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You searched for +publisher:"Virginia Tech" +contributor:("Schetz, Joseph A."). Showing records 1 – 30 of 184 total matches.

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Virginia Tech

1. McDonald, Melea E. The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft.

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

 In recent years, research has been conducted for alternative commercial transonic aircraft design configurations, such as the strut- braced wing and the truss-braced wing aircraft… (more)

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

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APA (6th Edition):

McDonald, M. E. (2010). The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34124

Chicago Manual of Style (16th Edition):

McDonald, Melea E. “The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft.” 2010. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/34124.

MLA Handbook (7th Edition):

McDonald, Melea E. “The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft.” 2010. Web. 19 Oct 2019.

Vancouver:

McDonald ME. The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/34124.

Council of Science Editors:

McDonald ME. The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/34124


Virginia Tech

2. Rusche, Max Thomas. Structure of Turbulent Boundary Layers and Surface Pressure Fluctuations on a Patch of Large Roughness Elements.

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

 Measurements were made in a zero pressure gradient turbulent boundary layer over two roughness patches containing hemispherical and cubical elements. The elements were 3 mm… (more)

Subjects/Keywords: turbulence; roughness; surface pressure; velocity spectra; boundary layer

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APA (6th Edition):

Rusche, M. T. (2011). Structure of Turbulent Boundary Layers and Surface Pressure Fluctuations on a Patch of Large Roughness Elements. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34773

Chicago Manual of Style (16th Edition):

Rusche, Max Thomas. “Structure of Turbulent Boundary Layers and Surface Pressure Fluctuations on a Patch of Large Roughness Elements.” 2011. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/34773.

MLA Handbook (7th Edition):

Rusche, Max Thomas. “Structure of Turbulent Boundary Layers and Surface Pressure Fluctuations on a Patch of Large Roughness Elements.” 2011. Web. 19 Oct 2019.

Vancouver:

Rusche MT. Structure of Turbulent Boundary Layers and Surface Pressure Fluctuations on a Patch of Large Roughness Elements. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/34773.

Council of Science Editors:

Rusche MT. Structure of Turbulent Boundary Layers and Surface Pressure Fluctuations on a Patch of Large Roughness Elements. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/34773


Virginia Tech

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

Degree: MS, Aerospace and Ocean 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 October 19, 2019. 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. 19 Oct 2019.

Vancouver:

Jingeleski DJ. Aerodynamic Analysis of Variable Geometry Raked Wingtips for Mid-Range Transonic Transport Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2019 Oct 19]. 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

4. Schneider, Alex Joseph. Computational Modeling of Total Temperature Probes.

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

 A study is presented to explore the suitability of CFD as a tool in the design and analysis of total temperature probes. Simulations were completed… (more)

Subjects/Keywords: Computational Fluid Dynamics; Heat Transfer; High Temperature Instrumentation

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APA (6th Edition):

Schneider, A. J. (2015). Computational Modeling of Total Temperature Probes. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/51550

Chicago Manual of Style (16th Edition):

Schneider, Alex Joseph. “Computational Modeling of Total Temperature Probes.” 2015. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/51550.

MLA Handbook (7th Edition):

Schneider, Alex Joseph. “Computational Modeling of Total Temperature Probes.” 2015. Web. 19 Oct 2019.

Vancouver:

Schneider AJ. Computational Modeling of Total Temperature Probes. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/51550.

Council of Science Editors:

Schneider AJ. Computational Modeling of Total Temperature Probes. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/51550


Virginia Tech

5. 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 and Ocean 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 October 19, 2019. 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. 19 Oct 2019.

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 2019 Oct 19]. 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

6. Maisto, Pietro. Experimental analysis and prospective flow diagnostic applications for fluorescence dye-doped microparticles.

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

 The work described focuses on characterization of fluorescence dye-doped polystyrene latex particles (PSLs) dispersed in air as a candidate for advanced flow diagnostic techniques for… (more)

Subjects/Keywords: Laser Diagnostics; Fluid Dynamics; LIF; Particles

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APA (6th Edition):

Maisto, P. (2014). Experimental analysis and prospective flow diagnostic applications for fluorescence dye-doped microparticles. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/64835

Chicago Manual of Style (16th Edition):

Maisto, Pietro. “Experimental analysis and prospective flow diagnostic applications for fluorescence dye-doped microparticles.” 2014. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/64835.

