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You searched for +publisher:"Virginia Tech" +contributor:("Kapania, Rakesh K."). Showing records 1 – 30 of 204 total matches.

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1. Rocker, Samantha Nicole. Piezoresistivity Characterization of Polymer Bonded Energetic Nanocomposites under Cyclic Load Cases for Structural Health Monitoring Applications.

Degree: MS, Aerospace Engineering, 2019, Virginia Tech

 The ability to characterize both deformation and damage in real time within materials of high energetic content, such as solid rocket propellant, is of great… (more)

Subjects/Keywords: Structural health monitoring; Piezoresistivity; Nanocomposites; Multifunctional composites; Energetics; Carbon nanotubes; Damage detection

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APA (6th Edition):

Rocker, S. N. (2019). Piezoresistivity Characterization of Polymer Bonded Energetic Nanocomposites under Cyclic Load Cases for Structural Health Monitoring Applications. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/91427

Chicago Manual of Style (16th Edition):

Rocker, Samantha Nicole. “Piezoresistivity Characterization of Polymer Bonded Energetic Nanocomposites under Cyclic Load Cases for Structural Health Monitoring Applications.” 2019. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/91427.

MLA Handbook (7th Edition):

Rocker, Samantha Nicole. “Piezoresistivity Characterization of Polymer Bonded Energetic Nanocomposites under Cyclic Load Cases for Structural Health Monitoring Applications.” 2019. Web. 13 Apr 2021.

Vancouver:

Rocker SN. Piezoresistivity Characterization of Polymer Bonded Energetic Nanocomposites under Cyclic Load Cases for Structural Health Monitoring Applications. [Internet] [Masters thesis]. Virginia Tech; 2019. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/91427.

Council of Science Editors:

Rocker SN. Piezoresistivity Characterization of Polymer Bonded Energetic Nanocomposites under Cyclic Load Cases for Structural Health Monitoring Applications. [Masters Thesis]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/91427

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

Degree: MS, Aerospace 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 April 13, 2021. 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. 13 Apr 2021.

Vancouver:

Olson NKK. Validation and Uncertainty Quantification of Doublet Lattice Flight Loads using Flight Test Data. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2021 Apr 13]. 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

3. Ng, Colin Uber. STEP-enabled Force Measurement Platform of Single Migratory Cells.

Degree: MS, Mechanical Engineering, 2014, Virginia Tech

 Spinneret based Tunable Engineered Parameters (STEP) Platform is a recently reported pseudo-dry spinning and non-electrospinning technique that allows for the deposition of aligned polymeric nano-fibers… (more)

Subjects/Keywords: nanofibers; group cell migration; cell forces; wound healing

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APA (6th Edition):

Ng, C. U. (2014). STEP-enabled Force Measurement Platform of Single Migratory Cells. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/25329

Chicago Manual of Style (16th Edition):

Ng, Colin Uber. “STEP-enabled Force Measurement Platform of Single Migratory Cells.” 2014. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/25329.

MLA Handbook (7th Edition):

Ng, Colin Uber. “STEP-enabled Force Measurement Platform of Single Migratory Cells.” 2014. Web. 13 Apr 2021.

Vancouver:

Ng CU. STEP-enabled Force Measurement Platform of Single Migratory Cells. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/25329.

Council of Science Editors:

Ng CU. STEP-enabled Force Measurement Platform of Single Migratory Cells. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/25329

4. Montero, Ryan M. Analysis, Design and Testing of a Wind Tunnel Model to Validate Fiber-Optic Shape Sensing Systems.

Degree: MS, Aerospace Engineering, 2013, Virginia Tech

 The ability to collect valuable data concerning the stress, strains, and shape profiles of aircraft and aircraft components during flight is important to fields such… (more)

Subjects/Keywords: flexible wing; shape sensing wing; aeroelastics

…jet tunnel experiments, but in two ways in the Virginia Tech Stability Wind Tunnel… …the measured uncertainty to 25 0.03125in. The experiments performed in the Virginia Tech… …Virginia Tech open throat wind tunnel [8]. A photograph of the wind tunnel is shown in… …Fig 4.1. Figure 4.1: Virginia Tech Subsonic Open Jet Wind Tunnel The tunnel is a blower… …functionality of the system and then more precise experiments were to be carried out in the Virginia… 

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APA (6th Edition):

Montero, R. M. (2013). Analysis, Design and Testing of a Wind Tunnel Model to Validate Fiber-Optic Shape Sensing Systems. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23233

Chicago Manual of Style (16th Edition):

Montero, Ryan M. “Analysis, Design and Testing of a Wind Tunnel Model to Validate Fiber-Optic Shape Sensing Systems.” 2013. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/23233.

