywords: Flow control; Fluid mechanics; Aerodynamics

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APA (6th Edition):

Lambert, T. J. (2016). Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56356

Chicago Manual of Style (16th Edition):

Lambert, Thomas John. “Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.” 2016. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/56356.

MLA Handbook (7th Edition):

Lambert, Thomas John. “Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.” 2016. Web. 24 Jul 2019.

Vancouver:

Lambert TJ. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/56356.

Council of Science Editors:

Lambert TJ. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56356


Georgia Tech

4. Abras, Jennifer N. Enhancement of aeroelastic rotor airload prediction methods.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 The accurate prediction of rotor air loads is a current topic of interest in the rotorcraft community. The complex nature of this loading makes this… (more)

Subjects/Keywords: Coupling; CFD-CSD; Comprehensive code; Free wake; CFD; Rotor; Aeroelasticity; Rotors (Helicopters) Aerodynamics; Structural dynamics; Prediction theory

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APA (6th Edition):

Abras, J. N. (2009). Enhancement of aeroelastic rotor airload prediction methods. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28182

Chicago Manual of Style (16th Edition):

Abras, Jennifer N. “Enhancement of aeroelastic rotor airload prediction methods.” 2009. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/28182.

MLA Handbook (7th Edition):

Abras, Jennifer N. “Enhancement of aeroelastic rotor airload prediction methods.” 2009. Web. 24 Jul 2019.

Vancouver:

Abras JN. Enhancement of aeroelastic rotor airload prediction methods. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/28182.

Council of Science Editors:

Abras JN. Enhancement of aeroelastic rotor airload prediction methods. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28182


Georgia Tech

5. Lynch, Charles Eric. Advanced CFD methods for wind turbine analysis.

Degree: PhD, Aerospace Engineering, 2011, Georgia Tech

 Horizontal-axis wind turbines operate in a complex, inherently unsteady aerodynamic environment. The flow over the blades is dominated by 3-D effects, particularly during stall, which… (more)

Subjects/Keywords: Unstructured; Wind turbine; Hybrid RANS-LES; Actuator; Aeroelasticity; CFD; Wind turbines; Computational fluid dynamics

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APA (6th Edition):

Lynch, C. E. (2011). Advanced CFD methods for wind turbine analysis. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/39491

Chicago Manual of Style (16th Edition):

Lynch, Charles Eric. “Advanced CFD methods for wind turbine analysis.” 2011. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/39491.

MLA Handbook (7th Edition):

Lynch, Charles Eric. “Advanced CFD methods for wind turbine analysis.” 2011. Web. 24 Jul 2019.

Vancouver:

Lynch CE. Advanced CFD methods for wind turbine analysis. [Internet] [Doctoral dissertation]. Georgia Tech; 2011. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/39491.

Council of Science Editors:

Lynch CE. Advanced CFD methods for wind turbine analysis. [Doctoral Dissertation]. Georgia Tech; 2011. Available from: http://hdl.handle.net/1853/39491


Georgia Tech

6. Zaki, Afifa Adel. Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Dynamic stall deeply affects the response of helicopter rotor blades, making its modeling accuracy very important. Two commonly used dynamic stall models were implemented in… (more)

Subjects/Keywords: CFD/CSD coupling; Rotorcraft stability analysis; Rotors (Helicopters); Rotors (Helicopters) Aerodynamics; Aerodynamics

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APA (6th Edition):

Zaki, A. A. (2012). Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/43579

Chicago Manual of Style (16th Edition):

Zaki, Afifa Adel. “Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis.” 2012. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/43579.

MLA Handbook (7th Edition):

Zaki, Afifa Adel. “Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis.” 2012. Web. 24 Jul 2019.

Vancouver:

Zaki AA. Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/43579.

Council of Science Editors:

Zaki AA. Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/43579


Georgia Tech

7. DeSalvo, Michael E. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 The mechanisms of aerodynamic flow control over lifting surfaces in which global, large-scale changes in aerodynamic characteristics are engendered by momentum injection across the flow… (more)

Subjects/Keywords: Flow control; Aerodynamics

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APA (6th Edition):

DeSalvo, M. E. (2015). Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55498

Chicago Manual of Style (16th Edition):

DeSalvo, Michael E. “Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.” 2015. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/55498.

MLA Handbook (7th Edition):

DeSalvo, Michael E. “Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.” 2015. Web. 24 Jul 2019.

Vancouver:

DeSalvo ME. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/55498.

