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You searched for +publisher:"University of Florida" +contributor:("Ifju, Peter "). Showing records 1 – 30 of 80 total matches.

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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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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. Mc Intire, Justin D. Investigating Torsional Compliance of Flapping Wings to Maximize Thrust Capability.

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

 This work involves maximizing the thrust capability of small flapping wings. The motivation of this work is to create a wing with a particular architecture… (more)

Subjects/Keywords: Aircraft wings; Bending; Boxes; Carbon fibers; Centroids; Digital images; Leading edges; Modeling; Stiffness; Wing flaps

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APA (6th Edition):

Mc Intire, J. D. (2011). Investigating Torsional Compliance of Flapping Wings to Maximize Thrust Capability. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043808

Chicago Manual of Style (16th Edition):

Mc Intire, Justin D. “Investigating Torsional Compliance of Flapping Wings to Maximize Thrust Capability.” 2011. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0043808.

MLA Handbook (7th Edition):

Mc Intire, Justin D. “Investigating Torsional Compliance of Flapping Wings to Maximize Thrust Capability.” 2011. Web. 18 Oct 2019.

Vancouver:

Mc Intire JD. Investigating Torsional Compliance of Flapping Wings to Maximize Thrust Capability. [Internet] [Masters thesis]. University of Florida; 2011. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0043808.

Council of Science Editors:

Mc Intire JD. Investigating Torsional Compliance of Flapping Wings to Maximize Thrust Capability. [Masters Thesis]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043808


University of Florida

3. Lee, Myong Hwa. Work Hardening Response of Case Hardened M50nil Steel Induced by Rolling Contact Fatigue.

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

 This study focused on investigation of the fundamental characteristics of M50NiL and its responses to Rolling Contact Fatigue (RCF). The carbon gradient caused by carburizing… (more)

Subjects/Keywords: Austenite; Carbides; Carbon; Etching; Hardness; Martensite; Material hardening; Specimens; Steels; Work hardening; case-hardened-steel  – m50nil  – rolling-contact-fatigue  – work-hardening

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APA (6th Edition):

Lee, M. H. (2012). Work Hardening Response of Case Hardened M50nil Steel Induced by Rolling Contact Fatigue. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044150

Chicago Manual of Style (16th Edition):

Lee, Myong Hwa. “Work Hardening Response of Case Hardened M50nil Steel Induced by Rolling Contact Fatigue.” 2012. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0044150.

MLA Handbook (7th Edition):

Lee, Myong Hwa. “Work Hardening Response of Case Hardened M50nil Steel Induced by Rolling Contact Fatigue.” 2012. Web. 18 Oct 2019.

Vancouver:

Lee MH. Work Hardening Response of Case Hardened M50nil Steel Induced by Rolling Contact Fatigue. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0044150.

Council of Science Editors:

Lee MH. Work Hardening Response of Case Hardened M50nil Steel Induced by Rolling Contact Fatigue. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044150


University of Florida

4. Bonsmann, Jarrod. Finite Element Analysis for Use in Fluid Structure Interaction of a High Aspect Ratio Thin Airfoil using Drop-Plies.

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

 Abstract of Thesis Presented to the Graduate School of the University of Florida in Partial Fulfillment of the Requirements for the Degree of Master of… (more)

Subjects/Keywords: Aluminum; Bending; Composite materials; Eggshells; Material properties; Modeling; Specimens; Strain gauges; Structural deflection; Wind surfing; avl, fea, vic

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APA (6th Edition):

Bonsmann, J. (2010). Finite Element Analysis for Use in Fluid Structure Interaction of a High Aspect Ratio Thin Airfoil using Drop-Plies. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041819

Chicago Manual of Style (16th Edition):

Bonsmann, Jarrod. “Finite Element Analysis for Use in Fluid Structure Interaction of a High Aspect Ratio Thin Airfoil using Drop-Plies.” 2010. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0041819.

MLA Handbook (7th Edition):

Bonsmann, Jarrod. “Finite Element Analysis for Use in Fluid Structure Interaction of a High Aspect Ratio Thin Airfoil using Drop-Plies.” 2010. Web. 18 Oct 2019.

