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You searched for +publisher:"Virginia Tech" +contributor:("Patil, Mayuresh J."). Showing records 1 – 30 of 104 total matches.

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1. Muthirevula, Neeharika. Cross-Sectional Stiffness Properties of Complex Drone Wings.

Degree: MS, Aerospace and Ocean Engineering, 2017, Virginia Tech

 The main purpose of this thesis is to develop a beam element in order to model the wing of a drone, made of composite materials.… (more)

Subjects/Keywords: Composites; Timoshenko beam; Cross-sectional Analysis; Drones; stress recovery; strain recovery.

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APA (6th Edition):

Muthirevula, N. (2017). Cross-Sectional Stiffness Properties of Complex Drone Wings. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/73988

Chicago Manual of Style (16th Edition):

Muthirevula, Neeharika. “Cross-Sectional Stiffness Properties of Complex Drone Wings.” 2017. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/73988.

MLA Handbook (7th Edition):

Muthirevula, Neeharika. “Cross-Sectional Stiffness Properties of Complex Drone Wings.” 2017. Web. 26 Feb 2020.

Vancouver:

Muthirevula N. Cross-Sectional Stiffness Properties of Complex Drone Wings. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/73988.

Council of Science Editors:

Muthirevula N. Cross-Sectional Stiffness Properties of Complex Drone Wings. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/73988

2. Burns, Meghan Colleen. Safety of Flight Prediction for Small Unmanned Aerial Vehicles Using Dynamic Bayesian Networks.

Degree: MS, Aerospace and Ocean Engineering, 2018, Virginia Tech

 This thesis compares three variations of the Bayesian network as an aid for decision-making using uncertain information. After reviewing the basic theory underlying probabilistic graphical… (more)

Subjects/Keywords: Dynamic Bayesian Network; Unmanned Aerial Systems; Risk

…Problem Virginia Tech student pilots frequently fly small unmanned aerial systems (sUAS… 

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APA (6th Edition):

Burns, M. C. (2018). Safety of Flight Prediction for Small Unmanned Aerial Vehicles Using Dynamic Bayesian Networks. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/83381

Chicago Manual of Style (16th Edition):

Burns, Meghan Colleen. “Safety of Flight Prediction for Small Unmanned Aerial Vehicles Using Dynamic Bayesian Networks.” 2018. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/83381.

MLA Handbook (7th Edition):

Burns, Meghan Colleen. “Safety of Flight Prediction for Small Unmanned Aerial Vehicles Using Dynamic Bayesian Networks.” 2018. Web. 26 Feb 2020.

Vancouver:

Burns MC. Safety of Flight Prediction for Small Unmanned Aerial Vehicles Using Dynamic Bayesian Networks. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/83381.

Council of Science Editors:

Burns MC. Safety of Flight Prediction for Small Unmanned Aerial Vehicles Using Dynamic Bayesian Networks. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/83381

3. Clark, Patrick Ryan. Reliability-Based Topology Optimization with Analytic Sensitivities.

Degree: MS, Aerospace and Ocean Engineering, 2017, Virginia Tech

 It is a common practice when designing a system to apply safety factors to the critical failure load or event. These safety factors provide a… (more)

Subjects/Keywords: Reliability-Based Topology Optimization; First-Order Reliability Method; Sensitivity Analysis

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APA (6th Edition):

Clark, P. R. (2017). Reliability-Based Topology Optimization with Analytic Sensitivities. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78665

Chicago Manual of Style (16th Edition):

Clark, Patrick Ryan. “Reliability-Based Topology Optimization with Analytic Sensitivities.” 2017. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/78665.

MLA Handbook (7th Edition):

Clark, Patrick Ryan. “Reliability-Based Topology Optimization with Analytic Sensitivities.” 2017. Web. 26 Feb 2020.

Vancouver:

Clark PR. Reliability-Based Topology Optimization with Analytic Sensitivities. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/78665.

Council of Science Editors:

Clark PR. Reliability-Based Topology Optimization with Analytic Sensitivities. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/78665

4. Olson, Nicholai Kenneth Keeney. Validation and Uncertainty Quantification of Doublet Lattice Flight Loads using Flight Test Data.

Degree: MS, Aerospace and Ocean Engineering, 2018, Virginia Tech

 This paper presents a framework for tuning, validating, and quantifying uncertainties for flight loads. The flight loads are computed using a Nastran doublet lattice model… (more)

Subjects/Keywords: Loads; Doublet Lattice; Validation; Uncertainty Quantification

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APA (6th Edition):

Olson, N. K. K. (2018). Validation and Uncertainty Quantification of Doublet Lattice Flight Loads using Flight Test Data. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/84345

Chicago Manual of Style (16th Edition):

Olson, Nicholai Kenneth Keeney. “Validation and Uncertainty Quantification of Doublet Lattice Flight Loads using Flight Test Data.” 2018. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/84345.