MLA Handbook (7th Edition):

Montero, Ryan M. “Analysis, Design and Testing of a Wind Tunnel Model to Validate Fiber-Optic Shape Sensing Systems.” 2013. Web. 13 Apr 2021.

Vancouver:

Montero RM. Analysis, Design and Testing of a Wind Tunnel Model to Validate Fiber-Optic Shape Sensing Systems. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/23233.

Council of Science Editors:

Montero RM. Analysis, Design and Testing of a Wind Tunnel Model to Validate Fiber-Optic Shape Sensing Systems. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23233

5. Koons, Brian Joseph. Cancer Protrusions on a Tightrope - Suspended Fiber Platform Reveals Protrusion Dynamics Independent of Cell Migration.

Degree: MS, Mechanical Engineering, 2015, Virginia Tech

 Indispensable to all modes of migration used during single cell metastasis, cytoplasmic protrusions are pivotal in surveying cells local surroundings which ultimately initiates migration of… (more)

Subjects/Keywords: protrusion; nanofiber; curvature; cancer cell

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APA (6th Edition):

Koons, B. J. (2015). Cancer Protrusions on a Tightrope - Suspended Fiber Platform Reveals Protrusion Dynamics Independent of Cell Migration. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/73508

Chicago Manual of Style (16th Edition):

Koons, Brian Joseph. “Cancer Protrusions on a Tightrope - Suspended Fiber Platform Reveals Protrusion Dynamics Independent of Cell Migration.” 2015. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/73508.

MLA Handbook (7th Edition):

Koons, Brian Joseph. “Cancer Protrusions on a Tightrope - Suspended Fiber Platform Reveals Protrusion Dynamics Independent of Cell Migration.” 2015. Web. 13 Apr 2021.

Vancouver:

Koons BJ. Cancer Protrusions on a Tightrope - Suspended Fiber Platform Reveals Protrusion Dynamics Independent of Cell Migration. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/73508.

Council of Science Editors:

Koons BJ. Cancer Protrusions on a Tightrope - Suspended Fiber Platform Reveals Protrusion Dynamics Independent of Cell Migration. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/73508

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

Degree: MS, Aerospace 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 April 13, 2021. http://hdl.handle.net/10919/73988.

MLA Handbook (7th Edition):

Muthirevula, Neeharika. “Cross-Sectional Stiffness Properties of Complex Drone Wings.” 2017. Web. 13 Apr 2021.

Vancouver:

Muthirevula N. Cross-Sectional Stiffness Properties of Complex Drone Wings. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2021 Apr 13]. 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

7. Chhabra, Rupanshi. Control Power Optimization using Artificial Intelligence for Hybrid Wing Body Aircraft.

Degree: MS, Aerospace Engineering, 2015, Virginia Tech

 Traditional methods of control allocation optimization have shown difficulties in exploiting the full potential of controlling a large array of control surfaces. This research investigates… (more)

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

…researchers from NASA Langley, Virginia Tech, and Boeing Research and Technology are exploring the… 

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APA (6th Edition):

Chhabra, R. (2015). Control Power Optimization using Artificial Intelligence for Hybrid Wing Body Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/56580

Chicago Manual of Style (16th Edition):

Chhabra, Rupanshi. “Control Power Optimization using Artificial Intelligence for Hybrid Wing Body Aircraft.” 2015. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/56580.

MLA Handbook (7th Edition):

Chhabra, Rupanshi. “Control Power Optimization using Artificial Intelligence for Hybrid Wing Body Aircraft.” 2015. Web. 13 Apr 2021.

Vancouver:

Chhabra R. Control Power Optimization using Artificial Intelligence for Hybrid Wing Body Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/56580.

Council of Science Editors:

Chhabra R. Control Power Optimization using Artificial Intelligence for Hybrid Wing Body Aircraft. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/56580

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

Degree: MS, Aerospace 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 April 13, 2021. http://hdl.handle.net/10919/78665.

MLA Handbook (7th Edition):

Clark, Patrick Ryan. “Reliability-Based Topology Optimization with Analytic Sensitivities.” 2017. Web. 13 Apr 2021.