Vancouver:

Bonsmann J. Finite Element Analysis for Use in Fluid Structure Interaction of a High Aspect Ratio Thin Airfoil using Drop-Plies. [Internet] [Masters thesis]. University of Florida; 2010. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0041819.

Council of Science Editors:

Bonsmann J. Finite Element Analysis for Use in Fluid Structure Interaction of a High Aspect Ratio Thin Airfoil using Drop-Plies. [Masters Thesis]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0041819


University of Florida

5. 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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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

6. 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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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

7. Evers, Brandon S. Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications.

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

 Aerial photogrammetry is traditionally a specialized application for small manned aircraft with large operating expenses. Emerging small unmanned aerial systems (sUAS) have the capability to… (more)

Subjects/Keywords: Aircraft wings; Airfoil camber; Airspeed; Cruises; Fuselages; Payloads; Remote sensing; Remotely piloted vehicles; Takeoff; Wing flaps; aerial  – aircraft  – autonomous  – flight  – photogrammetry  – planning  – remote  – sensing  – systems  – uas  – uav  – unmanned

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APA (6th Edition):

Evers, B. S. (2011). Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043857

Chicago Manual of Style (16th Edition):

Evers, Brandon S. “Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications.” 2011. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0043857.

MLA Handbook (7th Edition):

Evers, Brandon S. “Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications.” 2011. Web. 18 Oct 2019.

Vancouver:

Evers BS. Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications. [Internet] [Masters thesis]. University of Florida; 2011. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0043857.

Council of Science Editors:

Evers BS. Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications. [Masters Thesis]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043857


University of Florida

8. 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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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

9. Campos, Diego G. Effects of Isotropic Flexibility on Wings under a Plunging Motion.

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

 In recent years there has been an interest in studying and understanding natural flyers to incorporate some of their features into small engineered flying systems.… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Bending; Flexible wings; Kinematics; Lasers; Momentum; Stiffness; Velocity; Vorticity; bio-inspired  – flexibility  – fluid-structure  – interaction  – piv  – plunging

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APA (6th Edition):

Campos, D. G. (2012). Effects of Isotropic Flexibility on Wings under a Plunging Motion. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044213

Chicago Manual of Style (16th Edition):

Campos, Diego G. “Effects of Isotropic Flexibility on Wings under a Plunging Motion.” 2012. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0044213.

MLA Handbook (7th Edition):

Campos, Diego G. “Effects of Isotropic Flexibility on Wings under a Plunging Motion.” 2012. Web. 18 Oct 2019.

Vancouver:

Campos DG. Effects of Isotropic Flexibility on Wings under a Plunging Motion. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0044213.

Council of Science Editors:

Campos DG. Effects of Isotropic Flexibility on Wings under a Plunging Motion. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044213


University of Florida

10. Nadel, Adam. A Comparison of an Integrally Stiffened Beaded Panel Made From Stretch Broken Carbon Fiber and a Honeycomb Core Sandwich Panel.

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

 Honeycomb core sandwich panels are commonly used in aircraft construction. They provide a buckling-resistant, lighter-weight alternative to the classic skin and stringer aircraft construction. However,… (more)

Subjects/Keywords: Aircraft; Carbon fibers; Corrosion; Geometry; Honeycomb cores; Honeycombs; Laminates; Sandwiches; Skin; Structural deflection; aircraft, bead, broken, carbon, composite, core, corrosion, fiber, honeycomb, panel, sandwich, sbcf, skin, stretch

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APA (6th Edition):

Nadel, A. (2009). A Comparison of an Integrally Stiffened Beaded Panel Made From Stretch Broken Carbon Fiber and a Honeycomb Core Sandwich Panel. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041283

Chicago Manual of Style (16th Edition):

Nadel, Adam. “A Comparison of an Integrally Stiffened Beaded Panel Made From Stretch Broken Carbon Fiber and a Honeycomb Core Sandwich Panel.” 2009. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0041283.

MLA Handbook (7th Edition):

Nadel, Adam. “A Comparison of an Integrally Stiffened Beaded Panel Made From Stretch Broken Carbon Fiber and a Honeycomb Core Sandwich Panel.” 2009. Web. 18 Oct 2019.

Vancouver:

Nadel A. A Comparison of an Integrally Stiffened Beaded Panel Made From Stretch Broken Carbon Fiber and a Honeycomb Core Sandwich Panel. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0041283.