MLA Handbook (7th Edition):

Olson, Nicholai Kenneth Keeney. “Validation and Uncertainty Quantification of Doublet Lattice Flight Loads using Flight Test Data.” 2018. Web. 26 Feb 2020.

Vancouver:

Olson NKK. Validation and Uncertainty Quantification of Doublet Lattice Flight Loads using Flight Test Data. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/84345.

Council of Science Editors:

Olson NKK. Validation and Uncertainty Quantification of Doublet Lattice Flight Loads using Flight Test Data. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/84345

5. Albertson, Nicholas James. Mechanical and Electromagnetic Optimization of Structurally Embedded Waveguide Antennas.

Degree: MS, Aerospace and Ocean Engineering, 2018, Virginia Tech

 Use of Slotted Waveguide Antenna Stiffened Structures (SWASS) in future commercial and military aircraft calls for the development of an airworthiness certification procedure. The first… (more)

Subjects/Keywords: SWASS; structurally embedded antennas; multi-fidelity modeling; phased arrays

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APA (6th Edition):

Albertson, N. J. (2018). Mechanical and Electromagnetic Optimization of Structurally Embedded Waveguide Antennas. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/81959

Chicago Manual of Style (16th Edition):

Albertson, Nicholas James. “Mechanical and Electromagnetic Optimization of Structurally Embedded Waveguide Antennas.” 2018. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/81959.

MLA Handbook (7th Edition):

Albertson, Nicholas James. “Mechanical and Electromagnetic Optimization of Structurally Embedded Waveguide Antennas.” 2018. Web. 26 Feb 2020.

Vancouver:

Albertson NJ. Mechanical and Electromagnetic Optimization of Structurally Embedded Waveguide Antennas. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/81959.

Council of Science Editors:

Albertson NJ. Mechanical and Electromagnetic Optimization of Structurally Embedded Waveguide Antennas. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/81959

6. Turner, Aaron Michael. Continuum Sensitivity Analysis for Shape Optimization in Incompressible Flow Problems.

Degree: MS, Aerospace and Ocean Engineering, 2017, Virginia Tech

 An important part of an aerodynamic design process is optimizing designs to maximize quantities such as lift and the lift-to-drag ratio, in a process known… (more)

Subjects/Keywords: Continuum Sensitivity Analysis; Finite Element Method

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APA (6th Edition):

Turner, A. M. (2017). Continuum Sensitivity Analysis for Shape Optimization in Incompressible Flow Problems. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78362

Chicago Manual of Style (16th Edition):

Turner, Aaron Michael. “Continuum Sensitivity Analysis for Shape Optimization in Incompressible Flow Problems.” 2017. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/78362.

MLA Handbook (7th Edition):

Turner, Aaron Michael. “Continuum Sensitivity Analysis for Shape Optimization in Incompressible Flow Problems.” 2017. Web. 26 Feb 2020.

Vancouver:

Turner AM. Continuum Sensitivity Analysis for Shape Optimization in Incompressible Flow Problems. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/78362.

Council of Science Editors:

Turner AM. Continuum Sensitivity Analysis for Shape Optimization in Incompressible Flow Problems. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/78362

7. Adegbindin, Moustaine Kolawole Agnide. Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft.

Degree: MS, Aerospace and Ocean Engineering, 2017, Virginia Tech

 Many futuristic aircraft such as the Hybrid Wing Body have numerous control surfaces that can result in large hinge moments, high actuation power demands, and… (more)

Subjects/Keywords: Optimization; Artificial Intelligence; Neural Network; Genetic Algorithm; Forward Swept Wing; Hybrid Wing Body; Hinge Moment

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APA (6th Edition):

Adegbindin, M. K. A. (2017). Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/74950

Chicago Manual of Style (16th Edition):

Adegbindin, Moustaine Kolawole Agnide. “Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft.” 2017. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/74950.

MLA Handbook (7th Edition):

Adegbindin, Moustaine Kolawole Agnide. “Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft.” 2017. Web. 26 Feb 2020.

Vancouver:

Adegbindin MKA. Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/74950.

Council of Science Editors:

Adegbindin MKA. Control Power Optimization using Artificial Intelligence for Forward Swept Wing and Hybrid Wing Body Aircraft. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/74950


Virginia Tech

8. Leonard, Benjamin Yoshi. Flapping Wing Flight Dynamic Modeling.

Degree: MS, Aerospace and Ocean Engineering, 2011, Virginia Tech

 Highly agile, hover capable flapping wing flight is a relatively new area of study in engineering. Researchers are looking to flapping flight as a potential… (more)

Subjects/Keywords: Flight Dynamics; Flapping Flight

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APA (6th Edition):

Leonard, B. Y. (2011). Flapping Wing Flight Dynamic Modeling. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34790

Chicago Manual of Style (16th Edition):

Leonard, Benjamin Yoshi. “Flapping Wing Flight Dynamic Modeling.” 2011. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/34790.