Vancouver:

Clark PR. Reliability-Based Topology Optimization with Analytic Sensitivities. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2021 Apr 13]. 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

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

Degree: MS, Aerospace 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 April 13, 2021. 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. 13 Apr 2021.

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 2021 Apr 13]. 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

10. Nichols, Jonathan Tyler. Application of Load Updating to a Complex Three Dimensional Frame Structure.

Degree: MS, Aerospace Engineering, 2017, Virginia Tech

 This thesis presents a novel method for the correlation of FEM results to experimental test results known as the "Load updating method." Specifically, the load… (more)

Subjects/Keywords: Load Updating; Model Updating; Loads Prediction; Finite Element Method; Strain Gage Data Correlation; NASTRAN; Structural Testing

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APA (6th Edition):

Nichols, J. T. (2017). Application of Load Updating to a Complex Three Dimensional Frame Structure. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78274

Chicago Manual of Style (16th Edition):

Nichols, Jonathan Tyler. “Application of Load Updating to a Complex Three Dimensional Frame Structure.” 2017. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/78274.

MLA Handbook (7th Edition):

Nichols, Jonathan Tyler. “Application of Load Updating to a Complex Three Dimensional Frame Structure.” 2017. Web. 13 Apr 2021.

Vancouver:

Nichols JT. Application of Load Updating to a Complex Three Dimensional Frame Structure. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/78274.

Council of Science Editors:

Nichols JT. Application of Load Updating to a Complex Three Dimensional Frame Structure. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/78274

11. Li, Jingran. Integration of Physically-based and Data-driven Approaches for Thermal Field Prediction in Additive Manufacturing.

Degree: MS, Materials Science and Engineering, 2017, Virginia Tech

 This paper aims to achieve the layer to layer temperature monitoring and consequently predict the temperature distribution for any new freeform geometry. An engineering statistical… (more)

Subjects/Keywords: additive manufacturing; geometry of freeform; layer-to-layer modeling; numerical simulation

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APA (6th Edition):

Li, J. (2017). Integration of Physically-based and Data-driven Approaches for Thermal Field Prediction in Additive Manufacturing. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/79620

Chicago Manual of Style (16th Edition):

Li, Jingran. “Integration of Physically-based and Data-driven Approaches for Thermal Field Prediction in Additive Manufacturing.” 2017. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/79620.

MLA Handbook (7th Edition):

Li, Jingran. “Integration of Physically-based and Data-driven Approaches for Thermal Field Prediction in Additive Manufacturing.” 2017. Web. 13 Apr 2021.

Vancouver:

Li J. Integration of Physically-based and Data-driven Approaches for Thermal Field Prediction in Additive Manufacturing. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/79620.

Council of Science Editors:

Li J. Integration of Physically-based and Data-driven Approaches for Thermal Field Prediction in Additive Manufacturing. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/79620


Virginia Tech

12. Marshall, Peter Johannes. Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method.

Degree: MS, Aerospace Engineering, 2018, Virginia Tech

 Spacecraft structures are subject to a series of load environments during their service life, with the most severe of these occurring during the spacecraft's launch… (more)

Subjects/Keywords: Acoustics; Spacecraft Structures; Boundary Element Method

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APA (6th Edition):

Marshall, P. J. (2018). Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/83460

Chicago Manual of Style (16th Edition):

Marshall, Peter Johannes. “Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method.” 2018. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/83460.

MLA Handbook (7th Edition):

Marshall, Peter Johannes. “Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method.” 2018. Web. 13 Apr 2021.

Vancouver:

Marshall PJ. Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/83460.

Council of Science Editors:

Marshall PJ. Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/83460


Virginia Tech

13. Jingeleski, David John. Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft.

Degree: MS, Aerospace Engineering, 2012, Virginia Tech

 Previous applications have shown that a wingtip treatment on a commercial airliner will reduce drag and increase fuel efficiency and the most common types of… (more)

Subjects/Keywords: variable geometry wingtip; roll control; gust alleviation

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APA (6th Edition):

Jingeleski, D. J. (2012). Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49562

Chicago Manual of Style (16th Edition):

Jingeleski, David John. “Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft.” 2012. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/49562.

MLA Handbook (7th Edition):

Jingeleski, David John. “Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft.” 2012. Web. 13 Apr 2021.

Vancouver:

Jingeleski DJ. Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/49562.

