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You searched for +publisher:"Virginia Tech" +contributor:("O\'Brien, Walter F. Jr."). Showing records 1 – 30 of 162 total matches.

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1. Frohnapfel, Dustin Joseph. Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion.

Degree: MS, Mechanical Engineering, 2016, Virginia Tech

 Next generation aircraft design focuses on highly integrated airframe/engine architectures that exploit advantages in system level efficiency and performance. One such design concept incorporates boundary… (more)

Subjects/Keywords: Turbofan Engine; Inlet Distortion; Swirl; Secondary Flow; Ground Test

…testing was conducted using a modified turbofan research engine at the Virginia Tech… …Virginia Tech Turbomachinery and Propulsion Research Laboratory. A StreamVane swirl distortion… …to the Virginia Tech StreamVane Method which generated a three-dimensional swirl distortion… …JT15D-1 turbofan engine research platform at the Virginia Tech Turbomachinery and Propulsion… …station at the Virginia Tech Montgomery Executive Airport. Located less than one quarter mile… 

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APA (6th Edition):

Frohnapfel, D. J. (2016). Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71323

Chicago Manual of Style (16th Edition):

Frohnapfel, Dustin Joseph. “Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion.” 2016. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/71323.

MLA Handbook (7th Edition):

Frohnapfel, Dustin Joseph. “Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion.” 2016. Web. 30 Sep 2020.

Vancouver:

Frohnapfel DJ. Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/71323.

Council of Science Editors:

Frohnapfel DJ. Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion. [Masters Thesis]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71323

2. Hoopes, Kevin M. A New Method for Generating Swirl Inlet Distortion for Jet Engine Research.

Degree: MS, Mechanical Engineering, 2013, Virginia Tech

 Jet engines operate by ingesting incoming air, adding momentum to it, and exhausting it through a nozzle to produce thrust. Because of their reliance on… (more)

Subjects/Keywords: Swirl Inlet Distortion; Swirl Inlet Distortion Generation

…many years. Recently, the Virginia Tech Turbomachinery and Propulsion Research Laboratory has… 

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APA (6th Edition):

Hoopes, K. M. (2013). A New Method for Generating Swirl Inlet Distortion for Jet Engine Research. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49545

Chicago Manual of Style (16th Edition):

Hoopes, Kevin M. “A New Method for Generating Swirl Inlet Distortion for Jet Engine Research.” 2013. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/49545.

MLA Handbook (7th Edition):

Hoopes, Kevin M. “A New Method for Generating Swirl Inlet Distortion for Jet Engine Research.” 2013. Web. 30 Sep 2020.

Vancouver:

Hoopes KM. A New Method for Generating Swirl Inlet Distortion for Jet Engine Research. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/49545.

Council of Science Editors:

Hoopes KM. A New Method for Generating Swirl Inlet Distortion for Jet Engine Research. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/49545

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

Degree: MS, Aerospace 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. Many… (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 September 30, 2020. 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. 30 Sep 2020.

Vancouver:

Quickel RA. Mount Interference and Flow Angle Impacts on Unshielded Total Temperature Probes. [Internet] [Masters thesis]. Virginia Tech; 2019. [cited 2020 Sep 30]. 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

4. Janka, Adam Martin. Methods of Diffusing Pulse Detonation Combustion.

Degree: MS, Mechanical Engineering, 2014, Virginia Tech

 Pulse detonation combustion has been of interest for many years since it offers several advantages over standard deflagrative combustion. In theory, detonative combustion is a… (more)

Subjects/Keywords: Pressure gain combustion; pulse detonation combustion; wave dynamics

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APA (6th Edition):

Janka, A. M. (2014). Methods of Diffusing Pulse Detonation Combustion. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49152

Chicago Manual of Style (16th Edition):

Janka, Adam Martin. “Methods of Diffusing Pulse Detonation Combustion.” 2014. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/49152.

MLA Handbook (7th Edition):

Janka, Adam Martin. “Methods of Diffusing Pulse Detonation Combustion.” 2014. Web. 30 Sep 2020.

Vancouver:

Janka AM. Methods of Diffusing Pulse Detonation Combustion. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/49152.