MLA Handbook (7th Edition):

Leonard, Benjamin Yoshi. “Flapping Wing Flight Dynamic Modeling.” 2011. Web. 26 Feb 2020.

Vancouver:

Leonard BY. Flapping Wing Flight Dynamic Modeling. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/34790.

Council of Science Editors:

Leonard BY. Flapping Wing Flight Dynamic Modeling. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/34790


Virginia Tech

9. Ricciardi, Anthony Pasquale. Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations.

Degree: MS, Aerospace and Ocean Engineering, 2011, Virginia Tech

 Aeroelastic gust and maneuver loads have driven the sizing of primary aircraft structures since the beginning of aviation. Methodologies for determining the gust loads on… (more)

Subjects/Keywords: SensorCraft; Aeroelasticity; Gust Loads

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APA (6th Edition):

Ricciardi, A. P. (2011). Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35359

Chicago Manual of Style (16th Edition):

Ricciardi, Anthony Pasquale. “Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations.” 2011. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/35359.

MLA Handbook (7th Edition):

Ricciardi, Anthony Pasquale. “Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations.” 2011. Web. 26 Feb 2020.

Vancouver:

Ricciardi AP. Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/35359.

Council of Science Editors:

Ricciardi AP. Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/35359


Virginia Tech

10. Callahan, Joseph E. Analysis of Composite Helmet Impact by the Finite Element Method.

Degree: MS, Aerospace and Ocean Engineering, 2011, Virginia Tech

 We analyze by the finite element method transient deformations of a helmet mounted on a Roma Plastilina1 clay-filled rigid and stationary headform. The helmet is… (more)

Subjects/Keywords: Roma Plastilina1 Clay; Helmet; Laminated Composite; Impact

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APA (6th Edition):

Callahan, J. E. (2011). Analysis of Composite Helmet Impact by the Finite Element Method. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35649

Chicago Manual of Style (16th Edition):

Callahan, Joseph E. “Analysis of Composite Helmet Impact by the Finite Element Method.” 2011. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/35649.

MLA Handbook (7th Edition):

Callahan, Joseph E. “Analysis of Composite Helmet Impact by the Finite Element Method.” 2011. Web. 26 Feb 2020.

Vancouver:

Callahan JE. Analysis of Composite Helmet Impact by the Finite Element Method. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/35649.

Council of Science Editors:

Callahan JE. Analysis of Composite Helmet Impact by the Finite Element Method. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/35649


Virginia Tech

11. Capps, Ryan Anthony. Fatigue Characteristics of Pressurized Artificial Muscles.

Degree: MS, Aerospace and Ocean Engineering, 2014, Virginia Tech

 Pressurized artificial muscles show promise in both standard aircraft actuation operations and in morphing structures as an alternative to currently used actuation systems due to… (more)

Subjects/Keywords: Fatigue; Pressurized Artificial Muscles

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APA (6th Edition):

Capps, R. A. (2014). Fatigue Characteristics of Pressurized Artificial Muscles. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49702

Chicago Manual of Style (16th Edition):

Capps, Ryan Anthony. “Fatigue Characteristics of Pressurized Artificial Muscles.” 2014. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/49702.

MLA Handbook (7th Edition):

Capps, Ryan Anthony. “Fatigue Characteristics of Pressurized Artificial Muscles.” 2014. Web. 26 Feb 2020.

Vancouver:

Capps RA. Fatigue Characteristics of Pressurized Artificial Muscles. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/49702.

Council of Science Editors:

Capps RA. Fatigue Characteristics of Pressurized Artificial Muscles. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/49702


Virginia Tech

12. Names, Benjamin Joseph. An Efficient Reduced Order Modeling Method for Analyzing Composite Beams Under Aeroelastic Loading.

Degree: MS, Aerospace and Ocean Engineering, 2016, Virginia Tech

 Composite materials hold numerous advantages over conventional aircraft grade metals. These include high stiffness/strength-to-weight ratios and beneficial stiffness coupling typically used for aeroelastic tailoring. Due… (more)

Subjects/Keywords: Composites; Reduced Order Modeling; Stress Analysis; Aeroelasticity; Flutter

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APA (6th Edition):

Names, B. J. (2016). An Efficient Reduced Order Modeling Method for Analyzing Composite Beams Under Aeroelastic Loading. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71676

Chicago Manual of Style (16th Edition):

Names, Benjamin Joseph. “An Efficient Reduced Order Modeling Method for Analyzing Composite Beams Under Aeroelastic Loading.” 2016. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/71676.

MLA Handbook (7th Edition):

Names, Benjamin Joseph. “An Efficient Reduced Order Modeling Method for Analyzing Composite Beams Under Aeroelastic Loading.” 2016. Web. 26 Feb 2020.

