Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

Dept: Aerospace Engineering - Mechanical and Aerospace Engineering  University: University of Florida

You searched for subject:(cascading centrality coupling diffusion interdependent optimization). Showing records 1 – 20 of 20 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


University of Florida

1. Blanco, Ariel. The Rarefied Gas Electro Jet (RGEJ) Micro-Thruster for Propulsion of Small Satellites.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2017, University of Florida

 Small satellites have multiple applications such as commercial, military, and space science missions. Further development of micro-propulsion concepts is needed. In this dissertation, a micro-thrusters… (more)

Subjects/Keywords: drift-diffusion-approximation  – electrothermal-thrusters  – micro-propulsion  – plasma  – rarefied-gas

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Blanco, A. (2017). The Rarefied Gas Electro Jet (RGEJ) Micro-Thruster for Propulsion of Small Satellites. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0050292

Chicago Manual of Style (16th Edition):

Blanco, Ariel. “The Rarefied Gas Electro Jet (RGEJ) Micro-Thruster for Propulsion of Small Satellites.” 2017. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0050292.

MLA Handbook (7th Edition):

Blanco, Ariel. “The Rarefied Gas Electro Jet (RGEJ) Micro-Thruster for Propulsion of Small Satellites.” 2017. Web. 14 Dec 2019.

Vancouver:

Blanco A. The Rarefied Gas Electro Jet (RGEJ) Micro-Thruster for Propulsion of Small Satellites. [Internet] [Doctoral dissertation]. University of Florida; 2017. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0050292.

Council of Science Editors:

Blanco A. The Rarefied Gas Electro Jet (RGEJ) Micro-Thruster for Propulsion of Small Satellites. [Doctoral Dissertation]. University of Florida; 2017. Available from: http://ufdc.ufl.edu/UFE0050292


University of Florida

2. Nambi,Sara. Optimal Control and Design Using Genetic Algorithm Accelerated by Neural Networks.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 The main feature of this paper is the incorporation of Artificial Neural Networks (ANN) to accelerate the processing time of Genetic Algorithms (GA). In this… (more)

Subjects/Keywords: Approximation; Crossovers; Design engineering; Design optimization; Genetic algorithms; Mathematical vectors; Neural networks; Optimal solutions; Range searching; Trajectories; genetic  – neural  – optimization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Nambi,Sara. (2011). Optimal Control and Design Using Genetic Algorithm Accelerated by Neural Networks. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043086

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

Nambi,Sara. “Optimal Control and Design Using Genetic Algorithm Accelerated by Neural Networks.” 2011. Masters Thesis, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0043086.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

Nambi,Sara. “Optimal Control and Design Using Genetic Algorithm Accelerated by Neural Networks.” 2011. Web. 14 Dec 2019.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

Nambi,Sara. Optimal Control and Design Using Genetic Algorithm Accelerated by Neural Networks. [Internet] [Masters thesis]. University of Florida; 2011. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0043086.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

Nambi,Sara. Optimal Control and Design Using Genetic Algorithm Accelerated by Neural Networks. [Masters Thesis]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043086

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


University of Florida

3. Viana,Felipe Antonio C. Multiple Surrogates for Prediction and Optimization.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 Statistical modeling of computer experiments embraces the set of methodologies for generating a surrogate model (also known as metamodel or response surface approximation) used to… (more)

Subjects/Keywords: Boxes; Datasets; Design optimization; Engineering; Experiment design; Kriging; Modeling; Neural networks; Safety factors; Simulations; design  – kriging  – optimization  – surrogates

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

C, V. A. (2011). Multiple Surrogates for Prediction and Optimization. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043101

Chicago Manual of Style (16th Edition):

C, Viana,Felipe Antonio. “Multiple Surrogates for Prediction and Optimization.” 2011. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0043101.

MLA Handbook (7th Edition):

C, Viana,Felipe Antonio. “Multiple Surrogates for Prediction and Optimization.” 2011. Web. 14 Dec 2019.

Vancouver:

C VA. Multiple Surrogates for Prediction and Optimization. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0043101.