Council of Science Editors:

Nadel A. A Comparison of an Integrally Stiffened Beaded Panel Made From Stretch Broken Carbon Fiber and a Honeycomb Core Sandwich Panel. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0041283


University of Florida

11. Abudaram, Yaakov. Wind Tunnel Testing of Load-Alleviating Membrane Wings.

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

 This work is concerned with wind tunnel testing of elastic latex and silicone membrane wings intended for micro air vehicles. Erratic flow conditions are a… (more)

Subjects/Keywords: Aircraft wings; Bending; Carbon fibers; Geometric angles; Images; Rigid wings; Silicones; Stall; Trailing edges; Wind tunnels; aerodynamic, aeroelastic, alleviating, anisotropic, attack, batten, camber, carbon, chord, deformation, drag, elongation, epoxy, fiber, hyperelastic, latex, leading, lift, mav, membrane, mold, pitching, reynolds, scallop, silicone, stall, sting, trailing, tunnel, vic, vortex, wind, wing

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APA (6th Edition):

Abudaram, Y. (2009). Wind Tunnel Testing of Load-Alleviating Membrane Wings. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041340

Chicago Manual of Style (16th Edition):

Abudaram, Yaakov. “Wind Tunnel Testing of Load-Alleviating Membrane Wings.” 2009. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0041340.

MLA Handbook (7th Edition):

Abudaram, Yaakov. “Wind Tunnel Testing of Load-Alleviating Membrane Wings.” 2009. Web. 18 Oct 2019.

Vancouver:

Abudaram Y. Wind Tunnel Testing of Load-Alleviating Membrane Wings. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0041340.

Council of Science Editors:

Abudaram Y. Wind Tunnel Testing of Load-Alleviating Membrane Wings. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0041340


University of Florida

12. Love, Robert. Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles.

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

 Flapping-wing micro air-vehicles are being investigated for their potential to provide enhanced aerodynamic efficiency, maneuverability and gust tolerance. The flight dynamics of flapping-wing micro air-vehicles… (more)

Subjects/Keywords: Aircraft wings; Amplitude; Dynamic structural analysis; Fourier transformations; Polynomials; Signals; Structural deflection; Trailing edges; Velocity; Wavelet analysis; aerial, aeroelastic, aeroservoelastic, aerospace, analysis, correlation, deflection, deformation, dic, digital, doppler, dynamics, engineer, flapping, fourier, ground, gvt, image, laser, ldv, mav, modal, mode, model, ornithopter, processing, signal, testing, uav, unmanned, vehicle, vibration, vibrometer, wavelet, wing

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APA (6th Edition):

Love, R. (2009). Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024479

Chicago Manual of Style (16th Edition):

Love, Robert. “Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles.” 2009. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0024479.

MLA Handbook (7th Edition):

Love, Robert. “Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles.” 2009. Web. 18 Oct 2019.

Vancouver:

Love R. Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0024479.

Council of Science Editors:

Love R. Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024479


University of Florida

13. Timpe, Amory W. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.

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

 The inherent challenges associated with low Reynolds number flight have stemmed biologically inspired wing designs incorporating highly flexible membranes. Natural membrane wing flyers demonstrate advantages… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Modeling; Momentum; Near wakes; Pixels; Shear layers; Velocity; Vibration; Vorticity; compliant  – dic  – flexible  – fluid-structure  – fsi  – mav  – membrane  – piv  – reynolds  – wing

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APA (6th Edition):

Timpe, A. W. (2012). Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044220

Chicago Manual of Style (16th Edition):

Timpe, Amory W. “Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.” 2012. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0044220.

MLA Handbook (7th Edition):

Timpe, Amory W. “Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.” 2012. Web. 18 Oct 2019.

Vancouver:

Timpe AW. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0044220.

Council of Science Editors:

Timpe AW. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044220


University of Florida

14. Jagdale, Vijay. Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing.

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

 Demand for deployable MAVs and UAVs with wings designed to reduce aircraft storage volume led to the development of a bendable wing concept at the… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Airfoil camber; Airfoils; Buckling; Design optimization; Modeling; Remotely piloted vehicles; Sweepback; Velocity; aircraft, bendable, buckling, compact, compliant, design, experimental, foldable, mav, optimization, storage, uav, unmanned, wing

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APA (6th Edition):

Jagdale, V. (2010). Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042430

Chicago Manual of Style (16th Edition):

Jagdale, Vijay. “Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing.” 2010. Doctoral Dissertation, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0042430.