Council of Science Editors:

Jingeleski DJ. Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/49562


Virginia Tech

14. Sudalagunta, Praneeth Reddy. Control-oriented Modeling of an Air-breathing Hypersonic Vehicle.

Degree: PhD, Aerospace Engineering, 2016, Virginia Tech

 Design and development of future high speed aircraft require the use of advanced modeling tools early on in the design phase to study and analyze… (more)

Subjects/Keywords: Control-oriented Modeling; Aeroelasticity; Air-breathing Hypersonic Vehicles

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APA (6th Edition):

Sudalagunta, P. R. (2016). Control-oriented Modeling of an Air-breathing Hypersonic Vehicle. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/72872

Chicago Manual of Style (16th Edition):

Sudalagunta, Praneeth Reddy. “Control-oriented Modeling of an Air-breathing Hypersonic Vehicle.” 2016. Doctoral Dissertation, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/72872.

MLA Handbook (7th Edition):

Sudalagunta, Praneeth Reddy. “Control-oriented Modeling of an Air-breathing Hypersonic Vehicle.” 2016. Web. 13 Apr 2021.

Vancouver:

Sudalagunta PR. Control-oriented Modeling of an Air-breathing Hypersonic Vehicle. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/72872.

Council of Science Editors:

Sudalagunta PR. Control-oriented Modeling of an Air-breathing Hypersonic Vehicle. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/72872


Virginia Tech

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

Degree: MS, Aerospace 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 April 13, 2021. 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. 13 Apr 2021.

Vancouver:

Lyford AL. Failure Prediction of Honeycomb Panel Joints using Finite Element Analysis. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2021 Apr 13]. 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

16. Morris, Craig C. Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization.

Degree: PhD, Aerospace Engineering, 2014, Virginia Tech

 This work details the development of a stability and control module for implementation into a Multidisciplinary Design Optimization (MDO) framework for the conceptual design of… (more)

Subjects/Keywords: MDO; Dynamic Performance; Stability and Control; Linear Matrix Inequalities

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APA (6th Edition):

Morris, C. C. (2014). Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/25787

Chicago Manual of Style (16th Edition):

Morris, Craig C. “Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization.” 2014. Doctoral Dissertation, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/25787.

MLA Handbook (7th Edition):

Morris, Craig C. “Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization.” 2014. Web. 13 Apr 2021.

Vancouver:

Morris CC. Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/25787.

Council of Science Editors:

Morris CC. Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/25787


Virginia Tech

17. Riggins, Benjamin Kirby. Development of a Multi-Disciplinary Design Optimization Framework for a Strut-Braced Wing Transport Aircraft in PACELAB APD 3.1.

Degree: MS, Aerospace Engineering, 2015, Virginia Tech

 The purpose of this study was to extend the analysis methods in PACELAB APD 3.1, a recent commercially available aircraft preliminary design tool with potential… (more)

Subjects/Keywords: Aerospace; MDO; Multi-disciplinary Design and Optimization; PACELAB; FLOPS

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APA (6th Edition):

Riggins, B. K. (2015). Development of a Multi-Disciplinary Design Optimization Framework for a Strut-Braced Wing Transport Aircraft in PACELAB APD 3.1. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/52912

Chicago Manual of Style (16th Edition):

Riggins, Benjamin Kirby. “Development of a Multi-Disciplinary Design Optimization Framework for a Strut-Braced Wing Transport Aircraft in PACELAB APD 3.1.” 2015. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/52912.

MLA Handbook (7th Edition):

Riggins, Benjamin Kirby. “Development of a Multi-Disciplinary Design Optimization Framework for a Strut-Braced Wing Transport Aircraft in PACELAB APD 3.1.” 2015. Web. 13 Apr 2021.

Vancouver:

Riggins BK. Development of a Multi-Disciplinary Design Optimization Framework for a Strut-Braced Wing Transport Aircraft in PACELAB APD 3.1. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/52912.

Council of Science Editors:

Riggins BK. Development of a Multi-Disciplinary Design Optimization Framework for a Strut-Braced Wing Transport Aircraft in PACELAB APD 3.1. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/52912


Virginia Tech

18. Fave, Sebastian Philipp. Investigative Application of the Intrinsic Extended Finite Element Method for the Computational Characterization of Composite Materials.