Vancouver:

Names BJ. An Efficient Reduced Order Modeling Method for Analyzing Composite Beams Under Aeroelastic Loading. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/71676.

Council of Science Editors:

Names BJ. An Efficient Reduced Order Modeling Method for Analyzing Composite Beams Under Aeroelastic Loading. [Masters Thesis]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71676


Virginia Tech

13. Lyford, Andrew Lindquist. Failure Prediction of Honeycomb Panel Joints using Finite Element Analysis.

Degree: MS, Aerospace and Ocean Engineering, 2017, Virginia Tech

 Spacecraft structures rely on honeycomb panels to provide a light weight means to support the vehicle. Honeycomb panels can carry significant load but are most… (more)

Subjects/Keywords: Adhesive; Honeycomb; Joint; Finite Element Analysis

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APA (6th Edition):

Lyford, A. L. (2017). Failure Prediction of Honeycomb Panel Joints using Finite Element Analysis. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77029

Chicago Manual of Style (16th Edition):

Lyford, Andrew Lindquist. “Failure Prediction of Honeycomb Panel Joints using Finite Element Analysis.” 2017. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/77029.

MLA Handbook (7th Edition):

Lyford, Andrew Lindquist. “Failure Prediction of Honeycomb Panel Joints using Finite Element Analysis.” 2017. Web. 26 Feb 2020.

Vancouver:

Lyford AL. Failure Prediction of Honeycomb Panel Joints using Finite Element Analysis. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/77029.

Council of Science Editors:

Lyford AL. Failure Prediction of Honeycomb Panel Joints using Finite Element Analysis. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/77029


Virginia Tech

14. Palframan, Mark C. Real Time Biological Threat Agent Detection with a Surface Plasmon Resonance Equipped Unmanned Aerial Vehicle.

Degree: MS, Aerospace and Ocean Engineering, 2013, Virginia Tech

 A system was developed to perform real-time biological threat agent (BTA) detection with a small autonomous unmanned aerial vehicle (UAV). Biological sensors just recently reached… (more)

Subjects/Keywords: Surface Plasmon Resonance; Unmanned Aerial Vehicle; Biological Threat Agent; Aerial Sampling; Biological Sensor

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APA (6th Edition):

Palframan, M. C. (2013). Real Time Biological Threat Agent Detection with a Surface Plasmon Resonance Equipped Unmanned Aerial Vehicle. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23241

Chicago Manual of Style (16th Edition):

Palframan, Mark C. “Real Time Biological Threat Agent Detection with a Surface Plasmon Resonance Equipped Unmanned Aerial Vehicle.” 2013. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/23241.

MLA Handbook (7th Edition):

Palframan, Mark C. “Real Time Biological Threat Agent Detection with a Surface Plasmon Resonance Equipped Unmanned Aerial Vehicle.” 2013. Web. 26 Feb 2020.

Vancouver:

Palframan MC. Real Time Biological Threat Agent Detection with a Surface Plasmon Resonance Equipped Unmanned Aerial Vehicle. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/23241.

Council of Science Editors:

Palframan MC. Real Time Biological Threat Agent Detection with a Surface Plasmon Resonance Equipped Unmanned Aerial Vehicle. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23241


Virginia Tech

15. Aubuchon, Vanessa V. Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics.

Degree: MS, Aerospace and Ocean Engineering, 2013, Virginia Tech

 Currently, simulation predictions of the Orion Crew Module (CM) dynamics with drogue parachutes deployed are under-predicting the amount of damping as seen in free-flight tests.… (more)

Subjects/Keywords: parachutes; forced oscillation; damping; blunt body reentry vehicle; dynamic derivatives

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APA (6th Edition):

Aubuchon, V. V. (2013). Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23327

Chicago Manual of Style (16th Edition):

Aubuchon, Vanessa V. “Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics.” 2013. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/23327.

MLA Handbook (7th Edition):

Aubuchon, Vanessa V. “Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics.” 2013. Web. 26 Feb 2020.

Vancouver:

Aubuchon VV. Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/23327.

Council of Science Editors:

Aubuchon VV. Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23327


Virginia Tech

16. Degl'Incerti Tocci, Corrado. Analysis of Composites using Peridynamics.

Degree: MS, Aerospace and Ocean Engineering, 2014, Virginia Tech

 Since the last century a lot of effort has been spent trying to analyze damage and crack evolution in solids. This field is of interest… (more)

Subjects/Keywords: peridynamics; multiscale; carbon nanotube; finite element analysis; truss; micromechanics

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APA (6th Edition):

Degl'Incerti Tocci, C. (2014). Analysis of Composites using Peridynamics. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/25351

Chicago Manual of Style (16th Edition):

Degl'Incerti Tocci, Corrado. “Analysis of Composites using Peridynamics.” 2014. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/25351.