Council of Science Editors:

DeSalvo ME. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/55498


Georgia Tech

8. Kearney, John M. Aerodynamic control using distributed active bleed.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 A novel approach for controlling the global aerodynamic loads on lifting surfaces using regulated distributed active bleed that is driven by pressure differences across the… (more)

Subjects/Keywords: Fluid mechanics; Flow control

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APA (6th Edition):

Kearney, J. M. (2015). Aerodynamic control using distributed active bleed. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55515

Chicago Manual of Style (16th Edition):

Kearney, John M. “Aerodynamic control using distributed active bleed.” 2015. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/55515.

MLA Handbook (7th Edition):

Kearney, John M. “Aerodynamic control using distributed active bleed.” 2015. Web. 24 Jul 2019.

Vancouver:

Kearney JM. Aerodynamic control using distributed active bleed. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/55515.

Council of Science Editors:

Kearney JM. Aerodynamic control using distributed active bleed. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/55515


Georgia Tech

9. 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 July 24, 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. 24 Jul 2019.

Vancouver:

Kong YB. Development of a finite state coaxial rotor dynamic inflow model. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Jul 24]. 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

10. 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 July 24, 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. 24 Jul 2019.

Vancouver:

Clay MP. Strained turbulence and low-diffusivity turbulent mixing using high performance computing. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Jul 24]. 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

11. Rancourt, David. Method for the flight path optimization of the electric-powered reconfigurable rotor (EPR2) VTOL concept.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Vertical Takeoff and Landing aircraft (VTOL) have been essential to our society since their introduction in the mid-1940s.Today, helicopters are extensively used for military and… (more)

Subjects/Keywords: VTOL; Electric aircraft; Helicopters; Wake interaction; Tethers; EPR2 VTOL concept; Reconfigurable rotor

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APA (6th Edition):

Rancourt, D. (2016). Method for the flight path optimization of the electric-powered reconfigurable rotor (EPR2) VTOL concept. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56322

Chicago Manual of Style (16th Edition):

Rancourt, David. “Method for the flight path optimization of the electric-powered reconfigurable rotor (EPR2) VTOL concept.” 2016. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/56322.

MLA Handbook (7th Edition):

Rancourt, David. “Method for the flight path optimization of the electric-powered reconfigurable rotor (EPR2) VTOL concept.” 2016. Web. 24 Jul 2019.

Vancouver:

Rancourt D. Method for the flight path optimization of the electric-powered reconfigurable rotor (EPR2) VTOL concept. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/56322.

Council of Science Editors:

Rancourt D. Method for the flight path optimization of the electric-powered reconfigurable rotor (EPR2) VTOL concept. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56322


Georgia Tech

12. 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 July 24, 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. 24 Jul 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 Jul 24]. 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

13. 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 July 24, 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. 24 Jul 2019.

Vancouver:

Jacobson KE. Adjoint-based Aeroelastic Optimization with High-fidelity Time-accurate Analysis. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Jul 24]. 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

14. 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 July 24, 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. 24 Jul 2019.

Vancouver:

Patterson MD. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Jul 24]. 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

15. 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 July 24, 2019. http://hdl.handle.net/1853/51904.

MLA Handbook (7th Edition):

Reveles, Nicolas. “Advanced methods for dynamic aeroelastic analysis of rotors.” 2014. Web. 24 Jul 2019.

Vancouver:

Reveles N. Advanced methods for dynamic aeroelastic analysis of rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Jul 24]. 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

16. Shenoy, Rajiv. Overset adaptive strategies for complex rotating systems.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 The resolution of the complex physics of rotating configurations is critical for any engineering analysis that requires multiple frames of reference. Two well-known applications are… (more)

Subjects/Keywords: Unsteady; Chimera; Data transfer; Rotorcraft; Wind turbines; Accurate interpolation; Grid adaptation; Time-dependent; Accuracy verification; Localization; Robust search; Rotor-fuselage interaction; Rotor hub; Aeroelasticity; Navier-Stokes equations; Wakes (Aerodynamics); Boundary layer

…x5D; and the Georgia Tech hybrid RANS-LES (GTHRLES) [84] models were… 

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APA (6th Edition):

Shenoy, R. (2014). Overset adaptive strategies for complex rotating systems. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51796

Chicago Manual of Style (16th Edition):

Shenoy, Rajiv. “Overset adaptive strategies for complex rotating systems.” 2014. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/51796.

MLA Handbook (7th Edition):

Shenoy, Rajiv. “Overset adaptive strategies for complex rotating systems.” 2014. Web. 24 Jul 2019.

