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

You searched for +publisher:"University of Florida" +contributor:("IFJU,PETER G"). Showing records 1 – 23 of 23 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


University of Florida

1. Balmori, Abraham. Design of Secondary Control Surfaces on Unmanned Aircraft Systems to Achieve Low Glide Slope Ratios.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2014, University of Florida

 The mission environment for the Nova 2.1 unmanned aerial system (UAS) is typically constrictive and challenging to operate in. One of the most crucial factors… (more)

Subjects/Keywords: Aircraft; Aircraft wings; Altitude; Automatic pilots; Control surfaces; Glide paths; Remotely piloted vehicles; Spoilers; Vehicular flight; Wing flaps; aircraft  – control  – flap  – glide  – hybrid  – landing  – nova  – slope  – spoiler  – surfaces  – uas  – uav

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Balmori, A. (2014). Design of Secondary Control Surfaces on Unmanned Aircraft Systems to Achieve Low Glide Slope Ratios. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0047241

Chicago Manual of Style (16th Edition):

Balmori, Abraham. “Design of Secondary Control Surfaces on Unmanned Aircraft Systems to Achieve Low Glide Slope Ratios.” 2014. Masters Thesis, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0047241.

MLA Handbook (7th Edition):

Balmori, Abraham. “Design of Secondary Control Surfaces on Unmanned Aircraft Systems to Achieve Low Glide Slope Ratios.” 2014. Web. 10 Dec 2019.

Vancouver:

Balmori A. Design of Secondary Control Surfaces on Unmanned Aircraft Systems to Achieve Low Glide Slope Ratios. [Internet] [Masters thesis]. University of Florida; 2014. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0047241.

Council of Science Editors:

Balmori A. Design of Secondary Control Surfaces on Unmanned Aircraft Systems to Achieve Low Glide Slope Ratios. [Masters Thesis]. University of Florida; 2014. Available from: http://ufdc.ufl.edu/UFE0047241


University of Florida

2. Nelson, Jordan D. Development of an Advanced Automated Nondestructive Evaluation System for Investigation of Concrete Structures and Validation of Concrete NDE Instruments.

Degree: M.E., Mechanical Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 Nondestructive evaluation (NDE) of concrete has historically been a niche discipline within civil engineering and a process carried out by an individual operator in the… (more)

Subjects/Keywords: Bridge decks; Data processing; Lasers; Nondestructive testing; Profilometers; S waves; Software; Specimens; Ultrasonography; Velocity; antares  – automation  – concrete  – gpr  – infrastructure  – nde  – ndt  – nondestructive  – radar  – structures  – ultrasound

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Nelson, J. D. (2013). Development of an Advanced Automated Nondestructive Evaluation System for Investigation of Concrete Structures and Validation of Concrete NDE Instruments. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046341

Chicago Manual of Style (16th Edition):

Nelson, Jordan D. “Development of an Advanced Automated Nondestructive Evaluation System for Investigation of Concrete Structures and Validation of Concrete NDE Instruments.” 2013. Masters Thesis, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0046341.

MLA Handbook (7th Edition):

Nelson, Jordan D. “Development of an Advanced Automated Nondestructive Evaluation System for Investigation of Concrete Structures and Validation of Concrete NDE Instruments.” 2013. Web. 10 Dec 2019.

Vancouver:

Nelson JD. Development of an Advanced Automated Nondestructive Evaluation System for Investigation of Concrete Structures and Validation of Concrete NDE Instruments. [Internet] [Masters thesis]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0046341.

Council of Science Editors:

Nelson JD. Development of an Advanced Automated Nondestructive Evaluation System for Investigation of Concrete Structures and Validation of Concrete NDE Instruments. [Masters Thesis]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0046341


University of Florida

3. Rohde, Sean E. On the Experimental Validation, Modeling, and Optimization of Bend-Twist Coupling in Composite Beams, Tubes, and Shafts.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2016, University of Florida

 This document outlines the research performed on the design, manufacturing, modeling, and experimental testing of composite shafts possessing bend-twist coupling. A novel design for achieving… (more)

Subjects/Keywords: Carbon fibers; Composite materials; Curvature; Fiber orientation; Golf clubs; Laminates; Mandrels; Shear stress; Stiffness; Torque; bend  – composite  – composites  – coupling  – shafts  – tubes  – twist

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Rohde, S. E. (2016). On the Experimental Validation, Modeling, and Optimization of Bend-Twist Coupling in Composite Beams, Tubes, and Shafts. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0050253

Chicago Manual of Style (16th Edition):

Rohde, Sean E. “On the Experimental Validation, Modeling, and Optimization of Bend-Twist Coupling in Composite Beams, Tubes, and Shafts.” 2016. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0050253.