MLA Handbook (7th Edition):

Degl'Incerti Tocci, Corrado. “Analysis of Composites using Peridynamics.” 2014. Web. 26 Feb 2020.

Vancouver:

Degl'Incerti Tocci C. Analysis of Composites using Peridynamics. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/25351.

Council of Science Editors:

Degl'Incerti Tocci C. Analysis of Composites using Peridynamics. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/25351


Virginia Tech

17. Ouellette, Jeffrey. Flight Dynamics and Maneuver Loads on a Commercial Aircraft with Discrete Source Damage.

Degree: MS, Aerospace and Ocean Engineering, 2010, Virginia Tech

 To improve the recoverability and survivability of aircraft after damage, a better understanding of the flight dynamics and the structural loads is needed. However, damage… (more)

Subjects/Keywords: Maneuver Loads; Damaged Aircraft; Flight Dynamics

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APA (6th Edition):

Ouellette, J. (2010). Flight Dynamics and Maneuver Loads on a Commercial Aircraft with Discrete Source Damage. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32339

Chicago Manual of Style (16th Edition):

Ouellette, Jeffrey. “Flight Dynamics and Maneuver Loads on a Commercial Aircraft with Discrete Source Damage.” 2010. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/32339.

MLA Handbook (7th Edition):

Ouellette, Jeffrey. “Flight Dynamics and Maneuver Loads on a Commercial Aircraft with Discrete Source Damage.” 2010. Web. 26 Feb 2020.

Vancouver:

Ouellette J. Flight Dynamics and Maneuver Loads on a Commercial Aircraft with Discrete Source Damage. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/32339.

Council of Science Editors:

Ouellette J. Flight Dynamics and Maneuver Loads on a Commercial Aircraft with Discrete Source Damage. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/32339


Virginia Tech

18. Offenberger, Sean Alan. Investigation of Zinc Oxide Nanowires for Impedance Based Structural Health Monitoring.

Degree: MS, Aerospace and Ocean Engineering, 2018, Virginia Tech

 The goal of this work is to investigate the piezoelectricity of composite laminates embedded with layers of zinc oxide (ZnO) nanowires. ZnO nanowire embedded composites… (more)

Subjects/Keywords: Smart Materials; Piezoelectrics; Zinc Oxide Nanowires; Impedance-Based Structural Health Monitoring

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APA (6th Edition):

Offenberger, S. A. (2018). Investigation of Zinc Oxide Nanowires for Impedance Based Structural Health Monitoring. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82502

Chicago Manual of Style (16th Edition):

Offenberger, Sean Alan. “Investigation of Zinc Oxide Nanowires for Impedance Based Structural Health Monitoring.” 2018. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/82502.

MLA Handbook (7th Edition):

Offenberger, Sean Alan. “Investigation of Zinc Oxide Nanowires for Impedance Based Structural Health Monitoring.” 2018. Web. 26 Feb 2020.

Vancouver:

Offenberger SA. Investigation of Zinc Oxide Nanowires for Impedance Based Structural Health Monitoring. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/82502.

Council of Science Editors:

Offenberger SA. Investigation of Zinc Oxide Nanowires for Impedance Based Structural Health Monitoring. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/82502


Virginia Tech

19. Li, Tianyu. On the Formulation of a Hybrid Discontinuous Galerkin Finite Element Method (DG-FEM) for Multi-layered Shell Structures.

Degree: MS, Aerospace and Ocean Engineering, 2016, Virginia Tech

 A high-order hybrid discontinuous Galerkin finite element method (DG-FEM) is developed for multi-layered curved panels having large deformation and finite strain. The kinematics of the… (more)

Subjects/Keywords: hybrid discontinuous Galerkin finite element method; Multi-layered and stiffened plates and shells; large deformation and strain; Dirac's delta function; Orthogonal basis function

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APA (6th Edition):

Li, T. (2016). On the Formulation of a Hybrid Discontinuous Galerkin Finite Element Method (DG-FEM) for Multi-layered Shell Structures. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82962

Chicago Manual of Style (16th Edition):

Li, Tianyu. “On the Formulation of a Hybrid Discontinuous Galerkin Finite Element Method (DG-FEM) for Multi-layered Shell Structures.” 2016. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/82962.

MLA Handbook (7th Edition):

Li, Tianyu. “On the Formulation of a Hybrid Discontinuous Galerkin Finite Element Method (DG-FEM) for Multi-layered Shell Structures.” 2016. Web. 26 Feb 2020.

Vancouver:

Li T. On the Formulation of a Hybrid Discontinuous Galerkin Finite Element Method (DG-FEM) for Multi-layered Shell Structures. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/82962.

Council of Science Editors:

Li T. On the Formulation of a Hybrid Discontinuous Galerkin Finite Element Method (DG-FEM) for Multi-layered Shell Structures. [Masters Thesis]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/82962


Virginia Tech

20. Deshpande, Revati Rajeev. Effect of Centrifugal Stiffening on the Natural Frequencies of Aircraft Wings During Rapid Roll Maneuvers.