Degree: MS, Aerospace Engineering, 2014, Virginia Tech

 Computational micromechanics analysis of carbon nanotube-epoxy nanocomposites, containing aligned nanotubes, is performed using the mesh independent intrinsic extended finite element method (IXFEM). The IXFEM employs… (more)

Subjects/Keywords: Intrinsic XFEM; Moving Least Squares; Level-Set Method; Effective Material Properties; Composite Materials

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APA (6th Edition):

Fave, S. P. (2014). Investigative Application of the Intrinsic Extended Finite Element Method for the Computational Characterization of Composite Materials. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50483

Chicago Manual of Style (16th Edition):

Fave, Sebastian Philipp. “Investigative Application of the Intrinsic Extended Finite Element Method for the Computational Characterization of Composite Materials.” 2014. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/50483.

MLA Handbook (7th Edition):

Fave, Sebastian Philipp. “Investigative Application of the Intrinsic Extended Finite Element Method for the Computational Characterization of Composite Materials.” 2014. Web. 13 Apr 2021.

Vancouver:

Fave SP. Investigative Application of the Intrinsic Extended Finite Element Method for the Computational Characterization of Composite Materials. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/50483.

Council of Science Editors:

Fave SP. Investigative Application of the Intrinsic Extended Finite Element Method for the Computational Characterization of Composite Materials. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/50483


Virginia Tech

19. Singh, Raymond Charan. Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling.

Degree: MS, Aerospace Engineering, 2012, Virginia Tech

 Given the ever-growing need for device autonomy and renewable sources of energy, energy harvesting has become an increasingly popular field of research. This research focuses… (more)

Subjects/Keywords: Piezoelectric; Energy Harvesting; Computational Methods; Membranes

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APA (6th Edition):

Singh, R. C. (2012). Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76793

Chicago Manual of Style (16th Edition):

Singh, Raymond Charan. “Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling.” 2012. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/76793.

MLA Handbook (7th Edition):

Singh, Raymond Charan. “Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling.” 2012. Web. 13 Apr 2021.

Vancouver:

Singh RC. Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/76793.

Council of Science Editors:

Singh RC. Modeling Energy Harvesting From Membrane Vibrations using Multi-physics Modeling. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/76793


Virginia Tech

20. Meadows, Nicholas Andrew. Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft.

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

 This study utilizes Multidisciplinary Design Optimization (MDO) techniques to explore the effectiveness of the truss-braced (TBW) and strut-braced (SBW) wing configurations in enhancing the performance… (more)

Subjects/Keywords: Transonic Transport Aircraft; Truss-Braced Wing; Multidisciplinary Design Optimization; Strut-Braced Wing

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APA (6th Edition):

Meadows, N. A. (2011). Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/44022

Chicago Manual of Style (16th Edition):

Meadows, Nicholas Andrew. “Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft.” 2011. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/44022.

MLA Handbook (7th Edition):

Meadows, Nicholas Andrew. “Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft.” 2011. Web. 13 Apr 2021.

Vancouver:

Meadows NA. Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/44022.

Council of Science Editors:

Meadows NA. Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/44022


Virginia Tech

21. Powers, Sean W. Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature, Hypersonic Flows.

Degree: MS, Aerospace Engineering, 2020, Virginia Tech

 Thermocouples are a device for measuring temperature, consisting of two wires of different metals connected at two different points. This configuration produces a temperature-dependent voltage… (more)

Subjects/Keywords: Thermocouples; Survivability; Low-Order Modeling; Lamé’s Stresses; Hypersonics; High-Temperature

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APA (6th Edition):

Powers, S. W. (2020). Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature, Hypersonic Flows. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/98000

Chicago Manual of Style (16th Edition):

Powers, Sean W. “Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature, Hypersonic Flows.” 2020. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/98000.

MLA Handbook (7th Edition):

Powers, Sean W. “Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature, Hypersonic Flows.” 2020. Web. 13 Apr 2021.

Vancouver:

Powers SW. Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature, Hypersonic Flows. [Internet] [Masters thesis]. Virginia Tech; 2020. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/98000.

Council of Science Editors:

Powers SW. Analysis of Stresses in Metal Sheathed Thermocouples in High-Temperature, Hypersonic Flows. [Masters Thesis]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/98000


Virginia Tech

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

Degree: MS, Aerospace 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 April 13, 2021. 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. 13 Apr 2021.

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 2021 Apr 13]. 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

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

Degree: MS, Aerospace 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 April 13, 2021. 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. 13 Apr 2021.