MLA Handbook (7th Edition):

Rohde, Sean E. “On the Experimental Validation, Modeling, and Optimization of Bend-Twist Coupling in Composite Beams, Tubes, and Shafts.” 2016. Web. 10 Dec 2019.

Vancouver:

Rohde SE. On the Experimental Validation, Modeling, and Optimization of Bend-Twist Coupling in Composite Beams, Tubes, and Shafts. [Internet] [Doctoral dissertation]. University of Florida; 2016. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0050253.

Council of Science Editors:

Rohde SE. On the Experimental Validation, Modeling, and Optimization of Bend-Twist Coupling in Composite Beams, Tubes, and Shafts. [Doctoral Dissertation]. University of Florida; 2016. Available from: http://ufdc.ufl.edu/UFE0050253


University of Florida

4. Bhattacharyya, Abir. Evolution of Cyclic Plasticity during Rolling Contact Fatigue of a Case-Hardened Bearing Steel.

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

 A combined experimental and numerical methodology is developed for the investigation of progressive evolution of subsurface plasticity during prolonged rolling contact fatigue (RCF) loading of… (more)

Subjects/Keywords: Carbides; Compressive stress; Contact loads; Fatigue; Hardness; Materials fatigue; Plastics; Shear stress; Steels; Stress cycles; bearings  – fatigue  – indentation  – plasticity  – rcf  – steel

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bhattacharyya, A. (2015). Evolution of Cyclic Plasticity during Rolling Contact Fatigue of a Case-Hardened Bearing Steel. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0047669

Chicago Manual of Style (16th Edition):

Bhattacharyya, Abir. “Evolution of Cyclic Plasticity during Rolling Contact Fatigue of a Case-Hardened Bearing Steel.” 2015. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0047669.

MLA Handbook (7th Edition):

Bhattacharyya, Abir. “Evolution of Cyclic Plasticity during Rolling Contact Fatigue of a Case-Hardened Bearing Steel.” 2015. Web. 10 Dec 2019.

Vancouver:

Bhattacharyya A. Evolution of Cyclic Plasticity during Rolling Contact Fatigue of a Case-Hardened Bearing Steel. [Internet] [Doctoral dissertation]. University of Florida; 2015. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0047669.

Council of Science Editors:

Bhattacharyya A. Evolution of Cyclic Plasticity during Rolling Contact Fatigue of a Case-Hardened Bearing Steel. [Doctoral Dissertation]. University of Florida; 2015. Available from: http://ufdc.ufl.edu/UFE0047669


University of Florida

5. Abudaram, Yaakov J. Form Finding and Analysis of Extensible Membranes Attached to 2-D and 3-D Frames Intended for Micro Air Vehicles via Experimentally Validated Finite Element Methods.

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

 This work is concerned with a new method to apply consistent and known pre-tension to silicone rubber membranes intended formicro air vehicles as well as… (more)

Subjects/Keywords: Aircraft wings; Aspect ratio; Carbon fibers; Inflection points; Silicone rubbers; Silicones; Specimens; Stress ratio; Trailing edges; Wheelchairs; airplanes  – latex  – mav  – membrane  – silicone  – strain  – stress

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Abudaram, Y. J. (2013). Form Finding and Analysis of Extensible Membranes Attached to 2-D and 3-D Frames Intended for Micro Air Vehicles via Experimentally Validated Finite Element Methods. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045856

Chicago Manual of Style (16th Edition):

Abudaram, Yaakov J. “Form Finding and Analysis of Extensible Membranes Attached to 2-D and 3-D Frames Intended for Micro Air Vehicles via Experimentally Validated Finite Element Methods.” 2013. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0045856.