Council of Science Editors:

C VA. Multiple Surrogates for Prediction and Optimization. [Doctoral Dissertation]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043101


University of Florida

4. Villanueva, Diane C. Reliability Based Design Including Future Tests and Multi-Agent Approaches.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 The initial stages of reliability-based design optimization involve the formulation of objective functions and constraints, and building a model to estimate the reliability of the… (more)

Subjects/Keywords: Design engineering; Design optimization; Error rates; Mathematical optima; Modeling; Objective functions; Random variables; Safety factors; Temperature distribution; Thermal protection; agents  – optimization  – reliability  – surrogates  – uncertainty

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Villanueva, D. C. (2013). Reliability Based Design Including Future Tests and Multi-Agent Approaches. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045819

Chicago Manual of Style (16th Edition):

Villanueva, Diane C. “Reliability Based Design Including Future Tests and Multi-Agent Approaches.” 2013. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0045819.

MLA Handbook (7th Edition):

Villanueva, Diane C. “Reliability Based Design Including Future Tests and Multi-Agent Approaches.” 2013. Web. 14 Dec 2019.

Vancouver:

Villanueva DC. Reliability Based Design Including Future Tests and Multi-Agent Approaches. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0045819.

Council of Science Editors:

Villanueva DC. Reliability Based Design Including Future Tests and Multi-Agent Approaches. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045819


University of Florida

5. Picheny, Victor. Improving Accuracy and Compensating for Uncertainty in Surrogate Modeling.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 In most engineering fields, numerical simulators are used to model complex phenomena and obtain high-fidelity analysis. Despite the growth of computer capabilities, such simulators are… (more)

Subjects/Keywords: Covariance; Cumulative distribution functions; Design optimization; Estimate reliability; Estimators; Experiment design; Kriging; Modeling; Safety factors; Simulations; conservativeness, design, metamodel, prediction, reliability

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Picheny, V. (2009). Improving Accuracy and Compensating for Uncertainty in Surrogate Modeling. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041248

Chicago Manual of Style (16th Edition):

Picheny, Victor. “Improving Accuracy and Compensating for Uncertainty in Surrogate Modeling.” 2009. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0041248.

MLA Handbook (7th Edition):

Picheny, Victor. “Improving Accuracy and Compensating for Uncertainty in Surrogate Modeling.” 2009. Web. 14 Dec 2019.

Vancouver:

Picheny V. Improving Accuracy and Compensating for Uncertainty in Surrogate Modeling. [Internet] [Doctoral dissertation]. University of Florida; 2009. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0041248.

Council of Science Editors:

Picheny V. Improving Accuracy and Compensating for Uncertainty in Surrogate Modeling. [Doctoral Dissertation]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0041248


University of Florida

6. Tian, Ye. Adaptive Control of Separated Flow.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

Subjects/Keywords: closed; disturbance; optimization; separation; synthetic; system; znmf

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Tian, Y. (2007). Adaptive Control of Separated Flow. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0021285

Chicago Manual of Style (16th Edition):

Tian, Ye. “Adaptive Control of Separated Flow.” 2007. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0021285.

MLA Handbook (7th Edition):

Tian, Ye. “Adaptive Control of Separated Flow.” 2007. Web. 14 Dec 2019.

Vancouver:

Tian Y. Adaptive Control of Separated Flow. [Internet] [Doctoral dissertation]. University of Florida; 2007. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0021285.

Council of Science Editors:

Tian Y. Adaptive Control of Separated Flow. [Doctoral Dissertation]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0021285


University of Florida

7. Bhat, Sanketh. Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2010, University of Florida

 Traditionally, the design of structural systems and vehicles has focused first on the design of the structure and then the control and other aspects are… (more)

Subjects/Keywords: Design analysis; Design optimization; Distance functions; Elevators; Hypersonic aircraft; Kriging; Mathematical variables; Systems design; Vibration; Weighting functions; control, hypersonic, linear, surrogate

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bhat, S. (2010). Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042357

Chicago Manual of Style (16th Edition):

Bhat, Sanketh. “Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance.” 2010. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0042357.

MLA Handbook (7th Edition):

Bhat, Sanketh. “Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance.” 2010. Web. 14 Dec 2019.

Vancouver:

Bhat S. Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0042357.

