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You searched for +publisher:"Georgia Tech" +contributor:("Rimoli, Julian J."). Showing records 1 – 19 of 19 total matches.

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Georgia Tech

1. Carrara, Matteo. Fourier-based design of acoustic transducers.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 The work presented in this thesis investigates novel transducer implementations that take advantage of directional sensing and generation of acoustic waves. These transducers are conceived… (more)

Subjects/Keywords: Guided waves; Lamb waves; Piezoelectricity; Transducer design; Structural health monitoring; SAW; Strain sensing; Impact localization

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APA (6th Edition):

Carrara, M. (2015). Fourier-based design of acoustic transducers. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54925

Chicago Manual of Style (16th Edition):

Carrara, Matteo. “Fourier-based design of acoustic transducers.” 2015. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/54925.

MLA Handbook (7th Edition):

Carrara, Matteo. “Fourier-based design of acoustic transducers.” 2015. Web. 20 Oct 2019.

Vancouver:

Carrara M. Fourier-based design of acoustic transducers. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/54925.

Council of Science Editors:

Carrara M. Fourier-based design of acoustic transducers. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54925


Georgia Tech

2. Yuan, Zhangxian. Geometric nonlinearity effects on the behavior of sandwich structures.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 The Extended High-order Sandwich Panel Theory (EHSAPT) accounts for the axial rigidity, the transverse compressibility, and the shear effect of the core. Thus, it is… (more)

Subjects/Keywords: Sandwich structures; Geometric nonlinearity; High-order theory; Dynamic; Stability; Post-buckling

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APA (6th Edition):

Yuan, Z. (2017). Geometric nonlinearity effects on the behavior of sandwich structures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59271

Chicago Manual of Style (16th Edition):

Yuan, Zhangxian. “Geometric nonlinearity effects on the behavior of sandwich structures.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/59271.

MLA Handbook (7th Edition):

Yuan, Zhangxian. “Geometric nonlinearity effects on the behavior of sandwich structures.” 2017. Web. 20 Oct 2019.

Vancouver:

Yuan Z. Geometric nonlinearity effects on the behavior of sandwich structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/59271.

Council of Science Editors:

Yuan Z. Geometric nonlinearity effects on the behavior of sandwich structures. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59271


Georgia Tech

3. Sadat Hoseini Khajuee, Seyed Mohammad Hanif. A joined 3D/1D finite element method for aeroservoelastic analysis of damaged HALE aircraft wings.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Nonlinear aeroelastic analysis of damaged High-Altitude-Long-Endurance aircraft wings is considered. The structural model consists of a full three-dimensional finite element continuum model for the damaged… (more)

Subjects/Keywords: Nonlinear aeroelasticity; Aeroservoelasticity; Flutter suppression; Control; Damage; HALE aircraft

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APA (6th Edition):

Sadat Hoseini Khajuee, S. M. H. (2018). A joined 3D/1D finite element method for aeroservoelastic analysis of damaged HALE aircraft wings. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59916

Chicago Manual of Style (16th Edition):

Sadat Hoseini Khajuee, Seyed Mohammad Hanif. “A joined 3D/1D finite element method for aeroservoelastic analysis of damaged HALE aircraft wings.” 2018. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/59916.

MLA Handbook (7th Edition):

Sadat Hoseini Khajuee, Seyed Mohammad Hanif. “A joined 3D/1D finite element method for aeroservoelastic analysis of damaged HALE aircraft wings.” 2018. Web. 20 Oct 2019.

Vancouver:

Sadat Hoseini Khajuee SMH. A joined 3D/1D finite element method for aeroservoelastic analysis of damaged HALE aircraft wings. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/59916.

Council of Science Editors:

Sadat Hoseini Khajuee SMH. A joined 3D/1D finite element method for aeroservoelastic analysis of damaged HALE aircraft wings. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59916


Georgia Tech

4. Trainiti, Giuseppe. Wave propagation in space and time modulated structures.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 This thesis investigates structures with spatial and temporal modulation of the effective mechanical properties, contributing to the state-of-the-art of wave propagation control techniques and to… (more)

Subjects/Keywords: Wave propagation; Periodic structures; Metamaterials; Non-reciprocal systems; Digital image correlation; Lattice structures; Undulation; Curvature

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APA (6th Edition):

Trainiti, G. (2018). Wave propagation in space and time modulated structures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59920

Chicago Manual of Style (16th Edition):

Trainiti, Giuseppe. “Wave propagation in space and time modulated structures.” 2018. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/59920.