MLA Handbook (7th Edition):

Abudaram, Yaakov J. “Form Finding and Analysis of Extensible Membranes Attached to 2-D and 3-D Frames Intended for Micro Air Vehicles via Experimentally Validated Finite Element Methods.” 2013. Web. 10 Dec 2019.

Vancouver:

Abudaram YJ. Form Finding and Analysis of Extensible Membranes Attached to 2-D and 3-D Frames Intended for Micro Air Vehicles via Experimentally Validated Finite Element Methods. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0045856.

Council of Science Editors:

Abudaram YJ. Form Finding and Analysis of Extensible Membranes Attached to 2-D and 3-D Frames Intended for Micro Air Vehicles via Experimentally Validated Finite Element Methods. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045856


University of Florida

6. Lacroix, Bradley W. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.

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

 This document details the research performed on applying piezoelectric macro fiber composite actuators on micro air vehicles. The research objective was to apply the minimum… (more)

Subjects/Keywords: Aircraft; Aircraft pitch; Aircraft roll; Aircraft wings; Carbon fibers; Design optimization; Geometry; Steels; Swept wings; Wind tunnels; composite  – fiber  – flying  – macro  – materials  – mav  – mfc  – morphing  – optimization  – piezoelectric  – smart  – uav  – wing

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lacroix, B. W. (2013). On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046212

Chicago Manual of Style (16th Edition):

Lacroix, Bradley W. “On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.” 2013. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0046212.

MLA Handbook (7th Edition):

Lacroix, Bradley W. “On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.” 2013. Web. 10 Dec 2019.

Vancouver:

Lacroix BW. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0046212.

Council of Science Editors:

Lacroix BW. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0046212


University of Florida

7. Rue, Jason T. Investigating Manufacturing Techniques, Testing, and Design to Enhance Confidence in Thrust Production for Synthetic Flexible Small Flapping Wings.

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

 Flapping wing technology exists and continues to expand on many fronts, although without a solid understanding behind the physics of flapping flight, a purely experimental… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Aluminum; Carbon fibers; Flat plates; Hovering; Hummingbirds; Industrial design; Manufacturing processes; Stiffness; flapping  – manufacturing  – thrust  – wings

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Rue, J. T. (2013). Investigating Manufacturing Techniques, Testing, and Design to Enhance Confidence in Thrust Production for Synthetic Flexible Small Flapping Wings. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045987

Chicago Manual of Style (16th Edition):

Rue, Jason T. “Investigating Manufacturing Techniques, Testing, and Design to Enhance Confidence in Thrust Production for Synthetic Flexible Small Flapping Wings.” 2013. Masters Thesis, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0045987.

MLA Handbook (7th Edition):

Rue, Jason T. “Investigating Manufacturing Techniques, Testing, and Design to Enhance Confidence in Thrust Production for Synthetic Flexible Small Flapping Wings.” 2013. Web. 10 Dec 2019.

Vancouver:

Rue JT. Investigating Manufacturing Techniques, Testing, and Design to Enhance Confidence in Thrust Production for Synthetic Flexible Small Flapping Wings. [Internet] [Masters thesis]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0045987.

Council of Science Editors:

Rue JT. Investigating Manufacturing Techniques, Testing, and Design to Enhance Confidence in Thrust Production for Synthetic Flexible Small Flapping Wings. [Masters Thesis]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045987


University of Florida

8. 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 10, 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. 10 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 10]. 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

9. Zhang, Zhiyuan. Modal Superposition Using Implicit Boundary Finite Element Method and Application to Flapping Wing Design.

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

 Modal superposition is a widely used technique in engineering design for structural dynamic analysis. It uses the natural frequencies and mode shapes to characterize the… (more)

Subjects/Keywords: Aircraft wings; Cantilever plates; Coordinate systems; Damping; Dynamic structural analysis; Forced vibration; Free vibration; Frequency response; Harmonic excitation; Wrist; base  – boundary  – excitation  – implicit  – method  – vibration

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Zhang, Z. (2013). Modal Superposition Using Implicit Boundary Finite Element Method and Application to Flapping Wing Design. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045485

Chicago Manual of Style (16th Edition):

Zhang, Zhiyuan. “Modal Superposition Using Implicit Boundary Finite Element Method and Application to Flapping Wing Design.” 2013. Masters Thesis, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0045485.