MLA Handbook (7th Edition):

Jagdale, Vijay. “Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing.” 2010. Web. 18 Oct 2019.

Vancouver:

Jagdale V. Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0042430.

Council of Science Editors:

Jagdale V. Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0042430


University of Florida

15. Marchman, Kellon Ryan. In Situ Investigation of Sliding Direction Dependency on the Wear of Single Crystal Magnesium Oxide.

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

 Ionic solids are unique materials to study, offering a wide range of physical properties and varying crystallographic tendencies. Amongst this group is magnesium oxide (MgO).… (more)

Subjects/Keywords: Coefficient of friction; Friction; Ions; Magnesium compounds; Shear stress; Single crystals; Sliding; Stiffness; Tribology; Tribometers; crystal  – mgo  – wear

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APA (6th Edition):

Marchman, K. R. (2012). In Situ Investigation of Sliding Direction Dependency on the Wear of Single Crystal Magnesium Oxide. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044271

Chicago Manual of Style (16th Edition):

Marchman, Kellon Ryan. “In Situ Investigation of Sliding Direction Dependency on the Wear of Single Crystal Magnesium Oxide.” 2012. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0044271.

MLA Handbook (7th Edition):

Marchman, Kellon Ryan. “In Situ Investigation of Sliding Direction Dependency on the Wear of Single Crystal Magnesium Oxide.” 2012. Web. 18 Oct 2019.

Vancouver:

Marchman KR. In Situ Investigation of Sliding Direction Dependency on the Wear of Single Crystal Magnesium Oxide. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0044271.

Council of Science Editors:

Marchman KR. In Situ Investigation of Sliding Direction Dependency on the Wear of Single Crystal Magnesium Oxide. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044271


University of Florida

16. Li,Shi. A Molecular Dynamics Study on Cellulose Fiber Reinforced Nanocomposite.

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

 Wood has a hierarchical structure, whose macroscopic properties emerge from their micro- and nanostructural level. In micro- or nano-scale, the mechanical properties of cell wall… (more)

Subjects/Keywords: Atomic interactions; Atoms; Cell walls; Cells; Force field; Matrices; Modeling; Plant cells; Simulations; Software; celluloe  – hemicellulose  – md  – mfa

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APA (6th Edition):

Li,Shi. (2011). A Molecular Dynamics Study on Cellulose Fiber Reinforced Nanocomposite. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043441

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

Chicago Manual of Style (16th Edition):

Li,Shi. “A Molecular Dynamics Study on Cellulose Fiber Reinforced Nanocomposite.” 2011. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0043441.

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

MLA Handbook (7th Edition):

Li,Shi. “A Molecular Dynamics Study on Cellulose Fiber Reinforced Nanocomposite.” 2011. Web. 18 Oct 2019.

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

Vancouver:

Li,Shi. A Molecular Dynamics Study on Cellulose Fiber Reinforced Nanocomposite. [Internet] [Masters thesis]. University of Florida; 2011. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0043441.

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

Council of Science Editors:

Li,Shi. A Molecular Dynamics Study on Cellulose Fiber Reinforced Nanocomposite. [Masters Thesis]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043441

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


University of Florida

17. Ferraro, Christopher. Determination of Test Methods for the Prediction of the Behavior of Mass Concrete.

Degree: PhD, Civil Engineering - Civil and Coastal Engineering, 2009, University of Florida

 Hydration at early ages results from chemical and physical processes that take place between Portland cement and water, and is an exothermic process. The resultant… (more)

Subjects/Keywords: Cements; Compressive strength; Fly ash; Heat; Heat measurement; Hydraulic cements; Moduli of elasticity; Mortars; Slag; Specimens; calorimetry, concrete, heat, hydration, isothermal, mass, modulus, semi, strength

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APA (6th Edition):

Ferraro, C. (2009). Determination of Test Methods for the Prediction of the Behavior of Mass Concrete. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041062

Chicago Manual of Style (16th Edition):

Ferraro, Christopher. “Determination of Test Methods for the Prediction of the Behavior of Mass Concrete.” 2009. Doctoral Dissertation, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0041062.