Degree: MS, Aerospace and Ocean Engineering, 2018, Virginia Tech

 The rolling of an aircraft about its fuselage produces centrifugal forces which affect the stiffness of the wings. A number of previous studies explain the… (more)

Subjects/Keywords: Centrifugal Stiffening; Rotating beam; Natural Frequencies

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APA (6th Edition):

Deshpande, R. R. (2018). Effect of Centrifugal Stiffening on the Natural Frequencies of Aircraft Wings During Rapid Roll Maneuvers. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/92698

Chicago Manual of Style (16th Edition):

Deshpande, Revati Rajeev. “Effect of Centrifugal Stiffening on the Natural Frequencies of Aircraft Wings During Rapid Roll Maneuvers.” 2018. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/92698.

MLA Handbook (7th Edition):

Deshpande, Revati Rajeev. “Effect of Centrifugal Stiffening on the Natural Frequencies of Aircraft Wings During Rapid Roll Maneuvers.” 2018. Web. 26 Feb 2020.

Vancouver:

Deshpande RR. Effect of Centrifugal Stiffening on the Natural Frequencies of Aircraft Wings During Rapid Roll Maneuvers. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/92698.

Council of Science Editors:

Deshpande RR. Effect of Centrifugal Stiffening on the Natural Frequencies of Aircraft Wings During Rapid Roll Maneuvers. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/92698


Virginia Tech

21. Eger, Charles Alfred Gaitan. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.

Degree: MS, Aerospace Engineering, 2013, Virginia Tech

 A procedure for the design of a scaled aircraft using linear aeroelastic scaling is developed and demonstrated. Previous work has shown the viability in matching… (more)

Subjects/Keywords: Aeroelasticity; Scaling; Joined-wing

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APA (6th Edition):

Eger, C. A. G. (2013). Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23088

Chicago Manual of Style (16th Edition):

Eger, Charles Alfred Gaitan. “Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.” 2013. Masters Thesis, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/23088.

MLA Handbook (7th Edition):

Eger, Charles Alfred Gaitan. “Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.” 2013. Web. 26 Feb 2020.

Vancouver:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/23088.

Council of Science Editors:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23088

22. Arifianto, Ony. A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation.

Degree: PhD, Aerospace and Ocean Engineering, 2014, Virginia Tech

 This dissertation describes the development and modeling of a low-cost, open source, and reliable small fixed-wing unmanned aerial vehicle (UAV) for advanced control implementation. The… (more)

Subjects/Keywords: Unmanned Aerial Research Vehicles; Linear Time-Varying Control; Embedded Systems; System Identification

…performed in the Subsonic Open Jet Wind Tunnel at Virginia Tech following the procedure given in… 

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APA (6th Edition):

Arifianto, O. (2014). A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49301

Chicago Manual of Style (16th Edition):

Arifianto, Ony. “A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation.” 2014. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/49301.

MLA Handbook (7th Edition):

Arifianto, Ony. “A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation.” 2014. Web. 26 Feb 2020.

Vancouver:

Arifianto O. A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/49301.

Council of Science Editors:

Arifianto O. A Low-Cost Unmanned Aerial Vehicle Research Platform: Development, Modeling and Advanced Control Implementation. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/49301

23. Kancharala, Ashok Kumar. The role of flexibility on propulsive performance of flapping fins.

Degree: PhD, Aerospace and Ocean Engineering, 2015, Virginia Tech

 The versatility of the fish to adapt to diverse swimming requirements has attracted the attention of researchers in studying bioinspired propulsion for developing efficient underwater… (more)

Subjects/Keywords: Hydroelasticity; Caudal fin; Caudal peduncle; Self-propelled speed; Center of mass; Optimization; Macro Fiber Composites; Digital Image Correlation

…developed at Virginia Tech using Flexible Matrix Composite (FMC) actuators 1.1.1… …kinematics, optimal gaits and performance. The robotic fish developed at AOE department, Virginia… …Tech using flexible matrix composite (FMC) actuators is shown in figure 1.1. This… 

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APA (6th Edition):

Kancharala, A. K. (2015). The role of flexibility on propulsive performance of flapping fins. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/56563

Chicago Manual of Style (16th Edition):

Kancharala, Ashok Kumar. “The role of flexibility on propulsive performance of flapping fins.” 2015. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/56563.

MLA Handbook (7th Edition):

Kancharala, Ashok Kumar. “The role of flexibility on propulsive performance of flapping fins.” 2015. Web. 26 Feb 2020.

Vancouver:

Kancharala AK. The role of flexibility on propulsive performance of flapping fins. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/56563.