Council of Science Editors:

Janka AM. Methods of Diffusing Pulse Detonation Combustion. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/49152

5. Pham, Khang Duy. Quasi-Static Tensile and Fatigue Behavior of Extrusion Additive Manufactured ULTEM 9085.

Degree: MS, Mechanical Engineering, 2018, Virginia Tech

 Extrusion additive manufacturing technologies may be utilized to fabricate complex geometry devices. However, the success of these additive manufactured devices depends upon their ability to… (more)

Subjects/Keywords: Material Properties; Additive Manufacturing; Fused Deposition Modeling; ULTEM 9085

…Figure 55. S-N Curve Generated by Virginia Tech… …utilizing the Fortus 400MC machine that is available at Virginia Tech rather than relying on an… 

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APA (6th Edition):

Pham, K. D. (2018). Quasi-Static Tensile and Fatigue Behavior of Extrusion Additive Manufactured ULTEM 9085. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82047

Chicago Manual of Style (16th Edition):

Pham, Khang Duy. “Quasi-Static Tensile and Fatigue Behavior of Extrusion Additive Manufactured ULTEM 9085.” 2018. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/82047.

MLA Handbook (7th Edition):

Pham, Khang Duy. “Quasi-Static Tensile and Fatigue Behavior of Extrusion Additive Manufactured ULTEM 9085.” 2018. Web. 30 Sep 2020.

Vancouver:

Pham KD. Quasi-Static Tensile and Fatigue Behavior of Extrusion Additive Manufactured ULTEM 9085. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/82047.

Council of Science Editors:

Pham KD. Quasi-Static Tensile and Fatigue Behavior of Extrusion Additive Manufactured ULTEM 9085. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/82047

6. Smith, Katherine Nicole. New Methodology for the Estimation  of StreamVane Design Flow Profiles.

Degree: MS, Mechanical Engineering, 2018, Virginia Tech

 Inlet distortion research has become increasingly important over the past several years as demands for aircraft flight efficiency and performance has increased. To accommodate these… (more)

Subjects/Keywords: Inlet Distortion; Swirl; Parameter Estimation

…Square-Error StreamFlow StreamVane Virginia Tech MCMC Simulation Software x 1 Introduction… …StreamVane discharge profiles utilized at Virginia Tech. StreamFlow generates predictions of how a… …here and other research conducted at Virginia Tech with StreamVanes aims to target those… …generation device created by Virginia Tech is identified as the StreamVane, and has the ability to… …research at Virginia Tech to measure the effect of swirl in a turbofan engine inlet. Guimarães… 

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APA (6th Edition):

Smith, K. N. (2018). New Methodology for the Estimation  of StreamVane Design Flow Profiles. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82039

Chicago Manual of Style (16th Edition):

Smith, Katherine Nicole. “New Methodology for the Estimation  of StreamVane Design Flow Profiles.” 2018. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/82039.

MLA Handbook (7th Edition):

Smith, Katherine Nicole. “New Methodology for the Estimation  of StreamVane Design Flow Profiles.” 2018. Web. 30 Sep 2020.

Vancouver:

Smith KN. New Methodology for the Estimation  of StreamVane Design Flow Profiles. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/82039.

Council of Science Editors:

Smith KN. New Methodology for the Estimation  of StreamVane Design Flow Profiles. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/82039


Virginia Tech

7. Mondscehin, Brian David. Evaluation of Alternate Bearing Designs in a High Speed Automotive Turbocharger.

Degree: MS, Mechanical Engineering, 2010, Virginia Tech

 Automotive turbochargers experience self-excited instabilities through the majority of their operating speed range. The results of these instabilities can cause damage to the bearings, shafts,… (more)

Subjects/Keywords: Turbocharger; Stability; Bearing; Design

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APA (6th Edition):

Mondscehin, B. D. (2010). Evaluation of Alternate Bearing Designs in a High Speed Automotive Turbocharger. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33513

Chicago Manual of Style (16th Edition):

Mondscehin, Brian David. “Evaluation of Alternate Bearing Designs in a High Speed Automotive Turbocharger.” 2010. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/33513.

MLA Handbook (7th Edition):

Mondscehin, Brian David. “Evaluation of Alternate Bearing Designs in a High Speed Automotive Turbocharger.” 2010. Web. 30 Sep 2020.

Vancouver:

Mondscehin BD. Evaluation of Alternate Bearing Designs in a High Speed Automotive Turbocharger. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/33513.