MLA Handbook (7th Edition):

Trainiti, Giuseppe. “Wave propagation in space and time modulated structures.” 2018. Web. 20 Oct 2019.

Vancouver:

Trainiti G. Wave propagation in space and time modulated structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/59920.

Council of Science Editors:

Trainiti G. Wave propagation in space and time modulated structures. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59920


Georgia Tech

5. Gupta, Mohit. Enhancements in Analysis of Beam-Like Structures using Asymptotic Methods.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 As a complement to conventional FEA, state-of-the-art Variational Asymptotic Method (VAM) and a mixed formulation of Geometrically Exact Beam Theory (GEBT) are employed in this… (more)

Subjects/Keywords: Variation Asymptotic Method, VAM, Geometrically Exact Beam Theory, GEBT, Composite, Nonlinear, Transient, Dynamic, Smart, Piezoelectric, Damping, Aperiodic, Inhomogeneous; VAM; Geometrically Exact Beam Theory; GEBT; Composite; Nonlinear; Transient; Piezoelectric; Damping; Aperiodic; Inhomogeneous

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APA (6th Edition):

Gupta, M. (2019). Enhancements in Analysis of Beam-Like Structures using Asymptotic Methods. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61073

Chicago Manual of Style (16th Edition):

Gupta, Mohit. “Enhancements in Analysis of Beam-Like Structures using Asymptotic Methods.” 2019. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/61073.

MLA Handbook (7th Edition):

Gupta, Mohit. “Enhancements in Analysis of Beam-Like Structures using Asymptotic Methods.” 2019. Web. 20 Oct 2019.

Vancouver:

Gupta M. Enhancements in Analysis of Beam-Like Structures using Asymptotic Methods. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/61073.

Council of Science Editors:

Gupta M. Enhancements in Analysis of Beam-Like Structures using Asymptotic Methods. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61073


Georgia Tech

6. Sidor, Adam Thomas. Design and Manufacturing of Conformal Ablative Heatshields.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Conformal ablators, first introduced in the early 2000s under the NASA Hypersonics Project, are a type of rigid ablative thermal protection system that uses flexible,… (more)

Subjects/Keywords: Thermal protection system; heatshield; heat shield; materials; optimization; manufacturing; design; vacuum infusion

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APA (6th Edition):

Sidor, A. T. (2019). Design and Manufacturing of Conformal Ablative Heatshields. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61593

Chicago Manual of Style (16th Edition):

Sidor, Adam Thomas. “Design and Manufacturing of Conformal Ablative Heatshields.” 2019. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/61593.

MLA Handbook (7th Edition):

Sidor, Adam Thomas. “Design and Manufacturing of Conformal Ablative Heatshields.” 2019. Web. 20 Oct 2019.

Vancouver:

Sidor AT. Design and Manufacturing of Conformal Ablative Heatshields. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/61593.

Council of Science Editors:

Sidor AT. Design and Manufacturing of Conformal Ablative Heatshields. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61593


Georgia Tech

7. Capuano, German. Smart Finite Elements: An application of Machine Learning to Reduced-Order Modeling of Multi-Scale Problems.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 To design structures using state-of-the-art materials like composites and metamaterials, we need predictive tools that are capable of taking into account the phenomena occurring at… (more)

Subjects/Keywords: Multiscale; Finite Element; FEM; Nonlinear Constitutive Modeling; Computational Mechanics

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APA (6th Edition):

Capuano, G. (2019). Smart Finite Elements: An application of Machine Learning to Reduced-Order Modeling of Multi-Scale Problems. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61722

Chicago Manual of Style (16th Edition):

Capuano, German. “Smart Finite Elements: An application of Machine Learning to Reduced-Order Modeling of Multi-Scale Problems.” 2019. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/61722.

MLA Handbook (7th Edition):

Capuano, German. “Smart Finite Elements: An application of Machine Learning to Reduced-Order Modeling of Multi-Scale Problems.” 2019. Web. 20 Oct 2019.

Vancouver:

Capuano G. Smart Finite Elements: An application of Machine Learning to Reduced-Order Modeling of Multi-Scale Problems. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/61722.