Council of Science Editors:

Kancharala AK. The role of flexibility on propulsive performance of flapping fins. [Doctoral Dissertation]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/56563

24. Li, Zhongwei. Reliability-Based Design Optimization of Nonlinear Beam-Columns.

Degree: PhD, Aerospace Engineering, 2018, Virginia Tech

 This dissertation addresses the ultimate strength analysis of nonlinear beam-columns under axial compression, the sensitivity of the ultimate strength, structural optimization and reliability analysis using… (more)

Subjects/Keywords: Ultimate Strength; Nonlinear Beam-Column; Sensitivity Analysis; Structural Optimization; Structural Reliability; Reliability-Based Design Optimization

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APA (6th Edition):

Li, Z. (2018). Reliability-Based Design Optimization of Nonlinear Beam-Columns. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82958

Chicago Manual of Style (16th Edition):

Li, Zhongwei. “Reliability-Based Design Optimization of Nonlinear Beam-Columns.” 2018. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/82958.

MLA Handbook (7th Edition):

Li, Zhongwei. “Reliability-Based Design Optimization of Nonlinear Beam-Columns.” 2018. Web. 26 Feb 2020.

Vancouver:

Li Z. Reliability-Based Design Optimization of Nonlinear Beam-Columns. [Internet] [Doctoral dissertation]. Virginia Tech; 2018. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/82958.

Council of Science Editors:

Li Z. Reliability-Based Design Optimization of Nonlinear Beam-Columns. [Doctoral Dissertation]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/82958

25. Seifert, David Ryan. Topology Optimization of Multifunctional Nanocomposite Structures.

Degree: PhD, Aerospace Engineering, 2018, Virginia Tech

 This dissertation presents a method that allows for the best placement of a limited amount of filler material within a base matrix material to form… (more)

Subjects/Keywords: Topology Optimization; Carbon Nanotubes; Multifunctional Materials; Micromechanics; Analytic Sensitivities; Strain Sensing

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APA (6th Edition):

Seifert, D. R. (2018). Topology Optimization of Multifunctional Nanocomposite Structures. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/86195

Chicago Manual of Style (16th Edition):

Seifert, David Ryan. “Topology Optimization of Multifunctional Nanocomposite Structures.” 2018. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/86195.

MLA Handbook (7th Edition):

Seifert, David Ryan. “Topology Optimization of Multifunctional Nanocomposite Structures.” 2018. Web. 26 Feb 2020.

Vancouver:

Seifert DR. Topology Optimization of Multifunctional Nanocomposite Structures. [Internet] [Doctoral dissertation]. Virginia Tech; 2018. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/86195.

Council of Science Editors:

Seifert DR. Topology Optimization of Multifunctional Nanocomposite Structures. [Doctoral Dissertation]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/86195

26. Doepke, Edward Brady. Design Demonstration and Optimization of a Morphing  Aircraft Control Surface Using Flexible Matrix Composite Actuators.

Degree: PhD, Aerospace and Ocean Engineering, 2018, Virginia Tech

 The morphing of aircraft wings for flight control started as a necessity for the Wright Brothers but quickly fell out of favor as aircraft increased… (more)

Subjects/Keywords: Morphing; Aircraft Control Surfaces; Flexible Matrix Composite Actuator

…untaken at Virginia Tech to create the first fully solid-state piezoelectric controlled aircraft… 

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APA (6th Edition):

Doepke, E. B. (2018). Design Demonstration and Optimization of a Morphing  Aircraft Control Surface Using Flexible Matrix Composite Actuators. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82494

Chicago Manual of Style (16th Edition):

Doepke, Edward Brady. “Design Demonstration and Optimization of a Morphing  Aircraft Control Surface Using Flexible Matrix Composite Actuators.” 2018. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/82494.

MLA Handbook (7th Edition):

Doepke, Edward Brady. “Design Demonstration and Optimization of a Morphing  Aircraft Control Surface Using Flexible Matrix Composite Actuators.” 2018. Web. 26 Feb 2020.

Vancouver:

Doepke EB. Design Demonstration and Optimization of a Morphing  Aircraft Control Surface Using Flexible Matrix Composite Actuators. [Internet] [Doctoral dissertation]. Virginia Tech; 2018. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/82494.

Council of Science Editors:

Doepke EB. Design Demonstration and Optimization of a Morphing  Aircraft Control Surface Using Flexible Matrix Composite Actuators. [Doctoral Dissertation]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/82494


Virginia Tech

27. Emory, Christopher Wyatt. Prediction of Limit Cycle Oscillation in an Aeroelastic System using Nonlinear Normal Modes.

Degree: PhD, Aerospace and Ocean Engineering, 2010, Virginia Tech

 There is a need for a nonlinear flutter analysis method capable of predicting limit cycle oscillation in aeroelastic systems. A review is conducted of analysis… (more)

Subjects/Keywords: Nonlinear Normal Modes; Limit Cycle Oscillation; Nonlinear Aeroelasticity

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APA (6th Edition):

Emory, C. W. (2010). Prediction of Limit Cycle Oscillation in an Aeroelastic System using Nonlinear Normal Modes. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30133

Chicago Manual of Style (16th Edition):

Emory, Christopher Wyatt. “Prediction of Limit Cycle Oscillation in an Aeroelastic System using Nonlinear Normal Modes.” 2010. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/30133.