Council of Science Editors:

Bhat S. Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0042357


University of Florida

8. Graham, Kathryn F. Trajectory Optimization of Low-Thrust Orbit Transfers.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2015, University of Florida

 Since the world's first artificial satellite, the Sputnik 1, completed its first orbit around the Earth, we have persistently been developing new technology with an… (more)

Subjects/Keywords: Apocenter; Initial guess; Optimal control; Orbitals; Orbits; Periapsis; Semimajor axis; Spacecraft; Textual collocation; Trajectories; low-thrust  – orbit-transfers  – trajectory-optimization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Graham, K. F. (2015). Trajectory Optimization of Low-Thrust Orbit Transfers. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0049591

Chicago Manual of Style (16th Edition):

Graham, Kathryn F. “Trajectory Optimization of Low-Thrust Orbit Transfers.” 2015. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0049591.

MLA Handbook (7th Edition):

Graham, Kathryn F. “Trajectory Optimization of Low-Thrust Orbit Transfers.” 2015. Web. 14 Dec 2019.

Vancouver:

Graham KF. Trajectory Optimization of Low-Thrust Orbit Transfers. [Internet] [Doctoral dissertation]. University of Florida; 2015. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0049591.

Council of Science Editors:

Graham KF. Trajectory Optimization of Low-Thrust Orbit Transfers. [Doctoral Dissertation]. University of Florida; 2015. Available from: http://ufdc.ufl.edu/UFE0049591


University of Florida

9. Matsumura, Taiki. Effective Safety Measures with Tests Followed by Design Correction for Aerospace Structures.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 Analytical and computational prediction tools enable us to design aircraft and spacecraft components with high degree of confidence. While the accuracy of such predictions has… (more)

Subjects/Keywords: Accident investigation; Aircraft accidents; Cost efficiency; Cost estimates; Design optimization; Failure modes; Laminates; Modeling; Safety factors; Uncertainty; aviation  – design  – resource  – safty  – surrogate

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Matsumura, T. (2013). Effective Safety Measures with Tests Followed by Design Correction for Aerospace Structures. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046232

Chicago Manual of Style (16th Edition):

Matsumura, Taiki. “Effective Safety Measures with Tests Followed by Design Correction for Aerospace Structures.” 2013. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0046232.

MLA Handbook (7th Edition):

Matsumura, Taiki. “Effective Safety Measures with Tests Followed by Design Correction for Aerospace Structures.” 2013. Web. 14 Dec 2019.

Vancouver:

Matsumura T. Effective Safety Measures with Tests Followed by Design Correction for Aerospace Structures. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0046232.

Council of Science Editors:

Matsumura T. Effective Safety Measures with Tests Followed by Design Correction for Aerospace Structures. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0046232


University of Florida

10. Lin, Albert. Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Flexible wing micro air vehicles (MAVs) have been developed at the University of Florida to improve adverse flying conditions. Typically, such MAVs display low Reynolds… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Bats; Carbon fibers; Design optimization; Latex; Silicone rubbers; Silicones; Topology; Vacuum; aeroelastic, deformation, fabrication, manufacturing, mav, membrane, silicone, uav, vic, wings

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lin, A. (2009). Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041333

Chicago Manual of Style (16th Edition):

Lin, Albert. “Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings.” 2009. Masters Thesis, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0041333.

MLA Handbook (7th Edition):

Lin, Albert. “Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings.” 2009. Web. 14 Dec 2019.

Vancouver:

Lin A. Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0041333.

Council of Science Editors:

Lin A. Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0041333


University of Florida

11. Boesl, Benjamin. Fracture Toughening Mechanisms in Nanoparticle And Micro-Particle Reinforced Epoxy Systems Using Multi-scale Analysis.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Fracture toughness results from multi-scale experimentation and modeling of a polymer system reinforced with ZnO particles of two nominal diameters (53 nanometers and 75 microns)… (more)

Subjects/Keywords: Coefficient of friction; Composite materials; Composite particles; Diameters; Fracture strength; Nanocomposites; Nanoparticles; Polymers; Simulations; Stress fields; dispersion, fib, fracture, nanocomposite, optimization, tribology

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Boesl, B. (2009). Fracture Toughening Mechanisms in Nanoparticle And Micro-Particle Reinforced Epoxy Systems Using Multi-scale Analysis. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024281

Chicago Manual of Style (16th Edition):

Boesl, Benjamin. “Fracture Toughening Mechanisms in Nanoparticle And Micro-Particle Reinforced Epoxy Systems Using Multi-scale Analysis.” 2009. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0024281.