Council of Science Editors:

Capuano G. Smart Finite Elements: An application of Machine Learning to Reduced-Order Modeling of Multi-Scale Problems. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61722

8. Hardin, David Barrett. The role of viscoplasticity in the deformation and ignition response of polymer bonded explosives.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 The effect of viscoplastic deformation of the energetic material HMX on the mechanical, thermal, and ignition response of a two-phase (HMX and Estane) polymer bonded… (more)

Subjects/Keywords: HMX; Polymer bonded explosives; Ignition sensitivity

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APA (6th Edition):

Hardin, D. B. (2015). The role of viscoplasticity in the deformation and ignition response of polymer bonded explosives. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53516

Chicago Manual of Style (16th Edition):

Hardin, David Barrett. “The role of viscoplasticity in the deformation and ignition response of polymer bonded explosives.” 2015. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/53516.

MLA Handbook (7th Edition):

Hardin, David Barrett. “The role of viscoplasticity in the deformation and ignition response of polymer bonded explosives.” 2015. Web. 20 Oct 2019.

Vancouver:

Hardin DB. The role of viscoplasticity in the deformation and ignition response of polymer bonded explosives. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/53516.

Council of Science Editors:

Hardin DB. The role of viscoplasticity in the deformation and ignition response of polymer bonded explosives. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53516


Georgia Tech

9. Lloyd, Jeffrey T. Microstructure-sensitive simulation of shock loading in metals.

Degree: PhD, Mechanical Engineering, 2014, Georgia Tech

 A constitutive model has been developed to model the shock response of single crystal aluminum from peak pressures ranging from 2-110 GPa. This model couples… (more)

Subjects/Keywords: Continuum mechanics; Aluminum; High rate deformation; Dislocation dynamics; Crystal plasticity; Thermoelasticity; Viscoplasticity; Elasticity; Thermodynamics; Shock (Mechanics); Microstructure

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APA (6th Edition):

Lloyd, J. T. (2014). Microstructure-sensitive simulation of shock loading in metals. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51853

Chicago Manual of Style (16th Edition):

Lloyd, Jeffrey T. “Microstructure-sensitive simulation of shock loading in metals.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/51853.

MLA Handbook (7th Edition):

Lloyd, Jeffrey T. “Microstructure-sensitive simulation of shock loading in metals.” 2014. Web. 20 Oct 2019.

Vancouver:

Lloyd JT. Microstructure-sensitive simulation of shock loading in metals. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/51853.

Council of Science Editors:

Lloyd JT. Microstructure-sensitive simulation of shock loading in metals. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51853


Georgia Tech

10. 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 20, 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. 20 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 20]. 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

11. Chin, Ting Wei. Multi-Physics High Resolution Topology Optimization for Aerospace Structures.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Advancements in multimaterial additive manufacturing have the potential to enable the creation of topology optimized structures with both shape and material tailoring. These are extremely… (more)

Subjects/Keywords: Topology Optimization; Thermoelastic topology optimization; Multimaterial topology optimization; Higher Analysis and Design Parametrization; Natural Frequency; Large-scale topology optimization; High resolution topology optimization

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APA (6th Edition):

Chin, T. W. (2019). Multi-Physics High Resolution Topology Optimization for Aerospace Structures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61217

Chicago Manual of Style (16th Edition):

Chin, Ting Wei. “Multi-Physics High Resolution Topology Optimization for Aerospace Structures.” 2019. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/61217.

MLA Handbook (7th Edition):

Chin, Ting Wei. “Multi-Physics High Resolution Topology Optimization for Aerospace Structures.” 2019. Web. 20 Oct 2019.

Vancouver:

Chin TW. Multi-Physics High Resolution Topology Optimization for Aerospace Structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/61217.

Council of Science Editors:

Chin TW. Multi-Physics High Resolution Topology Optimization for Aerospace Structures. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61217

12. Hill, Jeremy Lee. Mechanical property determination for flexible material systems.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Inflatable Aerodynamic Decelerators (IADs) are a candidate technology NASA began investigating in the late 1960’s. Compared to supersonic parachutes, IADs represent a decelerator option capable… (more)

Subjects/Keywords: Inflatable aerodynamic decelerator; Flexible material systems; Finite element analysis; Multi-scale modeling; Parameter identification

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APA (6th Edition):

Hill, J. L. (2016). Mechanical property determination for flexible material systems. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54993

Chicago Manual of Style (16th Edition):

Hill, Jeremy Lee. “Mechanical property determination for flexible material systems.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/54993.

MLA Handbook (7th Edition):

Hill, Jeremy Lee. “Mechanical property determination for flexible material systems.” 2016. Web. 20 Oct 2019.