Vancouver:

Shenoy R. Overset adaptive strategies for complex rotating systems. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/51796.

Council of Science Editors:

Shenoy R. Overset adaptive strategies for complex rotating systems. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51796

17. Gryngarten, Leandro Damian. Multi-phase flows using discontinuous Galerkin methods.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 This thesis is concerned with the development of numerical techniques to simulate compressible multi-phase flows, in particular a high-accuracy numerical approach with mesh adaptivity. The… (more)

Subjects/Keywords: Computational fluid dynamics; Multi-fluid; Multi-phase; Discontinuous Galerking; Fluid dynamics; Numerical analysis; Navier-Stokes equations Numerical solutions; Simulation methods; Mathematical models

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APA (6th Edition):

Gryngarten, L. D. (2012). Multi-phase flows using discontinuous Galerkin methods. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/45824

Chicago Manual of Style (16th Edition):

Gryngarten, Leandro Damian. “Multi-phase flows using discontinuous Galerkin methods.” 2012. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/45824.

MLA Handbook (7th Edition):

Gryngarten, Leandro Damian. “Multi-phase flows using discontinuous Galerkin methods.” 2012. Web. 24 Jul 2019.

Vancouver:

Gryngarten LD. Multi-phase flows using discontinuous Galerkin methods. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/45824.

Council of Science Editors:

Gryngarten LD. Multi-phase flows using discontinuous Galerkin methods. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/45824

18. Liggett, Nicholas Dwayne. Numerical investigation of static and dynamic stall of single and flapped airfoils.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Separated flows about single and multi-element airfoils are featured in many scenarios of practical interest, including: stall of fixed wing aircraft, dynamic stall of rotorcraft… (more)

Subjects/Keywords: Separated flows; HRLES; LES; RANS; CFD; Stall; Separation; Turbulence; Numerical convergence; Oscillating airfoil; Multi-element airfoil; Stalling (Aerodynamics); Aerodynamics; Aerofoils

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APA (6th Edition):

Liggett, N. D. (2012). Numerical investigation of static and dynamic stall of single and flapped airfoils. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/45834

Chicago Manual of Style (16th Edition):

Liggett, Nicholas Dwayne. “Numerical investigation of static and dynamic stall of single and flapped airfoils.” 2012. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/45834.

MLA Handbook (7th Edition):

Liggett, Nicholas Dwayne. “Numerical investigation of static and dynamic stall of single and flapped airfoils.” 2012. Web. 24 Jul 2019.

Vancouver:

Liggett ND. Numerical investigation of static and dynamic stall of single and flapped airfoils. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/45834.

Council of Science Editors:

Liggett ND. Numerical investigation of static and dynamic stall of single and flapped airfoils. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/45834

19. Chierichetti, Maria. Combined analytical and experimental approaches to dynamic component stress prediction.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 In modern times, the ability to investigate the aeroelastic behavior of dynamic components on rotorcraft has become essential for the prediction of their useful fatigue… (more)

Subjects/Keywords: Plate; Beam; Rotorcraft; Load identification; Response identification; Aeroelasticity; Fatigue testing; Algorithms; Dynamics

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APA (6th Edition):

Chierichetti, M. (2012). Combined analytical and experimental approaches to dynamic component stress prediction. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/44850

Chicago Manual of Style (16th Edition):

Chierichetti, Maria. “Combined analytical and experimental approaches to dynamic component stress prediction.” 2012. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/44850.

MLA Handbook (7th Edition):

Chierichetti, Maria. “Combined analytical and experimental approaches to dynamic component stress prediction.” 2012. Web. 24 Jul 2019.

Vancouver:

Chierichetti M. Combined analytical and experimental approaches to dynamic component stress prediction. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/44850.

Council of Science Editors:

Chierichetti M. Combined analytical and experimental approaches to dynamic component stress prediction. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/44850

20. Li, Wei-En. Enhancement of roll maneuverability using post-reversal design.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 This dissertation consists of three main parts. The first part is to discuss aileron reversal problem for a typical section with linear aerodynamic and structural… (more)

Subjects/Keywords: Aeroelasticity; DYMORE; XFOIL; Aeroelastic nonlinearity; Aileron reversal; Roll maneuverability; Ailerons; Ailerons Performance; Aerodynamics; Rolling (Aerodynamics); Trailing edge flaps

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APA (6th Edition):

Li, W. (2009). Enhancement of roll maneuverability using post-reversal design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/29602

Chicago Manual of Style (16th Edition):

Li, Wei-En. “Enhancement of roll maneuverability using post-reversal design.” 2009. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/29602.