MLA Handbook (7th Edition):

Boesl, Benjamin. “Fracture Toughening Mechanisms in Nanoparticle And Micro-Particle Reinforced Epoxy Systems Using Multi-scale Analysis.” 2009. Web. 14 Dec 2019.

Vancouver:

Boesl B. Fracture Toughening Mechanisms in Nanoparticle And Micro-Particle Reinforced Epoxy Systems Using Multi-scale Analysis. [Internet] [Doctoral dissertation]. University of Florida; 2009. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0024281.

Council of Science Editors:

Boesl B. Fracture Toughening Mechanisms in Nanoparticle And Micro-Particle Reinforced Epoxy Systems Using Multi-scale Analysis. [Doctoral Dissertation]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024281


University of Florida

12. Carter, Ryan Elliot. System Identification and Trajectory Optimization for Guided Store Separation.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 Combat aircraft utilize expendable stores such as missiles, bombs, flares, and external tanks to execute their missions.  Safe and acceptable separation of these stores from… (more)

Subjects/Keywords: Aerodynamics; Aircraft; Flight conditions; Flight tests; Parametric models; Simulations; Sine function; System identification; Trajectories; Velocity; autopilot  – control  – identification  – neighboring  – optimal  – optimization  – separation  – store  – system  – trajectory

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Carter, R. E. (2012). System Identification and Trajectory Optimization for Guided Store Separation. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044483

Chicago Manual of Style (16th Edition):

Carter, Ryan Elliot. “System Identification and Trajectory Optimization for Guided Store Separation.” 2012. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0044483.

MLA Handbook (7th Edition):

Carter, Ryan Elliot. “System Identification and Trajectory Optimization for Guided Store Separation.” 2012. Web. 14 Dec 2019.

Vancouver:

Carter RE. System Identification and Trajectory Optimization for Guided Store Separation. [Internet] [Doctoral dissertation]. University of Florida; 2012. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0044483.

Council of Science Editors:

Carter RE. System Identification and Trajectory Optimization for Guided Store Separation. [Doctoral Dissertation]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044483


University of Florida

13. Mack, Yolanda T. CFD-Based Surrogate Modeling of Liquid Rocket Engine Components via Design Space Refinement and Sensitivity Assessment.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 Computational fluid dynamics (CFD) can be used to improve the design and optimization of rocket engine components that traditionally rely on empirical calculations and limited… (more)

Subjects/Keywords: Charge flow devices; Combustion; Combustion chambers; Design analysis; Design optimization; Heat flux; Internal combustion engines; Kriging; Modeling; Turbines; cfd, design, dsr, injector, optimization, refinement, rocket

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mack, Y. T. (2007). CFD-Based Surrogate Modeling of Liquid Rocket Engine Components via Design Space Refinement and Sensitivity Assessment. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0021303

Chicago Manual of Style (16th Edition):

Mack, Yolanda T. “CFD-Based Surrogate Modeling of Liquid Rocket Engine Components via Design Space Refinement and Sensitivity Assessment.” 2007. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0021303.

MLA Handbook (7th Edition):

Mack, Yolanda T. “CFD-Based Surrogate Modeling of Liquid Rocket Engine Components via Design Space Refinement and Sensitivity Assessment.” 2007. Web. 14 Dec 2019.

Vancouver:

Mack YT. CFD-Based Surrogate Modeling of Liquid Rocket Engine Components via Design Space Refinement and Sensitivity Assessment. [Internet] [Doctoral dissertation]. University of Florida; 2007. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0021303.

Council of Science Editors:

Mack YT. CFD-Based Surrogate Modeling of Liquid Rocket Engine Components via Design Space Refinement and Sensitivity Assessment. [Doctoral Dissertation]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0021303


University of Florida

14. Ramu, Palaniappan. Multiple Tail Models Including Inverse Measures for Structural Design under Uncertainties.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 Sampling-based reliability estimation with expensive computer models may be computationally prohibitive due to a large number of required simulations. One way to alleviate the computational… (more)

Subjects/Keywords: Cumulative distribution functions; Design analysis; Design optimization; Error rates; Estimate reliability; Estimation methods; Failure modes; Quantiles; Random variables; Safety factors; inverse, optimization, reliability, tail

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ramu, P. (2007). Multiple Tail Models Including Inverse Measures for Structural Design under Uncertainties. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0021707

Chicago Manual of Style (16th Edition):

Ramu, Palaniappan. “Multiple Tail Models Including Inverse Measures for Structural Design under Uncertainties.” 2007. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0021707.