Council of Science Editors:

Mondscehin BD. Evaluation of Alternate Bearing Designs in a High Speed Automotive Turbocharger. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/33513


Virginia Tech

8. Gvozdich, Grant Gregory. Modeling the Transient Effects of High Energy Subsystems on High-Performance Aerospace Systems.

Degree: MS, Mechanical Engineering, 2011, Virginia Tech

 As directed energy technology continues to evolve and become a viable weapon alternative, a need exists to investigate the impacts of these applications without a… (more)

Subjects/Keywords: aerospace; thermal storage; directed energy weapon; solid-state laser

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APA (6th Edition):

Gvozdich, G. G. (2011). Modeling the Transient Effects of High Energy Subsystems on High-Performance Aerospace Systems. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35704

Chicago Manual of Style (16th Edition):

Gvozdich, Grant Gregory. “Modeling the Transient Effects of High Energy Subsystems on High-Performance Aerospace Systems.” 2011. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/35704.

MLA Handbook (7th Edition):

Gvozdich, Grant Gregory. “Modeling the Transient Effects of High Energy Subsystems on High-Performance Aerospace Systems.” 2011. Web. 30 Sep 2020.

Vancouver:

Gvozdich GG. Modeling the Transient Effects of High Energy Subsystems on High-Performance Aerospace Systems. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/35704.

Council of Science Editors:

Gvozdich GG. Modeling the Transient Effects of High Energy Subsystems on High-Performance Aerospace Systems. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/35704


Virginia Tech

9. Ferrar, Anthony Maurice. Measurements of Flow in Boundary Layer Ingesting Serpentine Inlets.

Degree: MS, Mechanical Engineering, 2011, Virginia Tech

 Highly integrated airframe-propulsion systems featuring ingestion of the airframe boundary layer oer reduced noise, emissions, and fuel consumption. Embedded engine systems are envisioned which require… (more)

Subjects/Keywords: boundary layer ingestion; wake ingestion; distortion; flow control; diffuser; inlet

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APA (6th Edition):

Ferrar, A. M. (2011). Measurements of Flow in Boundary Layer Ingesting Serpentine Inlets. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36408

Chicago Manual of Style (16th Edition):

Ferrar, Anthony Maurice. “Measurements of Flow in Boundary Layer Ingesting Serpentine Inlets.” 2011. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/36408.

MLA Handbook (7th Edition):

Ferrar, Anthony Maurice. “Measurements of Flow in Boundary Layer Ingesting Serpentine Inlets.” 2011. Web. 30 Sep 2020.

Vancouver:

Ferrar AM. Measurements of Flow in Boundary Layer Ingesting Serpentine Inlets. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/36408.

Council of Science Editors:

Ferrar AM. Measurements of Flow in Boundary Layer Ingesting Serpentine Inlets. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/36408


Virginia Tech

10. Pickering, Todd Michael. Methods for Validation of a Turbomachinery Rotor Blade Tip Timing System.

Degree: MS, Mechanical Engineering, 2014, Virginia Tech

 This research developed two innovative test methods that were used to experimentally evaluate the performance of a novel blade tip timing (BTT) system from Prime… (more)

Subjects/Keywords: Blade Tip Timing; Non-Intrusive Stress Measurement System; Turbomachinery; Optical Sensor; Piezoelectric

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APA (6th Edition):

Pickering, T. M. (2014). Methods for Validation of a Turbomachinery Rotor Blade Tip Timing System. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/47496

Chicago Manual of Style (16th Edition):

Pickering, Todd Michael. “Methods for Validation of a Turbomachinery Rotor Blade Tip Timing System.” 2014. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/47496.

MLA Handbook (7th Edition):

Pickering, Todd Michael. “Methods for Validation of a Turbomachinery Rotor Blade Tip Timing System.” 2014. Web. 30 Sep 2020.

Vancouver:

Pickering TM. Methods for Validation of a Turbomachinery Rotor Blade Tip Timing System. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/47496.

Council of Science Editors:

Pickering TM. Methods for Validation of a Turbomachinery Rotor Blade Tip Timing System. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/47496


Virginia Tech

11. Steele, Steven Cory Wyatt. Optimal Engine Selection and Trajectory Optimization using Genetic Algorithms for Conceptual Design Optimization of Resuable Launch Vehicles.