MLA Handbook (7th Edition):

Zhang, Zhiyuan. “Modal Superposition Using Implicit Boundary Finite Element Method and Application to Flapping Wing Design.” 2013. Web. 10 Dec 2019.

Vancouver:

Zhang Z. Modal Superposition Using Implicit Boundary Finite Element Method and Application to Flapping Wing Design. [Internet] [Masters thesis]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0045485.

Council of Science Editors:

Zhang Z. Modal Superposition Using Implicit Boundary Finite Element Method and Application to Flapping Wing Design. [Masters Thesis]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045485


University of Florida

10. Parsard, Gregory G. Spatial Distribution of Amorphization Intensity in Boron Carbide during Rate-Dependent Indentation and Impact Processes.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2016, University of Florida

 Boron carbide is a lightweight ceramic commonly used in applications requiring high hardness. At sufficiently high stresses, the material experiences a localized phase transformation (amorphization)… (more)

Subjects/Keywords: Amorphous materials; Boron; Carbides; Ceramic materials; Compressive stress; Modeling; Raman scattering; Raman spectroscopy; Residual stress; Strain rate; amorphization  – boron  – carbide  – indentation  – raman  – spectroscopy

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Parsard, G. G. (2016). Spatial Distribution of Amorphization Intensity in Boron Carbide during Rate-Dependent Indentation and Impact Processes. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0050729

Chicago Manual of Style (16th Edition):

Parsard, Gregory G. “Spatial Distribution of Amorphization Intensity in Boron Carbide during Rate-Dependent Indentation and Impact Processes.” 2016. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0050729.

MLA Handbook (7th Edition):

Parsard, Gregory G. “Spatial Distribution of Amorphization Intensity in Boron Carbide during Rate-Dependent Indentation and Impact Processes.” 2016. Web. 10 Dec 2019.

Vancouver:

Parsard GG. Spatial Distribution of Amorphization Intensity in Boron Carbide during Rate-Dependent Indentation and Impact Processes. [Internet] [Doctoral dissertation]. University of Florida; 2016. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0050729.

Council of Science Editors:

Parsard GG. Spatial Distribution of Amorphization Intensity in Boron Carbide during Rate-Dependent Indentation and Impact Processes. [Doctoral Dissertation]. University of Florida; 2016. Available from: http://ufdc.ufl.edu/UFE0050729


University of Florida

11. Hart, Adam Benjamin. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.

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

 Natural fliers have shown the capability to utilize unsteady fluid phenomena to increase their flight performance. As engineered vehicles operating in equivalent flight regimes are… (more)

Subjects/Keywords: Aerodynamic lift; Aerodynamics; Aircraft wings; Angle of attack; Flow distribution; Kinematics; Leading edges; Momentum; Unsteady aerodynamics; Velocity; aerodynamics  – piv  – unsteady

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hart, A. B. (2013). Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045179

Chicago Manual of Style (16th Edition):

Hart, Adam Benjamin. “Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.” 2013. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0045179.

MLA Handbook (7th Edition):

Hart, Adam Benjamin. “Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.” 2013. Web. 10 Dec 2019.

Vancouver:

Hart AB. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0045179.

Council of Science Editors:

Hart AB. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045179


University of Florida

12. Babcock, Judson T. Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV.

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

 Some fixed-wing micro air vehicles (MAVs) have high levels of structural flexibility, a property which can change the flight dynamics and control characteristics of the… (more)

Subjects/Keywords: Aircraft; Aircraft roll; Aircraft wings; Bending; Damping; Flight dynamics; Gusts; Natural frequencies; Stiffness; Structural deflection; aeroelastic  – aeroelasticity  – aeroservoelasticity  – aswing  – closed-loop  – elastic-axis  – flight-control  – flight-dynamics  – gust  – lqr  – micro-air-vehicle  – stiffness

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Babcock, J. T. (2013). Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045699

Chicago Manual of Style (16th Edition):

Babcock, Judson T. “Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV.” 2013. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0045699.