MLA Handbook (7th Edition):

Ferraro, Christopher. “Determination of Test Methods for the Prediction of the Behavior of Mass Concrete.” 2009. Web. 18 Oct 2019.

Vancouver:

Ferraro C. Determination of Test Methods for the Prediction of the Behavior of Mass Concrete. [Internet] [Doctoral dissertation]. University of Florida; 2009. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0041062.

Council of Science Editors:

Ferraro C. Determination of Test Methods for the Prediction of the Behavior of Mass Concrete. [Doctoral Dissertation]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0041062


University of Florida

18. 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

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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 October 18, 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. 18 Oct 2019.

Vancouver:

Lin A. Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 18]. 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

19. 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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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

20. 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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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

21. Johnson, Baron. High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail.

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

 The angle-of-attack parameter has a significant influence on the aerodynamics, flight dynamics, and handling qualities of aircraft. Flight at high angle-of-attack conditions enables many missions;… (more)

Subjects/Keywords: Ailerons; Aircraft; Aircraft pitch; Aircraft roll; Flight stabilizers; Signals; Structural deflection; Vehicular flight; Wavelet analysis; Wing rock; 3d, aircraft, alpha, angle, attack, baron, harrier, high, inverted, lind, mav, of, rc, rock, showtime, tail, uav, upright, vertical, wing

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APA (6th Edition):

Johnson, B. (2009). High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024449

Chicago Manual of Style (16th Edition):

Johnson, Baron. “High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail.” 2009. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0024449.

MLA Handbook (7th Edition):

Johnson, Baron. “High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail.” 2009. Web. 18 Oct 2019.

Vancouver:

Johnson B. High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0024449.

Council of Science Editors:

Johnson B. High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024449


University of Florida

22. 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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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

23. 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

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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 October 18, 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. 18 Oct 2019.

Vancouver:

Villanueva DC. Reliability Based Design Including Future Tests and Multi-Agent Approaches. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Oct 18]. 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

24. Patil, Abhishek. Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing.

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

 The bendable UAV wing developed by researchers at the University of Florida has the ability to load stiffen in the positive load direction and at… (more)

Subjects/Keywords: Aircraft wings; Airfoil camber; Airfoils; Buckling; Eigenvalues; Load carrying capacity; Modeling; Remotely piloted vehicles; Structural deflection; Velocity; abhishek, analysis, bendable, buckling, expermiental, ifju, mav, patil, predictor, stress, tool, uav, ufl

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APA (6th Edition):

Patil, A. (2009). Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0025037

Chicago Manual of Style (16th Edition):

Patil, Abhishek. “Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing.” 2009. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0025037.

MLA Handbook (7th Edition):

Patil, Abhishek. “Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing.” 2009. Web. 18 Oct 2019.

Vancouver:

Patil A. Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0025037.

Council of Science Editors:

Patil A. Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0025037


University of Florida

25. Perry, John. A Synthesized Directly Georeferenced Remote Sensing Technique for Small Unmanned Aerial Vehicles.

Degree: MS, Forest Resources and Conservation, 2009, University of Florida

 Directly georeferenced remote sensing is an emerging technique for rapidly gathering accurate and repeatable observations of the landscape. It refers to the ability to independently… (more)

Subjects/Keywords: Calibration; Coordinate systems; Global positioning systems; Navigation; Payloads; Remote sensing; Remotely piloted vehicles; Sensors; Signals; Sine function; direct, georeferencing, mosaicing, navigation, photogrammetry, remote, sensing, uas, uav

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APA (6th Edition):

Perry, J. (2009). A Synthesized Directly Georeferenced Remote Sensing Technique for Small Unmanned Aerial Vehicles. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0025070

Chicago Manual of Style (16th Edition):

Perry, John. “A Synthesized Directly Georeferenced Remote Sensing Technique for Small Unmanned Aerial Vehicles.” 2009. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0025070.

MLA Handbook (7th Edition):

Perry, John. “A Synthesized Directly Georeferenced Remote Sensing Technique for Small Unmanned Aerial Vehicles.” 2009. Web. 18 Oct 2019.

Vancouver:

Perry J. A Synthesized Directly Georeferenced Remote Sensing Technique for Small Unmanned Aerial Vehicles. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0025070.