MLA Handbook (7th Edition):

Maisto, Pietro. “Experimental analysis and prospective flow diagnostic applications for fluorescence dye-doped microparticles.” 2014. Web. 19 Oct 2019.

Vancouver:

Maisto P. Experimental analysis and prospective flow diagnostic applications for fluorescence dye-doped microparticles. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/64835.

Council of Science Editors:

Maisto P. Experimental analysis and prospective flow diagnostic applications for fluorescence dye-doped microparticles. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/64835

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

Degree: MS, Aerospace and Ocean 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 October 19, 2019. http://hdl.handle.net/10919/71321.

MLA Handbook (7th Edition):

Segee, Molly Catherine. “Surrogate Models for Transonic Aerodynamics for Multidisciplinary Design Optimization.” 2016. Web. 19 Oct 2019.

Vancouver:

Segee MC. Surrogate Models for Transonic Aerodynamics for Multidisciplinary Design Optimization. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2019 Oct 19]. 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

8. 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 October 19, 2019. 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. 19 Oct 2019.

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 2019 Oct 19]. 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

9. Meritt, Ryan James. A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications.

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

 This study concerns the design, analysis, and initial testing of a novel skin friction gage for applications in three-dimensional, high-speed, high-enthalpy flows. Design conditions required… (more)

Subjects/Keywords: complex turbulent flow; aerodynamics; wall shear; skin friction; high-enthalpy

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APA (6th Edition):

Meritt, R. J. (2010). A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76783

Chicago Manual of Style (16th Edition):

Meritt, Ryan James. “A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications.” 2010. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/76783.

MLA Handbook (7th Edition):

Meritt, Ryan James. “A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications.” 2010. Web. 19 Oct 2019.

Vancouver:

Meritt RJ. A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/76783.

Council of Science Editors:

Meritt RJ. A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/76783


Virginia Tech

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

Degree: MS, Aerospace and Ocean 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 October 19, 2019. 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. 19 Oct 2019.

Vancouver:

Nichols JT. Application of Load Updating to a Complex Three Dimensional Frame Structure. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2019 Oct 19]. 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


Virginia Tech

11. 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 October 19, 2019. 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. 19 Oct 2019.

Vancouver:

Meadows NA. Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Oct 19]. 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

12. 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 October 19, 2019. 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. 19 Oct 2019.

Vancouver:

Butt LM. Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Oct 19]. 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

13. 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 October 19, 2019. 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. 19 Oct 2019.

Vancouver:

Morris CC. Flight Dynamic Constraints in Conceptual Aircraft Multidisciplinary Analysis and Design Optimization. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2019 Oct 19]. 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

14. Burger, Scott Kuhlman. Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow.

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

 This study examines the effect of varying injectant molecular weight on the penetration of transverse injection jets into a supersonic crossflow. The injectants considered here… (more)

Subjects/Keywords: molecular weight; mixing; injection; scramjet

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APA (6th Edition):

Burger, S. K. (2010). Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31981

Chicago Manual of Style (16th Edition):

Burger, Scott Kuhlman. “Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow.” 2010. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/31981.

MLA Handbook (7th Edition):

Burger, Scott Kuhlman. “Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow.” 2010. Web. 19 Oct 2019.

Vancouver:

Burger SK. Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/31981.

Council of Science Editors:

Burger SK. Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/31981


Virginia Tech

15. Knight, Kyle Cohn Davis. Assessment of RANS Turbulence Models for Strut-Wing Junctions.

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

 Multidisciplinary Design Optimization (MDO) studies show the Strut/Truss Braced Wing (SBW/TBW) concept has the potential to save a significant amount of fuel over conventional designs.… (more)

Subjects/Keywords: Turbulence; Interference; Transonic

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APA (6th Edition):

Knight, K. C. D. (2011). Assessment of RANS Turbulence Models for Strut-Wing Junctions. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31760

Chicago Manual of Style (16th Edition):

Knight, Kyle Cohn Davis. “Assessment of RANS Turbulence Models for Strut-Wing Junctions.” 2011. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/31760.