MLA Handbook (7th Edition):

Babcock, Judson T. “Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV.” 2013. Web. 10 Dec 2019.

Vancouver:

Babcock JT. Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0045699.

Council of Science Editors:

Babcock JT. Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045699


University of Florida

13. Cantrell, Jason T. Experimental Characterization and Computational Modeling of Unimorph Shape Memory Polymer Actuators Incorporating Transverse Curvature in the Substrate.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2016, University of Florida

 This document outlines in detail the research performed by applying shape memory polymers in a generic unimorph actuator configuration. A set of experiments designed to… (more)

Subjects/Keywords: Aircraft wings; Antennas; Bending; Carbon fibers; Cooling; Curvature; Radius of curvature; Ribs; Shape memory polymers; Structural deflection; actuator  – antenna  – composite  – curvature  – materials  – mav  – memory  – polymer  – satellite  – shape  – smart  – smp  – spring  – tape  – transverse  – unimorph  – wing

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Cantrell, J. T. (2016). Experimental Characterization and Computational Modeling of Unimorph Shape Memory Polymer Actuators Incorporating Transverse Curvature in the Substrate. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0050212

Chicago Manual of Style (16th Edition):

Cantrell, Jason T. “Experimental Characterization and Computational Modeling of Unimorph Shape Memory Polymer Actuators Incorporating Transverse Curvature in the Substrate.” 2016. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0050212.

MLA Handbook (7th Edition):

Cantrell, Jason T. “Experimental Characterization and Computational Modeling of Unimorph Shape Memory Polymer Actuators Incorporating Transverse Curvature in the Substrate.” 2016. Web. 10 Dec 2019.

Vancouver:

Cantrell JT. Experimental Characterization and Computational Modeling of Unimorph Shape Memory Polymer Actuators Incorporating Transverse Curvature in the Substrate. [Internet] [Doctoral dissertation]. University of Florida; 2016. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0050212.

Council of Science Editors:

Cantrell JT. Experimental Characterization and Computational Modeling of Unimorph Shape Memory Polymer Actuators Incorporating Transverse Curvature in the Substrate. [Doctoral Dissertation]. University of Florida; 2016. Available from: http://ufdc.ufl.edu/UFE0050212


University of Florida

14. Sytsma, Michael J. Effects of Turbulence on Fixed Wing Small Unmanned Aerial Systems.

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

 The stability of natural fliers would be an excellent trait to be designed into small unmanned aerial systems. However, there is a great deal of… (more)

Subjects/Keywords: Aircraft; Dynamic loads; Frequency response; Gusts; Reynolds number; Statistics; Throttles; Turbulence; Velocity; Wind tunnels; dynamic  – flow  – free-stream  – image  – loads  – particle  – shear  – structure  – turbulence  – unmanned  – velocimetry

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Sytsma, M. J. (2013). Effects of Turbulence on Fixed Wing Small Unmanned Aerial Systems. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045158

Chicago Manual of Style (16th Edition):

Sytsma, Michael J. “Effects of Turbulence on Fixed Wing Small Unmanned Aerial Systems.” 2013. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0045158.

MLA Handbook (7th Edition):

Sytsma, Michael J. “Effects of Turbulence on Fixed Wing Small Unmanned Aerial Systems.” 2013. Web. 10 Dec 2019.

Vancouver:

Sytsma MJ. Effects of Turbulence on Fixed Wing Small Unmanned Aerial Systems. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0045158.

Council of Science Editors:

Sytsma MJ. Effects of Turbulence on Fixed Wing Small Unmanned Aerial Systems. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045158

15. Chang, Kelvin T. Design of Flapping Wings for Application to Single Active Degree of Freedom Micro Air Vehicles.

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

 This dissertation covers an experimental program to understand how wing compliance influences the performance of flapping micro air vehicle wings. The focus is the design… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Centroids; Design optimization; Distance functions; Insects; Leading edges; Manufacturing processes; Stiffness; Structural deflection; flapping  – hover  – optimization  – stiffness  – uav  – wing

…Dissertation Presented to the Graduate School of the University of Florida in Partial Fulfillment of… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chang, K. T. (2015). Design of Flapping Wings for Application to Single Active Degree of Freedom Micro Air Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0047701

Chicago Manual of Style (16th Edition):

Chang, Kelvin T. “Design of Flapping Wings for Application to Single Active Degree of Freedom Micro Air Vehicles.” 2015. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0047701.