Council of Science Editors:

Perry J. A Synthesized Directly Georeferenced Remote Sensing Technique for Small Unmanned Aerial Vehicles. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0025070


University of Florida

26. Roberts, Brian. Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft.

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

 Mission performance for small aircraft is often dependent on turn radius. Various biologically-inspired concepts have demonstrated that performance can be improved by morphing the wings… (more)

Subjects/Keywords: Ailerons; Aircraft; Aircraft roll; Aircraft wings; Center of mass; Elbow joint; Elevators; Flight stabilizers; Sideslip; Structural deflection; dynamics, flight, mav, performance, pterosaur, radius, tail, turn, uav, vertical

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APA (6th Edition):

Roberts, B. (2009). Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024421

Chicago Manual of Style (16th Edition):

Roberts, Brian. “Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft.” 2009. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0024421.

MLA Handbook (7th Edition):

Roberts, Brian. “Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft.” 2009. Web. 18 Oct 2019.

Vancouver:

Roberts B. Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0024421.

Council of Science Editors:

Roberts B. Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024421


University of Florida

27. 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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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

28. Solai Rameshbabu, Vignesh. Mesh Independent Finite Element Analysis of Composite Plates.

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

 Mesh Independent Finite Element Analysis uses geometry that is represented using equations or surface triangles and uses a background mesh to perform analysis. The geometry… (more)

Subjects/Keywords: Bending; Boundary conditions; Composite materials; Eggshells; Finite element method; Geometry; Laminates; Plate theory; Stiffness; Stiffness matrix; composites

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APA (6th Edition):

Solai Rameshbabu, V. (2012). Mesh Independent Finite Element Analysis of Composite Plates. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044354

Chicago Manual of Style (16th Edition):

Solai Rameshbabu, Vignesh. “Mesh Independent Finite Element Analysis of Composite Plates.” 2012. Masters Thesis, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0044354.

MLA Handbook (7th Edition):

Solai Rameshbabu, Vignesh. “Mesh Independent Finite Element Analysis of Composite Plates.” 2012. Web. 18 Oct 2019.

Vancouver:

Solai Rameshbabu V. Mesh Independent Finite Element Analysis of Composite Plates. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0044354.

Council of Science Editors:

Solai Rameshbabu V. Mesh Independent Finite Element Analysis of Composite Plates. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044354


University of Florida

29. 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

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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 October 18, 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. 18 Oct 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 Oct 18]. 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

30. Song, Min Cheol. Effect of Translaminar Reinforcements and Hybridization on Damage Resistance and Tolerance of Composite Laminates.

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

 The effects of translaminar reinforcements (TLR) and hybridization on impact damage resistance and tolerance of laminated composites were analyzed. The TLR increase the apparent fracture… (more)

Subjects/Keywords: Composite materials; Delamination; Fracture strength; Hybrid composites; Laminates; Modeling; Shear stress; Simulations; Woven composites; Yarns; composites  – damage  – fea  – hybridization  – translaminar

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APA (6th Edition):

Song, M. C. (2012). Effect of Translaminar Reinforcements and Hybridization on Damage Resistance and Tolerance of Composite Laminates. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044505

Chicago Manual of Style (16th Edition):

Song, Min Cheol. “Effect of Translaminar Reinforcements and Hybridization on Damage Resistance and Tolerance of Composite Laminates.” 2012. Doctoral Dissertation, University of Florida. Accessed October 18, 2019. http://ufdc.ufl.edu/UFE0044505.

MLA Handbook (7th Edition):

Song, Min Cheol. “Effect of Translaminar Reinforcements and Hybridization on Damage Resistance and Tolerance of Composite Laminates.” 2012. Web. 18 Oct 2019.

Vancouver:

Song MC. Effect of Translaminar Reinforcements and Hybridization on Damage Resistance and Tolerance of Composite Laminates. [Internet] [Doctoral dissertation]. University of Florida; 2012. [cited 2019 Oct 18]. Available from: http://ufdc.ufl.edu/UFE0044505.

Council of Science Editors:

Song MC. Effect of Translaminar Reinforcements and Hybridization on Damage Resistance and Tolerance of Composite Laminates. [Doctoral Dissertation]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044505

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