MLA Handbook (7th Edition):

Knight, Kyle Cohn Davis. “Assessment of RANS Turbulence Models for Strut-Wing Junctions.” 2011. Web. 19 Oct 2019.

Vancouver:

Knight KCD. Assessment of RANS Turbulence Models for Strut-Wing Junctions. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/31760.

Council of Science Editors:

Knight KCD. Assessment of RANS Turbulence Models for Strut-Wing Junctions. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/31760


Virginia Tech

16. Tran, Kathleen. One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths.

Degree: MS, Mechanical Engineering, 2010, Virginia Tech

 One-Dimensional modeling of dual mode scramjet and ramjet flowpaths is a useful tool for scramjet conceptual design and wind tunnel testing. In this thesis, modeling… (more)

Subjects/Keywords: Hypersonic Propulsion; One Dimensional Modeling; Scramjets; Dual-Mode Scramjets

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APA (6th Edition):

Tran, K. (2010). One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30857

Chicago Manual of Style (16th Edition):

Tran, Kathleen. “One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths.” 2010. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/30857.

MLA Handbook (7th Edition):

Tran, Kathleen. “One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths.” 2010. Web. 19 Oct 2019.

Vancouver:

Tran K. One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/30857.

Council of Science Editors:

Tran K. One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/30857


Virginia Tech

17. Quickel, Reuben Alexander. Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes.

Degree: MS, Aerospace and Ocean Engineering, 2019, Virginia Tech

 Accurately measuring the total temperature of a high-speed fluid flow is a challenging task that is required in many research areas and industry applications. The… (more)

Subjects/Keywords: Total Temperature; Heat Transfer; Mount Effects; Flow Angle; Conduction; Convection; Aerodynamic Error

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APA (6th Edition):

Quickel, R. A. (2019). Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/89952

Chicago Manual of Style (16th Edition):

Quickel, Reuben Alexander. “Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes.” 2019. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/89952.

MLA Handbook (7th Edition):

Quickel, Reuben Alexander. “Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes.” 2019. Web. 19 Oct 2019.

Vancouver:

Quickel RA. Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes. [Internet] [Masters thesis]. Virginia Tech; 2019. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/89952.

Council of Science Editors:

Quickel RA. Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes. [Masters Thesis]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/89952

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

Degree: MS, Aerospace and Ocean 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 October 19, 2019. 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. 19 Oct 2019.

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 2019 Oct 19]. 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

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

Degree: MS, Aerospace and Ocean 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 October 19, 2019. 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. 19 Oct 2019.

Vancouver:

Chhabra R. Control Power Optimization using Artificial Intelligence for Hybrid Wing Body Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2019 Oct 19]. 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

20. Crosser, Kara Elizabeth. Heat Transfer Assessment of Aluminum Alloy Corrugated Naval Ship Deck Panels under VTOL Aircraft Thermal Loads.

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

 The behavior of aluminum alloy ship deck panels under the thermal loads of Vertical Take-off-and Landing (VTOL) capable aircraft has become a question of interest… (more)

Subjects/Keywords: Heat Transfer; Aluminum Alloy; Convection Coefficient

…surroundings. 3.3 Virginia Tech Hot Jet Facility The Virginia Tech Hot Jet was used in this study… …at the Virginia Tech Advanced Propulsion and Power Lab in Blacksburg, VA. The jet is driven… …Figure 7: Image of Virginia Tech Hot Jet Facility at the Advanced Propulsion and Power… …Laboratory Figure 8: Schematic of Virginia Tech Hot Jet Facility 3.4 Experimental Specimen… 

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APA (6th Edition):

Crosser, K. E. (2016). Heat Transfer Assessment of Aluminum Alloy Corrugated Naval Ship Deck Panels under VTOL Aircraft Thermal Loads. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/72947

Chicago Manual of Style (16th Edition):

Crosser, Kara Elizabeth. “Heat Transfer Assessment of Aluminum Alloy Corrugated Naval Ship Deck Panels under VTOL Aircraft Thermal Loads.” 2016. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/72947.