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 2021 Apr 13]. 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

24. Gill, Amritpal Singh. Development of a Novel Single-Cell Attachment and Spreading Platform Utilizing Fused-Fiber Nanonets.

Degree: MS, Mechanical Engineering, 2015, Virginia Tech

 Initial attachment to the extracellular matrix (ECM) and consequent spreading is a necessary process in the cell cycle of which little is known. Cell spreading… (more)

Subjects/Keywords: nanofiber; attachment; cell force; cell spreading; single-cell

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APA (6th Edition):

Gill, A. S. (2015). Development of a Novel Single-Cell Attachment and Spreading Platform Utilizing Fused-Fiber Nanonets. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/73504

Chicago Manual of Style (16th Edition):

Gill, Amritpal Singh. “Development of a Novel Single-Cell Attachment and Spreading Platform Utilizing Fused-Fiber Nanonets.” 2015. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/73504.

MLA Handbook (7th Edition):

Gill, Amritpal Singh. “Development of a Novel Single-Cell Attachment and Spreading Platform Utilizing Fused-Fiber Nanonets.” 2015. Web. 13 Apr 2021.

Vancouver:

Gill AS. Development of a Novel Single-Cell Attachment and Spreading Platform Utilizing Fused-Fiber Nanonets. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/73504.

Council of Science Editors:

Gill AS. Development of a Novel Single-Cell Attachment and Spreading Platform Utilizing Fused-Fiber Nanonets. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/73504

25. Segee, Molly Catherine. Surrogate Models for Transonic Aerodynamics for Multidisciplinary Design Optimization.

Degree: MS, Aerospace Engineering, 2016, Virginia Tech

 Multidisciplinary design optimization (MDO) requires many designs to be evaluated while searching for an optimum. As a result, the calculations done to evaluate the designs… (more)

Subjects/Keywords: Transonic Aerodynamics; Multidisciplinary Design Optimization; Truss-braced Wings; Strut-braced Wings; Computational Fluid Dynamics; Response Surface; Surrogate Models; Artificial Neural Networks; Buffet Boundary

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APA (6th Edition):

Segee, M. C. (2016). Surrogate Models for Transonic Aerodynamics for Multidisciplinary Design Optimization. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71321

Chicago Manual of Style (16th Edition):

Segee, Molly Catherine. “Surrogate Models for Transonic Aerodynamics for Multidisciplinary Design Optimization.” 2016. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/71321.

MLA Handbook (7th Edition):

Segee, Molly Catherine. “Surrogate Models for Transonic Aerodynamics for Multidisciplinary Design Optimization.” 2016. Web. 13 Apr 2021.

Vancouver:

Segee MC. Surrogate Models for Transonic Aerodynamics for Multidisciplinary Design Optimization. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/71321.

Council of Science Editors:

Segee MC. Surrogate Models for Transonic Aerodynamics for Multidisciplinary Design Optimization. [Masters Thesis]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71321


Virginia Tech

26. Butt, Lauren Marie. Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing.

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

 High aspect-ratio, long-endurance aircraft require different design modeling from those with traditional moderate aspect ratios. High aspect-ratio, long endurance aircraft are generally more flexible structures… (more)

Subjects/Keywords: Design Optimization; Aeroelasticity; Inflatable Wings

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APA (6th Edition):

Butt, L. M. (2011). Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/42641

Chicago Manual of Style (16th Edition):

Butt, Lauren Marie. “Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing.” 2011. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/42641.

MLA Handbook (7th Edition):

Butt, Lauren Marie. “Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing.” 2011. Web. 13 Apr 2021.

Vancouver:

Butt LM. Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/42641.

Council of Science Editors:

Butt LM. Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/42641


Virginia Tech

27. Shah, Udit. Mechanical Properties and Failure Analysis of Cellular Core Sandwich Panels.

Degree: MS, Aerospace Engineering, 2018, Virginia Tech

 Sandwich Panels with cellular cores are widely used in the aerospace industry for their higher stiffness to mass, strength to mass ratio, and excellent energy… (more)

Subjects/Keywords: Honeycomb Sandwich Panels; Cellular Cores; Triangular Core; Auxetic; Impact; Failure; Finite Element Analysis

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APA (6th Edition):

Shah, U. (2018). Mechanical Properties and Failure Analysis of Cellular Core Sandwich Panels. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/81699

Chicago Manual of Style (16th Edition):

Shah, Udit. “Mechanical Properties and Failure Analysis of Cellular Core Sandwich Panels.” 2018. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/81699.