MLA Handbook (7th Edition):

Ramu, Palaniappan. “Multiple Tail Models Including Inverse Measures for Structural Design under Uncertainties.” 2007. Web. 14 Dec 2019.

Vancouver:

Ramu P. Multiple Tail Models Including Inverse Measures for Structural Design under Uncertainties. [Internet] [Doctoral dissertation]. University of Florida; 2007. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0021707.

Council of Science Editors:

Ramu P. Multiple Tail Models Including Inverse Measures for Structural Design under Uncertainties. [Doctoral Dissertation]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0021707


University of Florida

15. Li, Yawei. Side-Implanted Piezoresistive Shear Stress Sensor for Turbulent Boundary Layer Measurement.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2008, University of Florida

 In this dissertation, I discuss the device modeling, design optimization, fabrication, packaging and characterization of a micromachined floating element piezoresistive shear stress sensor for the… (more)

Subjects/Keywords: Design optimization; Doping; Electric potential; Oxides; Resistors; Sensors; Shear stress; Silicon; Structural deflection; Thermal noise; drie, friction, implanted, mems, micromachining, optimization, piezoresistive, rie, sensor, shear, side, skin, stress

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Li, Y. (2008). Side-Implanted Piezoresistive Shear Stress Sensor for Turbulent Boundary Layer Measurement. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0017550

Chicago Manual of Style (16th Edition):

Li, Yawei. “Side-Implanted Piezoresistive Shear Stress Sensor for Turbulent Boundary Layer Measurement.” 2008. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0017550.

MLA Handbook (7th Edition):

Li, Yawei. “Side-Implanted Piezoresistive Shear Stress Sensor for Turbulent Boundary Layer Measurement.” 2008. Web. 14 Dec 2019.

Vancouver:

Li Y. Side-Implanted Piezoresistive Shear Stress Sensor for Turbulent Boundary Layer Measurement. [Internet] [Doctoral dissertation]. University of Florida; 2008. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0017550.

Council of Science Editors:

Li Y. Side-Implanted Piezoresistive Shear Stress Sensor for Turbulent Boundary Layer Measurement. [Doctoral Dissertation]. University of Florida; 2008. Available from: http://ufdc.ufl.edu/UFE0017550


University of Florida

16. Stanford, Bret Kennedy. Aeroelastic Analysis and Optimization of Membrane Micro Air Vehicle Wings.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2008, University of Florida

 Fixed-wing micro air vehicles are difficult to fly, due to their low Reynolds number, low aspect ratio nature: flow separation erodes wing efficiency, the wings… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Carbon fibers; Design optimization; Laminates; Leading edges; Rigid wings; Skin; Topology; Trailing edges; aeroelasticity, membrane

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Stanford, B. K. (2008). Aeroelastic Analysis and Optimization of Membrane Micro Air Vehicle Wings. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0021970

Chicago Manual of Style (16th Edition):

Stanford, Bret Kennedy. “Aeroelastic Analysis and Optimization of Membrane Micro Air Vehicle Wings.” 2008. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0021970.

MLA Handbook (7th Edition):

Stanford, Bret Kennedy. “Aeroelastic Analysis and Optimization of Membrane Micro Air Vehicle Wings.” 2008. Web. 14 Dec 2019.

Vancouver:

Stanford BK. Aeroelastic Analysis and Optimization of Membrane Micro Air Vehicle Wings. [Internet] [Doctoral dissertation]. University of Florida; 2008. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0021970.

Council of Science Editors:

Stanford BK. Aeroelastic Analysis and Optimization of Membrane Micro Air Vehicle Wings. [Doctoral Dissertation]. University of Florida; 2008. Available from: http://ufdc.ufl.edu/UFE0021970


University of Florida

17. Bhat, Sanketh. Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2008, University of Florida

 Hypersonic flight is seen as a feasible solution to make space travel faster, safer and more affordable. The design of the Air-breathing hypersonic vehicle is… (more)

Subjects/Keywords: Damping; Design analysis; Design optimization; Dynamic structural analysis; Fuselages; Hypersonic aircraft; Hypersonics; Modeling; Temperature profiles; Vibration; aerothermoelasticity, control, hypersonic, parameter, varying

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bhat, S. (2008). Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024107

Chicago Manual of Style (16th Edition):

Bhat, Sanketh. “Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle.” 2008. Masters Thesis, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0024107.