Degree: MS, Mechanical Engineering, 2015, Virginia Tech

 Proper engine selection for Reusable Launch Vehicles (RLVs) is a key factor in the design of low cost reusable launch systems for routine access to… (more)

Subjects/Keywords: Trajectory Optimization; Engine Selection; Reusable Launch Vehicle; RLV; Two Stage to Orbit; TSTO

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APA (6th Edition):

Steele, S. C. W. (2015). Optimal Engine Selection and Trajectory Optimization using Genetic Algorithms for Conceptual Design Optimization of Resuable Launch Vehicles. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/51771

Chicago Manual of Style (16th Edition):

Steele, Steven Cory Wyatt. “Optimal Engine Selection and Trajectory Optimization using Genetic Algorithms for Conceptual Design Optimization of Resuable Launch Vehicles.” 2015. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/51771.

MLA Handbook (7th Edition):

Steele, Steven Cory Wyatt. “Optimal Engine Selection and Trajectory Optimization using Genetic Algorithms for Conceptual Design Optimization of Resuable Launch Vehicles.” 2015. Web. 30 Sep 2020.

Vancouver:

Steele SCW. Optimal Engine Selection and Trajectory Optimization using Genetic Algorithms for Conceptual Design Optimization of Resuable Launch Vehicles. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/51771.

Council of Science Editors:

Steele SCW. Optimal Engine Selection and Trajectory Optimization using Genetic Algorithms for Conceptual Design Optimization of Resuable Launch Vehicles. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/51771


Virginia Tech

12. Weise, Peter Carl. Mission-Integrated Synthesis/Design Optimization of Aerospace Subsystems under Transient Conditions.

Degree: MS, Mechanical Engineering, 2012, Virginia Tech

 The equations governing the thermodynamic behavior of a military aircraft have been implemented by the Air Force Research Lab (AFRL) and other Integrated Vehicle Energy… (more)

Subjects/Keywords: optimization; design of experiments; surrogate modeling; aerospace

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APA (6th Edition):

Weise, P. C. (2012). Mission-Integrated Synthesis/Design Optimization of Aerospace Subsystems under Transient Conditions. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76855

Chicago Manual of Style (16th Edition):

Weise, Peter Carl. “Mission-Integrated Synthesis/Design Optimization of Aerospace Subsystems under Transient Conditions.” 2012. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/76855.

MLA Handbook (7th Edition):

Weise, Peter Carl. “Mission-Integrated Synthesis/Design Optimization of Aerospace Subsystems under Transient Conditions.” 2012. Web. 30 Sep 2020.

Vancouver:

Weise PC. Mission-Integrated Synthesis/Design Optimization of Aerospace Subsystems under Transient Conditions. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/76855.

Council of Science Editors:

Weise PC. Mission-Integrated Synthesis/Design Optimization of Aerospace Subsystems under Transient Conditions. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/76855


Virginia Tech

13. Lucas, James Redmond. Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance.

Degree: MS, Mechanical Engineering, 2013, Virginia Tech

 Boundary Layer Ingestion (BLI) is currently being researched as a potential method to improve efficiency and decrease emissions for the next generation of commercial aircraft.… (more)

Subjects/Keywords: Performance; Boundary Layer Ingestion; Turbofan Engine; Inlet Distortion

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APA (6th Edition):

Lucas, J. R. (2013). Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23272

Chicago Manual of Style (16th Edition):

Lucas, James Redmond. “Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance.” 2013. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/23272.

MLA Handbook (7th Edition):

Lucas, James Redmond. “Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance.” 2013. Web. 30 Sep 2020.

Vancouver:

Lucas JR. Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/23272.

Council of Science Editors:

Lucas JR. Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23272


Virginia Tech

14. Bailey, Justin Mark. The Influence of Development and Fan/Screen Interaction on Screen-Generated Total Pressure Distortion Profiles.

Degree: MS, Mechanical Engineering, 2014, Virginia Tech

 The rising interest in fan performance in the presence of total pressure distortion, a topic of fundamental interest for integrated airframe/engine architectures, has led to… (more)

Subjects/Keywords: Total Pressure Distortion Development; Fan/Screen Interaction; Wire-mesh Screens

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APA (6th Edition):

Bailey, J. M. (2014). The Influence of Development and Fan/Screen Interaction on Screen-Generated Total Pressure Distortion Profiles. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/25288

Chicago Manual of Style (16th Edition):

Bailey, Justin Mark. “The Influence of Development and Fan/Screen Interaction on Screen-Generated Total Pressure Distortion Profiles.” 2014. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/25288.