MLA Handbook (7th Edition):

Emory, Christopher Wyatt. “Prediction of Limit Cycle Oscillation in an Aeroelastic System using Nonlinear Normal Modes.” 2010. Web. 26 Feb 2020.

Vancouver:

Emory CW. Prediction of Limit Cycle Oscillation in an Aeroelastic System using Nonlinear Normal Modes. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/30133.

Council of Science Editors:

Emory CW. Prediction of Limit Cycle Oscillation in an Aeroelastic System using Nonlinear Normal Modes. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/30133


Virginia Tech

28. Yari Boroujeni, Ayoub. Fatigue, Fracture and Impact of Hybrid Carbon Fiber Reinforced Polymer Composites.

Degree: PhD, Engineering Science and Mechanics, 2017, Virginia Tech

 The excellent in-plane strength and stiffness to-weight ratios, as well as the ease of manufacturing have made the carbon fiber reinforced polymer composites (CFRPs) suitable… (more)

Subjects/Keywords: carbon fiber; hybrid composites; carbon nanotubes; ZnO nanorods; mechanical characterization; finite element modeling; fatigue

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APA (6th Edition):

Yari Boroujeni, A. (2017). Fatigue, Fracture and Impact of Hybrid Carbon Fiber Reinforced Polymer Composites. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/84223

Chicago Manual of Style (16th Edition):

Yari Boroujeni, Ayoub. “Fatigue, Fracture and Impact of Hybrid Carbon Fiber Reinforced Polymer Composites.” 2017. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/84223.

MLA Handbook (7th Edition):

Yari Boroujeni, Ayoub. “Fatigue, Fracture and Impact of Hybrid Carbon Fiber Reinforced Polymer Composites.” 2017. Web. 26 Feb 2020.

Vancouver:

Yari Boroujeni A. Fatigue, Fracture and Impact of Hybrid Carbon Fiber Reinforced Polymer Composites. [Internet] [Doctoral dissertation]. Virginia Tech; 2017. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/84223.

Council of Science Editors:

Yari Boroujeni A. Fatigue, Fracture and Impact of Hybrid Carbon Fiber Reinforced Polymer Composites. [Doctoral Dissertation]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/84223


Virginia Tech

29. Alipour Skandani, Amir. Computational and Experimental Nano Mechanics.

Degree: PhD, Engineering Science and Mechanics, 2014, Virginia Tech

 The many advances of nano technology extensively revolutionize mechanics. A tremendous need is growing to further bridge the gap between the classical mechanics and the… (more)

Subjects/Keywords: Carbon nano tubes; ZnO nano rods; Viscoelasticity; Viscoplasticity; molecular dynamics; nano composites; nano characterization; lipid cell membrane

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APA (6th Edition):

Alipour Skandani, A. (2014). Computational and Experimental Nano Mechanics. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/64869

Chicago Manual of Style (16th Edition):

Alipour Skandani, Amir. “Computational and Experimental Nano Mechanics.” 2014. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/64869.

MLA Handbook (7th Edition):

Alipour Skandani, Amir. “Computational and Experimental Nano Mechanics.” 2014. Web. 26 Feb 2020.

Vancouver:

Alipour Skandani A. Computational and Experimental Nano Mechanics. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/64869.

Council of Science Editors:

Alipour Skandani A. Computational and Experimental Nano Mechanics. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/64869


Virginia Tech

30. Walker, William Paul. Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency.

Degree: PhD, Aerospace and Ocean Engineering, 2012, Virginia Tech

 This dissertation presents both analytical and numerical approaches to optimizing thrust and thrust efficiency of harmonically deforming thin airfoils and membrane wings. A frequency domain… (more)

Subjects/Keywords: Unsteady Aerodynamics; Deformable Airfoils; Membrane Aeroelasticity; Aeroelastic Tailoring; Optimization

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APA (6th Edition):

Walker, W. P. (2012). Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/27748

Chicago Manual of Style (16th Edition):

Walker, William Paul. “Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency.” 2012. Doctoral Dissertation, Virginia Tech. Accessed February 26, 2020. http://hdl.handle.net/10919/27748.

MLA Handbook (7th Edition):

Walker, William Paul. “Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency.” 2012. Web. 26 Feb 2020.

Vancouver:

Walker WP. Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2020 Feb 26]. Available from: http://hdl.handle.net/10919/27748.

Council of Science Editors:

Walker WP. Optimization of Harmonically Deforming Thin Airfoils and Membrane Wings for Optimum Thrust and Efficiency. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/27748

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