MLA Handbook (7th Edition):

Chang, Kelvin T. “Design of Flapping Wings for Application to Single Active Degree of Freedom Micro Air Vehicles.” 2015. Web. 10 Dec 2019.

Vancouver:

Chang KT. Design of Flapping Wings for Application to Single Active Degree of Freedom Micro Air Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2015. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0047701.

Council of Science Editors:

Chang KT. Design of Flapping Wings for Application to Single Active Degree of Freedom Micro Air Vehicles. [Doctoral Dissertation]. University of Florida; 2015. Available from: http://ufdc.ufl.edu/UFE0047701

16. Allison, Bryan. Evolution of Mechanical Properties of M50 Bearing Steel Due to Rolling Contact Fatigue.

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

 Current bearing life models significantly under predict the life of bearings made of modern ultra-clean steels.  New life models that include the constitutive response of… (more)

Subjects/Keywords: Chemicals; Etching; Hardness; Mechanical bearings; Residual stress; Specimens; Steels; Stress functions; Stress tests; Yield strength; bearing  – fatigue  – rolling  – strength

…Graduate School of the University of Florida in Partial Fulfillment of the Requirements for the… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Allison, B. (2013). Evolution of Mechanical Properties of M50 Bearing Steel Due to Rolling Contact Fatigue. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046077

Chicago Manual of Style (16th Edition):

Allison, Bryan. “Evolution of Mechanical Properties of M50 Bearing Steel Due to Rolling Contact Fatigue.” 2013. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0046077.

MLA Handbook (7th Edition):

Allison, Bryan. “Evolution of Mechanical Properties of M50 Bearing Steel Due to Rolling Contact Fatigue.” 2013. Web. 10 Dec 2019.

Vancouver:

Allison B. Evolution of Mechanical Properties of M50 Bearing Steel Due to Rolling Contact Fatigue. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0046077.

Council of Science Editors:

Allison B. Evolution of Mechanical Properties of M50 Bearing Steel Due to Rolling Contact Fatigue. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0046077


University of Florida

17. Ewin, Jeffrey J. Tribology of Polytetrafluoroethylene and Alumina Composites in Varying Vacuum Pressures.

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

Subjects/Keywords: Coefficient of friction; Composite materials; Friction; Polymers; Pressure; Sliding; Solid lubricants; Stainless steels; Tribology; Vacuum; environment; polytetrafluoroethylene; vacuum

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ewin, J. J. (2013). Tribology of Polytetrafluoroethylene and Alumina Composites in Varying Vacuum Pressures. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045457

Chicago Manual of Style (16th Edition):

Ewin, Jeffrey J. “Tribology of Polytetrafluoroethylene and Alumina Composites in Varying Vacuum Pressures.” 2013. Masters Thesis, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0045457.

MLA Handbook (7th Edition):

Ewin, Jeffrey J. “Tribology of Polytetrafluoroethylene and Alumina Composites in Varying Vacuum Pressures.” 2013. Web. 10 Dec 2019.

Vancouver:

Ewin JJ. Tribology of Polytetrafluoroethylene and Alumina Composites in Varying Vacuum Pressures. [Internet] [Masters thesis]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0045457.

Council of Science Editors:

Ewin JJ. Tribology of Polytetrafluoroethylene and Alumina Composites in Varying Vacuum Pressures. [Masters Thesis]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045457


University of Florida

18. Wilkes, John R. An Energy Flow Approach to Progressive Collapse.

Degree: PhD, Civil Engineering - Civil and Coastal Engineering, 2016, University of Florida

Subjects/Keywords: blast; building; collapse; energy; flow; ls-dyna; mid-rise; progressive; steel

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Wilkes, J. R. (2016). An Energy Flow Approach to Progressive Collapse. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0050301

Chicago Manual of Style (16th Edition):

Wilkes, John R. “An Energy Flow Approach to Progressive Collapse.” 2016. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0050301.