MLA Handbook (7th Edition):

Crosser, Kara Elizabeth. “Heat Transfer Assessment of Aluminum Alloy Corrugated Naval Ship Deck Panels under VTOL Aircraft Thermal Loads.” 2016. Web. 19 Oct 2019.

Vancouver:

Crosser KE. Heat Transfer Assessment of Aluminum Alloy Corrugated Naval Ship Deck Panels under VTOL Aircraft Thermal Loads. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/72947.

Council of Science Editors:

Crosser KE. Heat Transfer Assessment of Aluminum Alloy Corrugated Naval Ship Deck Panels under VTOL Aircraft Thermal Loads. [Masters Thesis]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/72947

21. Englerth, Steven Tyler. An Experimental Conduction Error Calibration Procedure for Cooled Total Temperature Probes.

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

 The accurate measurement of total temperature in engine diagnostics is a challenging task which is subject to several sources of error. Conduction error is predominant… (more)

Subjects/Keywords: Heat transfer; Conduction Error; Total Temperature Probe

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APA (6th Edition):

Englerth, S. T. (2015). An Experimental Conduction Error Calibration Procedure for Cooled Total Temperature Probes. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/51631

Chicago Manual of Style (16th Edition):

Englerth, Steven Tyler. “An Experimental Conduction Error Calibration Procedure for Cooled Total Temperature Probes.” 2015. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/51631.

MLA Handbook (7th Edition):

Englerth, Steven Tyler. “An Experimental Conduction Error Calibration Procedure for Cooled Total Temperature Probes.” 2015. Web. 19 Oct 2019.

Vancouver:

Englerth ST. An Experimental Conduction Error Calibration Procedure for Cooled Total Temperature Probes. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/51631.

Council of Science Editors:

Englerth ST. An Experimental Conduction Error Calibration Procedure for Cooled Total Temperature Probes. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/51631


Virginia Tech

22. Celik, Ahmet Ozan. Experimental Investigation of the Role of Turbulence Fluctuations on Incipient Motion of Sediment.

Degree: PhD, Civil Engineering, 2011, Virginia Tech

 The movement of granular material along a streambed has been a challenging subject for researchers for more than a century. Predicting the limiting case of… (more)

Subjects/Keywords: Pressure Measurements; Particle Tracking System; Open channel flow; Impulse; Turbulence; Hydrodynamic Forces; Incipient Motion; Rough bed

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APA (6th Edition):

Celik, A. O. (2011). Experimental Investigation of the Role of Turbulence Fluctuations on Incipient Motion of Sediment. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28731

Chicago Manual of Style (16th Edition):

Celik, Ahmet Ozan. “Experimental Investigation of the Role of Turbulence Fluctuations on Incipient Motion of Sediment.” 2011. Doctoral Dissertation, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/28731.

MLA Handbook (7th Edition):

Celik, Ahmet Ozan. “Experimental Investigation of the Role of Turbulence Fluctuations on Incipient Motion of Sediment.” 2011. Web. 19 Oct 2019.

Vancouver:

Celik AO. Experimental Investigation of the Role of Turbulence Fluctuations on Incipient Motion of Sediment. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/28731.

Council of Science Editors:

Celik AO. Experimental Investigation of the Role of Turbulence Fluctuations on Incipient Motion of Sediment. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/28731


Virginia Tech

23. Ecker, Tobias. Experimental Investigation of Particle Lag behind a Shock Wave using a Novel Laser Doppler Accelerometer.

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

 Determination of particle slip is a major concern for particle based measurements in un- heated supersonic facilities, as it is a limiting factor for the… (more)

Subjects/Keywords: Acceleration; Particle Drag; Multiphase Flow; Laser Doppler; Supersonic; Slip Flow; Non-Continuum Flow

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APA (6th Edition):

Ecker, T. (2011). Experimental Investigation of Particle Lag behind a Shock Wave using a Novel Laser Doppler Accelerometer. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34720

Chicago Manual of Style (16th Edition):

Ecker, Tobias. “Experimental Investigation of Particle Lag behind a Shock Wave using a Novel Laser Doppler Accelerometer.” 2011. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/34720.