Vancouver:

Hill JL. Mechanical property determination for flexible material systems. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/54993.

Council of Science Editors:

Hill JL. Mechanical property determination for flexible material systems. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/54993

13. Kulpe, Jason. Analysis of acoustic scattering from large fish schools using Bloch wave formalism.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 In the open ocean acoustic scattering by SONAR sources can be dominated by large fish schools. Multiple scattering effects are strong and the individual fish… (more)

Subjects/Keywords: Bloch; Acoustic scattering; Dispersion; Phononic crystal; Fish

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APA (6th Edition):

Kulpe, J. (2015). Analysis of acoustic scattering from large fish schools using Bloch wave formalism. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54864

Chicago Manual of Style (16th Edition):

Kulpe, Jason. “Analysis of acoustic scattering from large fish schools using Bloch wave formalism.” 2015. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/54864.

MLA Handbook (7th Edition):

Kulpe, Jason. “Analysis of acoustic scattering from large fish schools using Bloch wave formalism.” 2015. Web. 20 Oct 2019.

Vancouver:

Kulpe J. Analysis of acoustic scattering from large fish schools using Bloch wave formalism. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/54864.

Council of Science Editors:

Kulpe J. Analysis of acoustic scattering from large fish schools using Bloch wave formalism. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54864

14. Kovvali, Ravi Kumar. A nonlinear theory of Cosserat elastic plates using the variational-asymptotic method.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 One of the most important branches of applied mechanics is the theory of plates - defined to be plane structural elements whose thickness is very… (more)

Subjects/Keywords: Cosserat; Plate; Variational; Asymptotic; Drilling; Nonlinear

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APA (6th Edition):

Kovvali, R. K. (2015). A nonlinear theory of Cosserat elastic plates using the variational-asymptotic method. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54342

Chicago Manual of Style (16th Edition):

Kovvali, Ravi Kumar. “A nonlinear theory of Cosserat elastic plates using the variational-asymptotic method.” 2015. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/54342.

MLA Handbook (7th Edition):

Kovvali, Ravi Kumar. “A nonlinear theory of Cosserat elastic plates using the variational-asymptotic method.” 2015. Web. 20 Oct 2019.

Vancouver:

Kovvali RK. A nonlinear theory of Cosserat elastic plates using the variational-asymptotic method. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/54342.

Council of Science Editors:

Kovvali RK. A nonlinear theory of Cosserat elastic plates using the variational-asymptotic method. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54342

15. Richards, Phillip W. Design strategies for rotorcraft blades and HALE aircraft wings applied to damage tolerant wind turbine blade design.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Offshore wind power production is an attractive clean energy option, but the difficulty of access can lead to expensive and rare opportunities for maintenance. Smart… (more)

Subjects/Keywords: Aeroelasticity; Damage tolerance; Design; Flutter; Control design; Rotorcraft; Rotor blades; Wind turbine blades; HALE aircraft

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APA (6th Edition):

Richards, P. W. (2014). Design strategies for rotorcraft blades and HALE aircraft wings applied to damage tolerant wind turbine blade design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53488

Chicago Manual of Style (16th Edition):

Richards, Phillip W. “Design strategies for rotorcraft blades and HALE aircraft wings applied to damage tolerant wind turbine blade design.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/53488.

MLA Handbook (7th Edition):

Richards, Phillip W. “Design strategies for rotorcraft blades and HALE aircraft wings applied to damage tolerant wind turbine blade design.” 2014. Web. 20 Oct 2019.

Vancouver:

Richards PW. Design strategies for rotorcraft blades and HALE aircraft wings applied to damage tolerant wind turbine blade design. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/53488.

Council of Science Editors:

Richards PW. Design strategies for rotorcraft blades and HALE aircraft wings applied to damage tolerant wind turbine blade design. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53488

16. Musinski, William D. Modeling the effects of shot-peened residual stresses and inclusions on microstructure-sensitive fatigue of Ni-base superalloy components.

Degree: PhD, Mechanical Engineering, 2014, Georgia Tech

 The simulation and design of advanced materials for fatigue resistance requires an understanding of the response of their hierarchical microstructure attributes to imposed load, temperature,… (more)

Subjects/Keywords: Fatigue; Micro-structure sensitive; Ni-based superalloy; IN100; Residual stresses; Inclusions

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APA (6th Edition):

Musinski, W. D. (2014). Modeling the effects of shot-peened residual stresses and inclusions on microstructure-sensitive fatigue of Ni-base superalloy components. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/52337

Chicago Manual of Style (16th Edition):

Musinski, William D. “Modeling the effects of shot-peened residual stresses and inclusions on microstructure-sensitive fatigue of Ni-base superalloy components.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/52337.