MLA Handbook (7th Edition):

Wilkes, John R. “An Energy Flow Approach to Progressive Collapse.” 2016. Web. 10 Dec 2019.

Vancouver:

Wilkes JR. An Energy Flow Approach to Progressive Collapse. [Internet] [Doctoral dissertation]. University of Florida; 2016. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0050301.

Council of Science Editors:

Wilkes JR. An Energy Flow Approach to Progressive Collapse. [Doctoral Dissertation]. University of Florida; 2016. Available from: http://ufdc.ufl.edu/UFE0050301


University of Florida

19. Brenkus, Natassia Rae. Ultimate Strength of Post-Tensioned Girders with Mixed Bonded and Unbonded Prestressing.

Degree: PhD, Civil Engineering - Civil and Coastal Engineering, 2016, University of Florida

Subjects/Keywords: bridge; concrete; post-tensioning; prestressed; unbonded; wax

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Brenkus, N. R. (2016). Ultimate Strength of Post-Tensioned Girders with Mixed Bonded and Unbonded Prestressing. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0050659

Chicago Manual of Style (16th Edition):

Brenkus, Natassia Rae. “Ultimate Strength of Post-Tensioned Girders with Mixed Bonded and Unbonded Prestressing.” 2016. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0050659.

MLA Handbook (7th Edition):

Brenkus, Natassia Rae. “Ultimate Strength of Post-Tensioned Girders with Mixed Bonded and Unbonded Prestressing.” 2016. Web. 10 Dec 2019.

Vancouver:

Brenkus NR. Ultimate Strength of Post-Tensioned Girders with Mixed Bonded and Unbonded Prestressing. [Internet] [Doctoral dissertation]. University of Florida; 2016. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0050659.

Council of Science Editors:

Brenkus NR. Ultimate Strength of Post-Tensioned Girders with Mixed Bonded and Unbonded Prestressing. [Doctoral Dissertation]. University of Florida; 2016. Available from: http://ufdc.ufl.edu/UFE0050659


University of Florida

20. Davis, Brian M. Study of the Dynamic Material Behavior and Its Correlation to the Chip Formation Mechanism and Chip Morphology during Machining.

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

Subjects/Keywords: dic; johnson-cook; machining; mechanism; morphology

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Davis, B. M. (2017). Study of the Dynamic Material Behavior and Its Correlation to the Chip Formation Mechanism and Chip Morphology during Machining. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0051023

Chicago Manual of Style (16th Edition):

Davis, Brian M. “Study of the Dynamic Material Behavior and Its Correlation to the Chip Formation Mechanism and Chip Morphology during Machining.” 2017. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0051023.

MLA Handbook (7th Edition):

Davis, Brian M. “Study of the Dynamic Material Behavior and Its Correlation to the Chip Formation Mechanism and Chip Morphology during Machining.” 2017. Web. 10 Dec 2019.

Vancouver:

Davis BM. Study of the Dynamic Material Behavior and Its Correlation to the Chip Formation Mechanism and Chip Morphology during Machining. [Internet] [Doctoral dissertation]. University of Florida; 2017. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0051023.

Council of Science Editors:

Davis BM. Study of the Dynamic Material Behavior and Its Correlation to the Chip Formation Mechanism and Chip Morphology during Machining. [Doctoral Dissertation]. University of Florida; 2017. Available from: http://ufdc.ufl.edu/UFE0051023


University of Florida

21. Paulson, Christopher R. Utilizing Glint Phenomenology to Perform Classification of Civilian Vehicle Using Synthetic Aperture Radar.

Degree: PhD, Electrical and Computer Engineering, 2013, University of Florida

Subjects/Keywords: Bandwidth; Civilian personnel; Geometric angles; Geometrical optics; Image classification; Pixels; Radar; Sensors; Signals; Term weighting; classification; cvdomes; database; glrt; gotcha; optics; pose; sar

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Paulson, C. R. (2013). Utilizing Glint Phenomenology to Perform Classification of Civilian Vehicle Using Synthetic Aperture Radar. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045195

Chicago Manual of Style (16th Edition):

Paulson, Christopher R. “Utilizing Glint Phenomenology to Perform Classification of Civilian Vehicle Using Synthetic Aperture Radar.” 2013. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0045195.