MLA Handbook (7th Edition):

Bailey, Justin Mark. “The Influence of Development and Fan/Screen Interaction on Screen-Generated Total Pressure Distortion Profiles.” 2014. Web. 30 Sep 2020.

Vancouver:

Bailey JM. The Influence of Development and Fan/Screen Interaction on Screen-Generated Total Pressure Distortion Profiles. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/25288.

Council of Science Editors:

Bailey JM. The Influence of Development and Fan/Screen Interaction on Screen-Generated Total Pressure Distortion Profiles. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/25288


Virginia Tech

15. Carmack, Andrew Cardin. Heat Transfer and Flow Measurements in Gas Turbine Engine Can and Annular Combustors.

Degree: MS, Mechanical Engineering, 2012, Virginia Tech

 A comparison study between axial and radial swirler performance in a gas turbine can combustor was conducted by investigating the correlation between combustor flow field… (more)

Subjects/Keywords: Swirler; Combustor liner cooing; Infrared Thermal Imaging; Dry Low Emission (DLE) combustors

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APA (6th Edition):

Carmack, A. C. (2012). Heat Transfer and Flow Measurements in Gas Turbine Engine Can and Annular Combustors. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32466

Chicago Manual of Style (16th Edition):

Carmack, Andrew Cardin. “Heat Transfer and Flow Measurements in Gas Turbine Engine Can and Annular Combustors.” 2012. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/32466.

MLA Handbook (7th Edition):

Carmack, Andrew Cardin. “Heat Transfer and Flow Measurements in Gas Turbine Engine Can and Annular Combustors.” 2012. Web. 30 Sep 2020.

Vancouver:

Carmack AC. Heat Transfer and Flow Measurements in Gas Turbine Engine Can and Annular Combustors. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/32466.

Council of Science Editors:

Carmack AC. Heat Transfer and Flow Measurements in Gas Turbine Engine Can and Annular Combustors. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/32466


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 September 30, 2020. http://hdl.handle.net/10919/30857.

MLA Handbook (7th Edition):

Tran, Kathleen. “One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths.” 2010. Web. 30 Sep 2020.

Vancouver:

Tran K. One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2020 Sep 30]. 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. Siddens, Aaron Jeffrey. A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures.

Degree: MS, Mechanical Engineering, 2012, Virginia Tech

 This work presents a detailed predictive modeling methodology for comprehensive crashworthiness analysis of advanced jet engine forward sections, containing hybrid and composite structures, when subjected… (more)

Subjects/Keywords: Composite damage; Hybrid structures; Progressive failure; Jet engine forward section; Soft impact

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APA (6th Edition):

Siddens, A. J. (2012). A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76957

Chicago Manual of Style (16th Edition):

Siddens, Aaron Jeffrey. “A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures.” 2012. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/76957.

MLA Handbook (7th Edition):

Siddens, Aaron Jeffrey. “A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures.” 2012. Web. 30 Sep 2020.

Vancouver:

Siddens AJ. A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/76957.

Council of Science Editors:

Siddens AJ. A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/76957


Virginia Tech

18. Farina, Jordan Thomas. Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization.

Degree: MS, Mechanical Engineering, 2010, Virginia Tech

 The continued use of fossil fuels along with a rise in energy demand has led to increasing levels of carbon emissions over the past years.… (more)

Subjects/Keywords: Hydrogen; Lean-Premixed; Gas Turbine

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APA (6th Edition):

Farina, J. T. (2010). Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31067

Chicago Manual of Style (16th Edition):

Farina, Jordan Thomas. “Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization.” 2010. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/31067.

MLA Handbook (7th Edition):

Farina, Jordan Thomas. “Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization.” 2010. Web. 30 Sep 2020.

Vancouver:

Farina JT. Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/31067.

Council of Science Editors:

Farina JT. Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/31067


Virginia Tech

19. Mitchell, Morgan Adrienne. Passive Noise Control in Incubators.

Degree: MS, Mechanical Engineering, 2013, Virginia Tech

 Incubators in the Neonatal Intensive Care Unit (NICU) are known to produce high Sound Pressure Levels (SPL) that can have detrimental effects on infants. Currently… (more)

Subjects/Keywords: finite element model; anechoic chamber; incubator; acoustics; passive noise control treatments

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APA (6th Edition):

Mitchell, M. A. (2013). Passive Noise Control in Incubators. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/51603

Chicago Manual of Style (16th Edition):

Mitchell, Morgan Adrienne. “Passive Noise Control in Incubators.” 2013. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/51603.