MLA Handbook (7th Edition):

Ecker, Tobias. “Experimental Investigation of Particle Lag behind a Shock Wave using a Novel Laser Doppler Accelerometer.” 2011. Web. 19 Oct 2019.

Vancouver:

Ecker T. Experimental Investigation of Particle Lag behind a Shock Wave using a Novel Laser Doppler Accelerometer. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/34720.

Council of Science Editors:

Ecker T. Experimental Investigation of Particle Lag behind a Shock Wave using a Novel Laser Doppler Accelerometer. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/34720


Virginia Tech

24. Forest, Jonathan Bradley. The Wall Pressure Spectrum of High Reynolds Number Rough-Wall Turbulent Boundary Layers.

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

 The presence of roughness on a surface subject to high Reynolds number flows promotes the formation of a turbulent boundary layer and the generation of… (more)

Subjects/Keywords: high Reynolds number; rough wall; turbulent boundary layer; surface pressure

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APA (6th Edition):

Forest, J. B. (2012). The Wall Pressure Spectrum of High Reynolds Number Rough-Wall Turbulent Boundary Layers. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31114

Chicago Manual of Style (16th Edition):

Forest, Jonathan Bradley. “The Wall Pressure Spectrum of High Reynolds Number Rough-Wall Turbulent Boundary Layers.” 2012. Masters Thesis, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/31114.

MLA Handbook (7th Edition):

Forest, Jonathan Bradley. “The Wall Pressure Spectrum of High Reynolds Number Rough-Wall Turbulent Boundary Layers.” 2012. Web. 19 Oct 2019.

Vancouver:

Forest JB. The Wall Pressure Spectrum of High Reynolds Number Rough-Wall Turbulent Boundary Layers. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/31114.

Council of Science Editors:

Forest JB. The Wall Pressure Spectrum of High Reynolds Number Rough-Wall Turbulent Boundary Layers. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/31114


Virginia Tech

25. Rock, Christopher. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors.

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

 A flush-wall injector model and a strut injector model representative of state of the art scramjet engine combustion chambers were experimentally studied in a cold-flow… (more)

Subjects/Keywords: Fuel Injection; Mixing; Hypersonic Propulsion; Supersonic Combustion; Scramjet

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APA (6th Edition):

Rock, C. (2010). Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77208

Chicago Manual of Style (16th Edition):

Rock, Christopher. “Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors.” 2010. Doctoral Dissertation, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/77208.

MLA Handbook (7th Edition):

Rock, Christopher. “Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors.” 2010. Web. 19 Oct 2019.

Vancouver:

Rock C. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/77208.

Council of Science Editors:

Rock C. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/77208


Virginia Tech

26. Allison, Darcy L. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.

Degree: PhD, Aerospace Engineering, 2013, Virginia Tech

 This work seeks to develop multidisciplinary design optimization (MDO) methods to find the optimal design of a particular aircraft called an Efficient Supersonic Air Vehicle… (more)

Subjects/Keywords: aircraft design; multidisciplinary design optimization; supersonic military aircraft; design of computer experiments

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APA (6th Edition):

Allison, D. L. (2013). Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24187

Chicago Manual of Style (16th Edition):

Allison, Darcy L. “Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.” 2013. Doctoral Dissertation, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/24187.

MLA Handbook (7th Edition):

Allison, Darcy L. “Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.” 2013. Web. 19 Oct 2019.

Vancouver:

Allison DL. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/24187.

Council of Science Editors:

Allison DL. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/24187


Virginia Tech

27. Alexander, William Nathan. Sound from Rough Wall Boundary Layers.

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

 Turbulent flow over a rough surface produces sound that radiates outside the near wall region. This noise source is often at a lower level than… (more)

Subjects/Keywords: roughness noise; wall-jet; microphone array

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APA (6th Edition):

Alexander, W. N. (2011). Sound from Rough Wall Boundary Layers. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/29246

Chicago Manual of Style (16th Edition):

Alexander, William Nathan. “Sound from Rough Wall Boundary Layers.” 2011. Doctoral Dissertation, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/29246.