MLA Handbook (7th Edition):

Bhat, Sanketh. “Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle.” 2008. Web. 14 Dec 2019.

Vancouver:

Bhat S. Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle. [Internet] [Masters thesis]. University of Florida; 2008. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0024107.

Council of Science Editors:

Bhat S. Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle. [Masters Thesis]. University of Florida; 2008. Available from: http://ufdc.ufl.edu/UFE0024107


University of Florida

18. Love,Robert D. An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 Morphing and flapping wings are enabling technologies for vehicles of the future. Vehicles with morphing and flapping wings will have greater mission capability and flexibility… (more)

Subjects/Keywords: Aerodynamics; Aircraft; Aircraft wings; Dynamic structural analysis; Kinematics; Modeling; Piezoelectric actuators; Sensors; Signals; Structural deflection; aeroelastic  – aeroelasticity  – aeroservoelastic  – aeroservoelasticity  – aerospace  – aircraft  – analysis  – basis  – control  – design  – dynamics  – experimental  – feedback  – feedforward  – flapping  – flexibility  – flexible  – flight  – frequency  – hydroelasticity  – identification  – interdisciplinary  – mav  – mechanics  – model  – morphing  – optimization  – performance  – periodic  – processing  – robustness  – sensor  – shape  – signal  – structural  – time  – uav  – wing  – wings

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

D, L. (2011). An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043309

Chicago Manual of Style (16th Edition):

D, Love,Robert. “An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings.” 2011. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0043309.

MLA Handbook (7th Edition):

D, Love,Robert. “An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings.” 2011. Web. 14 Dec 2019.

Vancouver:

D L. An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0043309.

Council of Science Editors:

D L. An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings. [Doctoral Dissertation]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043309


University of Florida

19. Liu, Fei. A Tunable Electromechanical Helmholtz Resonator.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

Subjects/Keywords: Acoustic ducts; Acoustic impedance; Acoustic noise; Damping; Design optimization; Helmholtz resonators; Microphones; Neck; Resonant frequencies; Velocity; acoustic, electromechanical, helmholtz, impedance, noise, pareto

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Liu, F. (2007). A Tunable Electromechanical Helmholtz Resonator. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0019815

Chicago Manual of Style (16th Edition):

Liu, Fei. “A Tunable Electromechanical Helmholtz Resonator.” 2007. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0019815.

MLA Handbook (7th Edition):

Liu, Fei. “A Tunable Electromechanical Helmholtz Resonator.” 2007. Web. 14 Dec 2019.

Vancouver:

Liu F. A Tunable Electromechanical Helmholtz Resonator. [Internet] [Doctoral dissertation]. University of Florida; 2007. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0019815.

Council of Science Editors:

Liu F. A Tunable Electromechanical Helmholtz Resonator. [Doctoral Dissertation]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0019815


University of Florida

20. Boria, Frank J. Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 Advancements of compliant actuator technologies and flexible composite structures have enabled true wing morphing capabilities. The resultant effect of these new capabilities is optimal wing… (more)

Subjects/Keywords: Aerodynamic coefficients; Aerodynamics; Aircraft wings; Airfoil camber; Airfoils; Drag coefficient; Genetic algorithms; Servomotors; Three dimensional imaging; Wind tunnels; aerodynamic, air, aircraft, algorithm, biorobots, boria, change, composite, dic, ga, genetic, hardware, loop, mav, morph, morphing, optimization, shape, uav, vehicle, vic, wing

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Boria, F. J. (2007). Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0021478

Chicago Manual of Style (16th Edition):

Boria, Frank J. “Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop.” 2007. Masters Thesis, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0021478.

MLA Handbook (7th Edition):

Boria, Frank J. “Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop.” 2007. Web. 14 Dec 2019.

Vancouver:

Boria FJ. Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop. [Internet] [Masters thesis]. University of Florida; 2007. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0021478.

Council of Science Editors:

Boria FJ. Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop. [Masters Thesis]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0021478

.