MLA Handbook (7th Edition):

Paulson, Christopher R. “Utilizing Glint Phenomenology to Perform Classification of Civilian Vehicle Using Synthetic Aperture Radar.” 2013. Web. 10 Dec 2019.

Vancouver:

Paulson CR. Utilizing Glint Phenomenology to Perform Classification of Civilian Vehicle Using Synthetic Aperture Radar. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0045195.

Council of Science Editors:

Paulson CR. Utilizing Glint Phenomenology to Perform Classification of Civilian Vehicle Using Synthetic Aperture Radar. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045195


University of Florida

22. Burgess, Matthew A. Small Unmanned Aircraft Systems and Their Payloads as Aerial Data Collection Platforms for Natural Resource-Based Applications.

Degree: PhD, Wildlife Ecology and Conservation, 2017, University of Florida

Subjects/Keywords: suas; unmanned

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Burgess, M. A. (2017). Small Unmanned Aircraft Systems and Their Payloads as Aerial Data Collection Platforms for Natural Resource-Based Applications. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0051051

Chicago Manual of Style (16th Edition):

Burgess, Matthew A. “Small Unmanned Aircraft Systems and Their Payloads as Aerial Data Collection Platforms for Natural Resource-Based Applications.” 2017. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0051051.

MLA Handbook (7th Edition):

Burgess, Matthew A. “Small Unmanned Aircraft Systems and Their Payloads as Aerial Data Collection Platforms for Natural Resource-Based Applications.” 2017. Web. 10 Dec 2019.

Vancouver:

Burgess MA. Small Unmanned Aircraft Systems and Their Payloads as Aerial Data Collection Platforms for Natural Resource-Based Applications. [Internet] [Doctoral dissertation]. University of Florida; 2017. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0051051.

Council of Science Editors:

Burgess MA. Small Unmanned Aircraft Systems and Their Payloads as Aerial Data Collection Platforms for Natural Resource-Based Applications. [Doctoral Dissertation]. University of Florida; 2017. Available from: http://ufdc.ufl.edu/UFE0051051


University of Florida

23. Draa, Phillip M. The Heat Treatment and Evaluation of Single Crystal Nickel Base Superalloys for Industrial Gas Turbine Applications.

Degree: PhD, Materials Science and Engineering, 2013, University of Florida

Subjects/Keywords: Alloys; Carbides; Dendrites; Eutectics; Heat resistant alloys; Heat treatment; Material concentration; Melting; Porosity; Single crystals; boron; carbide; carbon; cmsx-486; cmsx-8b-c; crystal; dendrite; dissolution; dsc; epma; eutectic; gas; heat; homogenization; igt; incipient; kirkendall; melting; microsegregation; ni-base; porosity; pwa1484; rhenium; segregation; single; solidification; solution; strain-assisted; stress-relief; superalloy; treatment; turbine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Draa, P. M. (2013). The Heat Treatment and Evaluation of Single Crystal Nickel Base Superalloys for Industrial Gas Turbine Applications. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046312

Chicago Manual of Style (16th Edition):

Draa, Phillip M. “The Heat Treatment and Evaluation of Single Crystal Nickel Base Superalloys for Industrial Gas Turbine Applications.” 2013. Doctoral Dissertation, University of Florida. Accessed December 10, 2019. http://ufdc.ufl.edu/UFE0046312.

MLA Handbook (7th Edition):

Draa, Phillip M. “The Heat Treatment and Evaluation of Single Crystal Nickel Base Superalloys for Industrial Gas Turbine Applications.” 2013. Web. 10 Dec 2019.

Vancouver:

Draa PM. The Heat Treatment and Evaluation of Single Crystal Nickel Base Superalloys for Industrial Gas Turbine Applications. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Dec 10]. Available from: http://ufdc.ufl.edu/UFE0046312.

Council of Science Editors:

Draa PM. The Heat Treatment and Evaluation of Single Crystal Nickel Base Superalloys for Industrial Gas Turbine Applications. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0046312

.