MLA Handbook (7th Edition):

Alexander, William Nathan. “Sound from Rough Wall Boundary Layers.” 2011. Web. 19 Oct 2019.

Vancouver:

Alexander WN. Sound from Rough Wall Boundary Layers. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/29246.

Council of Science Editors:

Alexander WN. Sound from Rough Wall Boundary Layers. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/29246


Virginia Tech

28. Leslie, Brian Robert. Design, Analysis, and Testing of Nanoparticle-Infused Thin Film Sensors for Low Skin Friction Applications.

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

 Accurate measurement of skin friction in complex flows is important for: documentation and monitoring of fluid system performance, input information for flow control, development of… (more)

Subjects/Keywords: Aerospace; Fluid Dynamics; Skin Friction; Sensor; Instrumentation; CFD; FEM; Turbulent; Design

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APA (6th Edition):

Leslie, B. R. (2012). Design, Analysis, and Testing of Nanoparticle-Infused Thin Film Sensors for Low Skin Friction Applications. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/19199

Chicago Manual of Style (16th Edition):

Leslie, Brian Robert. “Design, Analysis, and Testing of Nanoparticle-Infused Thin Film Sensors for Low Skin Friction Applications.” 2012. Doctoral Dissertation, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/19199.

MLA Handbook (7th Edition):

Leslie, Brian Robert. “Design, Analysis, and Testing of Nanoparticle-Infused Thin Film Sensors for Low Skin Friction Applications.” 2012. Web. 19 Oct 2019.

Vancouver:

Leslie BR. Design, Analysis, and Testing of Nanoparticle-Infused Thin Film Sensors for Low Skin Friction Applications. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/19199.

Council of Science Editors:

Leslie BR. Design, Analysis, and Testing of Nanoparticle-Infused Thin Film Sensors for Low Skin Friction Applications. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/19199


Virginia Tech

29. Valyrakis, Manousos. Initiation of Particle Movement in Turbulent Open Channel Flow.

Degree: PhD, Civil Engineering, 2011, Virginia Tech

 The objective of this thesis is to investigate the flow conditions that lead to coarse grain entrainment at near incipient motion conditions. Herein, a new… (more)

Subjects/Keywords: extreme value theory; impulse and energy event based criteria; wavelet analysis; onset of particle entrainment; neuro-fuzzy inference systems; coherent flow structures

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APA (6th Edition):

Valyrakis, M. (2011). Initiation of Particle Movement in Turbulent Open Channel Flow. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/27289

Chicago Manual of Style (16th Edition):

Valyrakis, Manousos. “Initiation of Particle Movement in Turbulent Open Channel Flow.” 2011. Doctoral Dissertation, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/27289.

MLA Handbook (7th Edition):

Valyrakis, Manousos. “Initiation of Particle Movement in Turbulent Open Channel Flow.” 2011. Web. 19 Oct 2019.

Vancouver:

Valyrakis M. Initiation of Particle Movement in Turbulent Open Channel Flow. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/27289.

Council of Science Editors:

Valyrakis M. Initiation of Particle Movement in Turbulent Open Channel Flow. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/27289


Virginia Tech

30. Mallik, Wrik. Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization.

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

 This study highlights the aeroelastic behavior of very flexible truss-braced wing (TBW) aircraft designs obtained through a multidisciplinary design optimization (MDO) framework. Several improvements to… (more)

Subjects/Keywords: Aeroelasticity; Multidisciplinary Design Optimization; Truss-Braced Wing Aircraft; Variable Geometry Raked Wingtip; State-space Aerodynamics

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APA (6th Edition):

Mallik, W. (2016). Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71650

Chicago Manual of Style (16th Edition):

Mallik, Wrik. “Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization.” 2016. Doctoral Dissertation, Virginia Tech. Accessed October 19, 2019. http://hdl.handle.net/10919/71650.

MLA Handbook (7th Edition):

Mallik, Wrik. “Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization.” 2016. Web. 19 Oct 2019.

Vancouver:

Mallik W. Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/10919/71650.

Council of Science Editors:

Mallik W. Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71650

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