MLA Handbook (7th Edition):

Shah, Udit. “Mechanical Properties and Failure Analysis of Cellular Core Sandwich Panels.” 2018. Web. 13 Apr 2021.

Vancouver:

Shah U. Mechanical Properties and Failure Analysis of Cellular Core Sandwich Panels. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/81699.

Council of Science Editors:

Shah U. Mechanical Properties and Failure Analysis of Cellular Core Sandwich Panels. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/81699


Virginia Tech

28. Singhvi, Sarvesh. Analysis, shape sensitivities and approximations of modal response of generally laminated tapered skew plates.

Degree: MS, Aerospace Engineering, 1991, Virginia Tech

Subjects/Keywords: Composite materials; LD5655.V855 1991.S5643

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APA (6th Edition):

Singhvi, S. (1991). Analysis, shape sensitivities and approximations of modal response of generally laminated tapered skew plates. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/41331

Chicago Manual of Style (16th Edition):

Singhvi, Sarvesh. “Analysis, shape sensitivities and approximations of modal response of generally laminated tapered skew plates.” 1991. Masters Thesis, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/41331.

MLA Handbook (7th Edition):

Singhvi, Sarvesh. “Analysis, shape sensitivities and approximations of modal response of generally laminated tapered skew plates.” 1991. Web. 13 Apr 2021.

Vancouver:

Singhvi S. Analysis, shape sensitivities and approximations of modal response of generally laminated tapered skew plates. [Internet] [Masters thesis]. Virginia Tech; 1991. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/41331.

Council of Science Editors:

Singhvi S. Analysis, shape sensitivities and approximations of modal response of generally laminated tapered skew plates. [Masters Thesis]. Virginia Tech; 1991. Available from: http://hdl.handle.net/10919/41331

29. Yang, Shu. Modeling and Control of Tensegrity-Membrane Systems.

Degree: PhD, Aerospace Engineering, 2016, Virginia Tech

 Tensegrity-membrane systems are a class of new bar-tendon-membrane systems. Such novel systems can be treated as extensions of tensegrity structures and are generally lightweight and… (more)

Subjects/Keywords: tensegrity-membrane systems; nonlinear finite element model; control-oriented model; nonlinear adaptive control; linear parameter-varying control

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APA (6th Edition):

Yang, S. (2016). Modeling and Control of Tensegrity-Membrane Systems. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71686

Chicago Manual of Style (16th Edition):

Yang, Shu. “Modeling and Control of Tensegrity-Membrane Systems.” 2016. Doctoral Dissertation, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/71686.

MLA Handbook (7th Edition):

Yang, Shu. “Modeling and Control of Tensegrity-Membrane Systems.” 2016. Web. 13 Apr 2021.

Vancouver:

Yang S. Modeling and Control of Tensegrity-Membrane Systems. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/71686.

Council of Science Editors:

Yang S. Modeling and Control of Tensegrity-Membrane Systems. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71686

30. Khan, Arafat Islam. Progressive Failure Analysis of Laminated Composite Structures.

Degree: PhD, Aerospace Engineering, 2015, Virginia Tech

 Laminated composite structures have started to play a very significant role in today's aircraft industry. The application of composite materials has now gone beyond the… (more)

Subjects/Keywords: Composites; Progressive Failure; Puck and Schürmann Failure Criteria; USDFLD; Laminated Structure

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APA (6th Edition):

Khan, A. I. (2015). Progressive Failure Analysis of Laminated Composite Structures. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/64389

Chicago Manual of Style (16th Edition):

Khan, Arafat Islam. “Progressive Failure Analysis of Laminated Composite Structures.” 2015. Doctoral Dissertation, Virginia Tech. Accessed April 13, 2021. http://hdl.handle.net/10919/64389.

MLA Handbook (7th Edition):

Khan, Arafat Islam. “Progressive Failure Analysis of Laminated Composite Structures.” 2015. Web. 13 Apr 2021.

Vancouver:

Khan AI. Progressive Failure Analysis of Laminated Composite Structures. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2021 Apr 13]. Available from: http://hdl.handle.net/10919/64389.

Council of Science Editors:

Khan AI. Progressive Failure Analysis of Laminated Composite Structures. [Doctoral Dissertation]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/64389

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