MLA Handbook (7th Edition):

Mitchell, Morgan Adrienne. “Passive Noise Control in Incubators.” 2013. Web. 30 Sep 2020.

Vancouver:

Mitchell MA. Passive Noise Control in Incubators. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/51603.

Council of Science Editors:

Mitchell MA. Passive Noise Control in Incubators. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/51603


Virginia Tech

20. Kishore, Ravi Anant. Small-scale Wind Energy Portable Turbine (SWEPT).

Degree: MS, Mechanical Engineering, 2013, Virginia Tech

 Large Scale Wind Turbines (LSWTs) have been extensively examined for decades but very few studies have been conducted on the small scale wind turbines (SSWTs)… (more)

Subjects/Keywords: Small scale wind turbine; Diffuser augmented wind turbine; Computational Fluid Dynamics; Portable Power; Wind Energy

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APA (6th Edition):

Kishore, R. A. (2013). Small-scale Wind Energy Portable Turbine (SWEPT). (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23099

Chicago Manual of Style (16th Edition):

Kishore, Ravi Anant. “Small-scale Wind Energy Portable Turbine (SWEPT).” 2013. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/23099.

MLA Handbook (7th Edition):

Kishore, Ravi Anant. “Small-scale Wind Energy Portable Turbine (SWEPT).” 2013. Web. 30 Sep 2020.

Vancouver:

Kishore RA. Small-scale Wind Energy Portable Turbine (SWEPT). [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/23099.

Council of Science Editors:

Kishore RA. Small-scale Wind Energy Portable Turbine (SWEPT). [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23099


Virginia Tech

21. Buehrle, Bridget Erin. Modeling of Small-Scale Wind Energy Conversion Systems.

Degree: MS, Mechanical Engineering, 2013, Virginia Tech

 As wind turbines are increasingly being adopted for meeting growing energy needs, their implementation for personal home use in the near future is imminent. There… (more)

Subjects/Keywords: diffuser; wind; vertical axis; tubercles; small-scale

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APA (6th Edition):

Buehrle, B. E. (2013). Modeling of Small-Scale Wind Energy Conversion Systems. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50920

Chicago Manual of Style (16th Edition):

Buehrle, Bridget Erin. “Modeling of Small-Scale Wind Energy Conversion Systems.” 2013. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/50920.

MLA Handbook (7th Edition):

Buehrle, Bridget Erin. “Modeling of Small-Scale Wind Energy Conversion Systems.” 2013. Web. 30 Sep 2020.

Vancouver:

Buehrle BE. Modeling of Small-Scale Wind Energy Conversion Systems. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/50920.

Council of Science Editors:

Buehrle BE. Modeling of Small-Scale Wind Energy Conversion Systems. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/50920


Virginia Tech

22. Jain, Sakshi. Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring.

Degree: MS, Mechanical Engineering, 2014, Virginia Tech

 The present study investigates mixed out aerodynamic loss coefficient measurements for a high turning, contoured endwall passage under transonic operating conditions in presence of upstream… (more)

Subjects/Keywords: Gas Turbines; Transonic Cascade; Secondary Flow; Upstream Purge Slot; Mateface gap; Endwall Contouring

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APA (6th Edition):

Jain, S. (2014). Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/54577

Chicago Manual of Style (16th Edition):

Jain, Sakshi. “Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring.” 2014. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/54577.

MLA Handbook (7th Edition):

Jain, Sakshi. “Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring.” 2014. Web. 30 Sep 2020.

Vancouver:

Jain S. Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/54577.

Council of Science Editors:

Jain S. Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/54577


Virginia Tech

23. Zetts, Andrew Wyatt. The Impact of a Microturbine Power Plant on an Off Road Range Extended Electric Vehicle.

Degree: MS, Mechanical Engineering, 2015, Virginia Tech

 The purpose of this thesis is to examine the feasibility of using a microturbine to power an off-road Series Hybrid Autonomous Vehicle (SHEV), and evaluate… (more)

Subjects/Keywords: Microturbine; HEV; Autonomy

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APA (6th Edition):

Zetts, A. W. (2015). The Impact of a Microturbine Power Plant on an Off Road Range Extended Electric Vehicle. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/72974

Chicago Manual of Style (16th Edition):

Zetts, Andrew Wyatt. “The Impact of a Microturbine Power Plant on an Off Road Range Extended Electric Vehicle.” 2015. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/72974.