MLA Handbook (7th Edition):

Li, Wei-En. “Enhancement of roll maneuverability using post-reversal design.” 2009. Web. 24 Jul 2019.

Vancouver:

Li W. Enhancement of roll maneuverability using post-reversal design. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/29602.

Council of Science Editors:

Li W. Enhancement of roll maneuverability using post-reversal design. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/29602

21. 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 July 24, 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. 24 Jul 2019.

Vancouver:

Hodara J. Hybrid RANS-LES closure for separated flows in the transitional regime. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Jul 24]. 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

22. 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 July 24, 2019. http://hdl.handle.net/1853/58659.

MLA Handbook (7th Edition):

Heo, Seun Do. “Parallel computation algorithms for multibody dynamics simulations.” 2017. Web. 24 Jul 2019.

Vancouver:

Heo SD. Parallel computation algorithms for multibody dynamics simulations. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Jul 24]. 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

23. 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 July 24, 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. 24 Jul 2019.

Vancouver:

Woo TK. Transitory control of separated shear layer using impulsive jet actuation. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Jul 24]. 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

24. 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 July 24, 2019. http://hdl.handle.net/1853/53024.

MLA Handbook (7th Edition):

Quon, Eliot. “Data transfer strategies for overset and hybrid computational methods.” 2014. Web. 24 Jul 2019.

Vancouver:

Quon E. Data transfer strategies for overset and hybrid computational methods. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Jul 24]. 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

25. 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 July 24, 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. 24 Jul 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 Jul 24]. 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

26. Pate, David Joyner. A surface vorticity method for wake–body interactions.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 The objective of this dissertation research is to develop a surface vorticity method for simulating high Reynolds number incompressible aerodynamic flows with strong unsteady interactions… (more)

Subjects/Keywords: Boundary element method; Vortex sheet; Surface vorticity; Aerodynamics; Vortex methods; Treecode

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APA (6th Edition):

Pate, D. J. (2017). A surface vorticity method for wake–body interactions. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/58265

Chicago Manual of Style (16th Edition):

Pate, David Joyner. “A surface vorticity method for wake–body interactions.” 2017. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/58265.

MLA Handbook (7th Edition):

Pate, David Joyner. “A surface vorticity method for wake–body interactions.” 2017. Web. 24 Jul 2019.

Vancouver:

Pate DJ. A surface vorticity method for wake–body interactions. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/58265.

Council of Science Editors:

Pate DJ. A surface vorticity method for wake–body interactions. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/58265


Georgia Tech

27. Lee, Jae-doo. Development of an Efficient Viscous Approach in a Cartesian Grid Framework and Application to Rotor-Fuselage Interaction.

Degree: PhD, Aerospace Engineering, 2006, Georgia Tech

 Despite the high cost of memory and CPU time required to resolve the boundary layer, a viscous unstructured grid solver has many advantages over a… (more)

Subjects/Keywords: FVM; Immersed; Embedded; Ghost cell; Cartesian grid; CFD; Unstructured; Conservative; Helicopter; Rotor/frame; Cut cell; Actuator disk; Turbulence modeling; Wall function

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APA (6th Edition):

Lee, J. (2006). Development of an Efficient Viscous Approach in a Cartesian Grid Framework and Application to Rotor-Fuselage Interaction. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/11474

Chicago Manual of Style (16th Edition):

Lee, Jae-doo. “Development of an Efficient Viscous Approach in a Cartesian Grid Framework and Application to Rotor-Fuselage Interaction.” 2006. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/11474.

MLA Handbook (7th Edition):

Lee, Jae-doo. “Development of an Efficient Viscous Approach in a Cartesian Grid Framework and Application to Rotor-Fuselage Interaction.” 2006. Web. 24 Jul 2019.

Vancouver:

Lee J. Development of an Efficient Viscous Approach in a Cartesian Grid Framework and Application to Rotor-Fuselage Interaction. [Internet] [Doctoral dissertation]. Georgia Tech; 2006. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/11474.