MLA Handbook (7th Edition):

Musinski, William D. “Modeling the effects of shot-peened residual stresses and inclusions on microstructure-sensitive fatigue of Ni-base superalloy components.” 2014. Web. 20 Oct 2019.

Vancouver:

Musinski WD. Modeling the effects of shot-peened residual stresses and inclusions on microstructure-sensitive fatigue of Ni-base superalloy components. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/52337.

Council of Science Editors:

Musinski WD. Modeling the effects of shot-peened residual stresses and inclusions on microstructure-sensitive fatigue of Ni-base superalloy components. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/52337

17. Mardanpour, Pezhman. Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 Effects of engine placement on flutter characteristics of a very flexible high-aspect-ratio wing are investigated using the code NATASHA (Nonlinear Aeroelastic Trim And Stability of… (more)

Subjects/Keywords: Nonlinear aeroelasticity; Follower force; Effects of engine placement; HALE aircraft; Flying wing aircraft; Area of minimum kinetic energy; Passive morphing; Solar powered flying wing; Airplanes, Tailless; Aeroelasticity; Solar airplanes; Airplanes

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APA (6th Edition):

Mardanpour, P. (2013). Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50268

Chicago Manual of Style (16th Edition):

Mardanpour, Pezhman. “Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft.” 2013. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/50268.

MLA Handbook (7th Edition):

Mardanpour, Pezhman. “Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft.” 2013. Web. 20 Oct 2019.

Vancouver:

Mardanpour P. Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/50268.

Council of Science Editors:

Mardanpour P. Effects of engine placement and morphing on nonlinear aeroelastic behavior of flying wing aircraft. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50268

18. Muralidharan, Balaji. An embedded boundary approach for simulation of reacting flow problems in complex geometries with moving and stationary boundaries.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 Many useful engineering devices involve moving boundaries interacting with a reacting compressible flow. Examples of such applications include propulsion systems with moving components such as… (more)

Subjects/Keywords: AMR; Cut-cell; High-order; LES; Reacting; Moving boundaries

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

APA (6th Edition):

Muralidharan, B. (2017). An embedded boundary approach for simulation of reacting flow problems in complex geometries with moving and stationary boundaries. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/58656

Chicago Manual of Style (16th Edition):

Muralidharan, Balaji. “An embedded boundary approach for simulation of reacting flow problems in complex geometries with moving and stationary boundaries.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/58656.

MLA Handbook (7th Edition):

Muralidharan, Balaji. “An embedded boundary approach for simulation of reacting flow problems in complex geometries with moving and stationary boundaries.” 2017. Web. 20 Oct 2019.

Vancouver:

Muralidharan B. An embedded boundary approach for simulation of reacting flow problems in complex geometries with moving and stationary boundaries. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/58656.

Council of Science Editors:

Muralidharan B. An embedded boundary approach for simulation of reacting flow problems in complex geometries with moving and stationary boundaries. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/58656

19. Schinder, Aaron M. Investigation of Hall effect thruster channel wall erosion mechanisms.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 The primary life-limiting mechanism for Hall effect thrusters (HETs) is the plasma erosion of the discharge channel wall. Over the course of tens of thousands… (more)

Subjects/Keywords: Electric propulsion; Hall effect thrusters; HETs; Erosion; Sputtering; Microscopy; Channel wall; Plasma erosion

Georgia Tech Research Institute HET Hall Effect Thruster LIST OF ABBREVIATIONS xviii NASA… 

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

APA (6th Edition):

Schinder, A. M. (2016). Investigation of Hall effect thruster channel wall erosion mechanisms. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56240

Chicago Manual of Style (16th Edition):

Schinder, Aaron M. “Investigation of Hall effect thruster channel wall erosion mechanisms.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 20, 2019. http://hdl.handle.net/1853/56240.

MLA Handbook (7th Edition):

Schinder, Aaron M. “Investigation of Hall effect thruster channel wall erosion mechanisms.” 2016. Web. 20 Oct 2019.

Vancouver:

Schinder AM. Investigation of Hall effect thruster channel wall erosion mechanisms. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/1853/56240.

Council of Science Editors:

Schinder AM. Investigation of Hall effect thruster channel wall erosion mechanisms. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56240

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