MLA Handbook (7th Edition):

Zetts, Andrew Wyatt. “The Impact of a Microturbine Power Plant on an Off Road Range Extended Electric Vehicle.” 2015. Web. 30 Sep 2020.

Vancouver:

Zetts AW. The Impact of a Microturbine Power Plant on an Off Road Range Extended Electric Vehicle. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/72974.

Council of Science Editors:

Zetts AW. The Impact of a Microturbine Power Plant on an Off Road Range Extended Electric Vehicle. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/72974


Virginia Tech

24. Jagani, Jakin Nitinkumar. Design of Percutaneous Dual Propeller Pump to assist Patients with Single Functional Ventricle.

Degree: MS, Mechanical Engineering, 2018, Virginia Tech

 Various congenital heart defects (CHDs) are characterized by the existence of a single functional ventricle, which perfuses both the systemic and pulmonary circulation in parallel.… (more)

Subjects/Keywords: Cavopulmonary Assist Device; Dual Propeller Pump; Computational Fluid Dynamics; Hemodynamics; Blood Damage; Experimental Testing

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APA (6th Edition):

Jagani, J. N. (2018). Design of Percutaneous Dual Propeller Pump to assist Patients with Single Functional Ventricle. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82667

Chicago Manual of Style (16th Edition):

Jagani, Jakin Nitinkumar. “Design of Percutaneous Dual Propeller Pump to assist Patients with Single Functional Ventricle.” 2018. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/82667.

MLA Handbook (7th Edition):

Jagani, Jakin Nitinkumar. “Design of Percutaneous Dual Propeller Pump to assist Patients with Single Functional Ventricle.” 2018. Web. 30 Sep 2020.

Vancouver:

Jagani JN. Design of Percutaneous Dual Propeller Pump to assist Patients with Single Functional Ventricle. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/82667.

Council of Science Editors:

Jagani JN. Design of Percutaneous Dual Propeller Pump to assist Patients with Single Functional Ventricle. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/82667


Virginia Tech

25. Mack, Elizabeth. Hemodynamic Optimization of a Passive Assist Total Cavopulmonary Connector for ages 1-20.

Degree: MS, Biomedical Engineering and Mechanics, 2018, Virginia Tech

 Currently, the surgical procedure followed by the majority of cardiac surgeons to address a nonfunctioning right portion of the heart is the Fontan procedure, which… (more)

Subjects/Keywords: Computational Fluid Dynamics; Heart; Hemodynamics; Biomedical

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APA (6th Edition):

Mack, E. (2018). Hemodynamic Optimization of a Passive Assist Total Cavopulmonary Connector for ages 1-20. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/84450

Chicago Manual of Style (16th Edition):

Mack, Elizabeth. “Hemodynamic Optimization of a Passive Assist Total Cavopulmonary Connector for ages 1-20.” 2018. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/84450.

MLA Handbook (7th Edition):

Mack, Elizabeth. “Hemodynamic Optimization of a Passive Assist Total Cavopulmonary Connector for ages 1-20.” 2018. Web. 30 Sep 2020.

Vancouver:

Mack E. Hemodynamic Optimization of a Passive Assist Total Cavopulmonary Connector for ages 1-20. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/84450.

Council of Science Editors:

Mack E. Hemodynamic Optimization of a Passive Assist Total Cavopulmonary Connector for ages 1-20. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/84450


Virginia Tech

26. Blot, Dorian Matthew. Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing.

Degree: MS, Mechanical Engineering, 2013, Virginia Tech

 Endwall contouring has been widely studied as an effective measure to improve aerodynamic performance by reducing secondary flow strength. The effects of endwall contouring with… (more)

Subjects/Keywords: Gas Turbines; Transonic Cascade; Aerodynamics. Heat Transfer; Film Cooling; Upstream Purge Slot; Discrete Hole Cooling; Endwall

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APA (6th Edition):

Blot, D. M. (2013). Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/19257

Chicago Manual of Style (16th Edition):

Blot, Dorian Matthew. “Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing.” 2013. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/19257.

MLA Handbook (7th Edition):

Blot, Dorian Matthew. “Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing.” 2013. Web. 30 Sep 2020.

Vancouver:

Blot DM. Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/19257.