Council of Science Editors:

Lee J. Development of an Efficient Viscous Approach in a Cartesian Grid Framework and Application to Rotor-Fuselage Interaction. [Doctoral Dissertation]. Georgia Tech; 2006. Available from: http://hdl.handle.net/1853/11474


Georgia Tech

28. O'Brien, David Michael, Jr. Analysis Of Computational Modeling Techniques For Complete Rotorcraft Configurations.

Degree: PhD, Aerospace Engineering, 2006, Georgia Tech

 Recent increases in computing power and memory have created renewed interest in alternative grid schemes such as unstructured grids, which facilitate rapid grid generation by… (more)

Subjects/Keywords: Rotor; Actuator disk; Overset; Helicopter; Navier Stokes; Navier-Stokes equations; Rotors (Helicopters)

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APA (6th Edition):

O'Brien, David Michael, J. (2006). Analysis Of Computational Modeling Techniques For Complete Rotorcraft Configurations. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/10535

Chicago Manual of Style (16th Edition):

O'Brien, David Michael, Jr. “Analysis Of Computational Modeling Techniques For Complete Rotorcraft Configurations.” 2006. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/10535.

MLA Handbook (7th Edition):

O'Brien, David Michael, Jr. “Analysis Of Computational Modeling Techniques For Complete Rotorcraft Configurations.” 2006. Web. 24 Jul 2019.

Vancouver:

O'Brien, David Michael J. Analysis Of Computational Modeling Techniques For Complete Rotorcraft Configurations. [Internet] [Doctoral dissertation]. Georgia Tech; 2006. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/10535.

Council of Science Editors:

O'Brien, David Michael J. Analysis Of Computational Modeling Techniques For Complete Rotorcraft Configurations. [Doctoral Dissertation]. Georgia Tech; 2006. Available from: http://hdl.handle.net/1853/10535


Georgia Tech

29. Vasilescu, Roxana. Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing.

Degree: PhD, Aerospace Engineering, 2004, Georgia Tech

 Aeroacoustic investigations regarding different types of helicopter noise have indicated that the most annoying noise is caused by impulsive blade surface pressure changes in descent… (more)

Subjects/Keywords: Piezoelectric actuation; Active flow control; CFD rotor wake; Rotor blade tip vortices; Unsteady modulated blowing; Flutter (Aerodynamics); Rotors (Helicopters) Aerodynamics

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APA (6th Edition):

Vasilescu, R. (2004). Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/4896

Chicago Manual of Style (16th Edition):

Vasilescu, Roxana. “Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing.” 2004. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/4896.

MLA Handbook (7th Edition):

Vasilescu, Roxana. “Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing.” 2004. Web. 24 Jul 2019.

Vancouver:

Vasilescu R. Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing. [Internet] [Doctoral dissertation]. Georgia Tech; 2004. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/4896.

Council of Science Editors:

Vasilescu R. Helicopter Blade Tip Vortex Modifications in Hover Using Piezoelectrically Modulated Blowing. [Doctoral Dissertation]. Georgia Tech; 2004. Available from: http://hdl.handle.net/1853/4896


Georgia Tech

30. Xu, Shuyi. Turbulent Mixing of Passive Scalars at High Schmidt Number.

Degree: PhD, Aerospace Engineering, 2005, Georgia Tech

 A numerical study of fundamental aspects of turbulent mixing has been performed,with emphasis on the behavior of passive scalars of low molecular diffusivity (high Schmidt… (more)

Subjects/Keywords: Turbulent mixing; Passive scalars; Intermittency exponent; Direct numerical simulation; Mixing Simulation methods; Turbulence Simulation methods; Fluid mechanics Statistical methods

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APA (6th Edition):

Xu, S. (2005). Turbulent Mixing of Passive Scalars at High Schmidt Number. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/7002

Chicago Manual of Style (16th Edition):

Xu, Shuyi. “Turbulent Mixing of Passive Scalars at High Schmidt Number.” 2005. Doctoral Dissertation, Georgia Tech. Accessed July 24, 2019. http://hdl.handle.net/1853/7002.

MLA Handbook (7th Edition):

Xu, Shuyi. “Turbulent Mixing of Passive Scalars at High Schmidt Number.” 2005. Web. 24 Jul 2019.

Vancouver:

Xu S. Turbulent Mixing of Passive Scalars at High Schmidt Number. [Internet] [Doctoral dissertation]. Georgia Tech; 2005. [cited 2019 Jul 24]. Available from: http://hdl.handle.net/1853/7002.

Council of Science Editors:

Xu S. Turbulent Mixing of Passive Scalars at High Schmidt Number. [Doctoral Dissertation]. Georgia Tech; 2005. Available from: http://hdl.handle.net/1853/7002

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