Council of Science Editors:

Blot DM. Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/19257


Virginia Tech

27. 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 September 30, 2020. http://hdl.handle.net/10919/77208.

MLA Handbook (7th Edition):

Rock, Christopher. “Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors.” 2010. Web. 30 Sep 2020.

Vancouver:

Rock C. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2020 Sep 30]. 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

28. Song, Yangkun. Development of Comprehensive Dynamic Damage Assessment Methodology for High-Bypass Air Breathing Propulsion Subject to Foreign Object Ingestion.

Degree: PhD, Mechanical Engineering, 2016, Virginia Tech

 Foreign object ingestion (FOI) into jet engines is a recurring scenario during the operation life of aircraft. Objects can range from as small as a… (more)

Subjects/Keywords: Foreign Object Ingestion; Fluid-Structure Interaction; Finite Element; Bird; Ice; Advanced Propulsion; Composite Structures; Particle Methods

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APA (6th Edition):

Song, Y. (2016). Development of Comprehensive Dynamic Damage Assessment Methodology for High-Bypass Air Breathing Propulsion Subject to Foreign Object Ingestion. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/93960

Chicago Manual of Style (16th Edition):

Song, Yangkun. “Development of Comprehensive Dynamic Damage Assessment Methodology for High-Bypass Air Breathing Propulsion Subject to Foreign Object Ingestion.” 2016. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/93960.

MLA Handbook (7th Edition):

Song, Yangkun. “Development of Comprehensive Dynamic Damage Assessment Methodology for High-Bypass Air Breathing Propulsion Subject to Foreign Object Ingestion.” 2016. Web. 30 Sep 2020.

Vancouver:

Song Y. Development of Comprehensive Dynamic Damage Assessment Methodology for High-Bypass Air Breathing Propulsion Subject to Foreign Object Ingestion. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/93960.

Council of Science Editors:

Song Y. Development of Comprehensive Dynamic Damage Assessment Methodology for High-Bypass Air Breathing Propulsion Subject to Foreign Object Ingestion. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/93960

29. Vincent, Tyler Graham. Total Temperature Probe Performance for Subsonic Flows using Mixed Fidelity Modeling.

Degree: PhD, Mechanical Engineering, 2019, Virginia Tech

 An accurate measurement of total temperature in turbomachinery flows remains critical for component life models and cycle performance optimization. While many techniques exist to measure… (more)

Subjects/Keywords: Total temperature; gas turbine instrumentation; Computational Fluid Dynamics (CFD); Conjugate Heat Transfer (CHT); conduction; convection; radiation

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APA (6th Edition):

Vincent, T. G. (2019). Total Temperature Probe Performance for Subsonic Flows using Mixed Fidelity Modeling. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/88867

Chicago Manual of Style (16th Edition):

Vincent, Tyler Graham. “Total Temperature Probe Performance for Subsonic Flows using Mixed Fidelity Modeling.” 2019. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/88867.

MLA Handbook (7th Edition):

Vincent, Tyler Graham. “Total Temperature Probe Performance for Subsonic Flows using Mixed Fidelity Modeling.” 2019. Web. 30 Sep 2020.

Vancouver:

Vincent TG. Total Temperature Probe Performance for Subsonic Flows using Mixed Fidelity Modeling. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/88867.

Council of Science Editors:

Vincent TG. Total Temperature Probe Performance for Subsonic Flows using Mixed Fidelity Modeling. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/88867

30. Mayo Jr, David Earl. The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities.

Degree: PhD, Mechanical Engineering, 2019, Virginia Tech

 Increasingly large and powerful engines are required as the mission requirements for tactical aircraft become more advanced. These demands come at the cost of an… (more)

Subjects/Keywords: fluid dynamics; supersonic jets; particle image velocimetry; compressible shear layers; jet noise; turbulence

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APA (6th Edition):

Mayo Jr, D. E. (2019). The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/93532

Chicago Manual of Style (16th Edition):

Mayo Jr, David Earl. “The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities.” 2019. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/93532.

MLA Handbook (7th Edition):

Mayo Jr, David Earl. “The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities.” 2019. Web. 30 Sep 2020.

Vancouver:

Mayo Jr DE. The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/93532.

Council of Science Editors:

Mayo Jr DE. The Turbulence Structure of Heated Supersonic Jets with Offset Total Temperature Non-Uniformities. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/93532

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