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Articles 151 - 180 of 513
Full-Text Articles in Mechanical Engineering
Assessing Thickness Accommodation Techniques For Deployable Hexagonal Origami Space Arrays, Collin Ynchausti
Assessing Thickness Accommodation Techniques For Deployable Hexagonal Origami Space Arrays, Collin Ynchausti
Utah Space Grant Consortium
Origami-based and origami-inspired designs provide paths to achieve highly compact, stowable designs, that can be deployed to large surface areas. This potential is highly beneficial to the area of space antennas and LIDAR as these require compact stowing in a launch payload, but large apertures when deployed in space. Because the engineering materials used to build these antennas are thick, thickness accommodation techniques must be applied to realize the same folding motions as the zero-thickness models. This paper presents a hexagonal twist origami pattern in thick materials using three different thickness accommodation techniques. These techniques are compared. The metrics used …
Electromagnetic 3d Printing For Responsive Architectures With An Orthogonal Magnetic Field, Brian Elder
Electromagnetic 3d Printing For Responsive Architectures With An Orthogonal Magnetic Field, Brian Elder
Utah Space Grant Consortium
The integration of nanomaterials with 3D printing can enable the creation of responsive architecture with highly tunable functional properties. Magnetic nanopatterning is attractive for its ability to produce untethered, high energy density actuation with a broad range of applications. For example, biocompatible materials (such as silicone rubber) can be programmed in an extrusion-based 3D printing process to create a responsive medical soft robot structure.
Defect Detection Limits For Additively Manufactured Parts Using Current Thermography Techniques, Nicholas J. Wallace
Defect Detection Limits For Additively Manufactured Parts Using Current Thermography Techniques, Nicholas J. Wallace
Utah Space Grant Consortium
Additive manufacturing (AM) will support NASA in their moon and mars missions by reducing the amount of redundant equipment carried into space and by providing crew members with the flexibility to design and create parts as needed. The ability to monitor the quality of these additively manufactured parts is critical, especially when using recycled or in-situ materials as NASA plans to do. This project assesses the possibility of detecting small, shallow AM defects with existing active thermography techniques. An axisymmetric, numerical model was created in COMSOL to simulate the heat transfer within AM structures during active thermography. The effects of …
Aerodynamic Interactions Of Synchronized Propellers, Nathan Welker
Aerodynamic Interactions Of Synchronized Propellers, Nathan Welker
Utah Space Grant Consortium
Emerging advances in electric-propulsion technology are enabling aircraft to use distributed electric propulsion (DEP) to increase efficiency and maneuverability. Distributed electric propulsion can also provide unique take-off and landing abilities which are not commonly found on traditional aircraft. The implementation of DEP effectively decreases the spacing between propellers, introducing complex aerodynamic interactions that are not well understood. This study aims to obtain experimental measurements of the flow fields of synchronized propellers at close-proximity in a side-by-side configuration using both 2D particle image velocimetry (PIV) and 3D stereoscopic PIV (SPIV) in a wind tunnel. The results of this work will be …
Sonic Boom Loudness Reduction Through Localized Supersonic Aircraft Equivalent-Area Changes, Troy A. Abraham
Sonic Boom Loudness Reduction Through Localized Supersonic Aircraft Equivalent-Area Changes, Troy A. Abraham
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
The NASA University Leadership Initiative (ULI) titled “Adaptive Aerostructures for Revolutionary Civil Supersonic Transportation” looks to study the feasibility of distributed structural adaptivity on a supersonic aircraft for maintaining acceptable en-route sonic boom loudness during overland flight. The ULI includes a team of industry and university partners that are working together to develop and implement the systems necessary to accomplish this goal.
The Utah State University Aerolab is a member of this ULI team and has been tasked with developing and using low-fidelity supersonic aerodynamic and sonic boom predictions tools to rapidly study the effects of localized geometry changes on …
Computational Fluid Dynamics Benchmark Validation Experiment Of Plenum-To-Plenum Flow Through Vertical Heated Parallel Channels, Austin W. Parker
Computational Fluid Dynamics Benchmark Validation Experiment Of Plenum-To-Plenum Flow Through Vertical Heated Parallel Channels, Austin W. Parker
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
The next generation of nuclear power plants will have higher efficiency and improved safety, among other benefits; one attractive option is the high temperature gas reactor. An ability to predict the physics that occur within the reactor under normal conditions and accident scenarios is necessary before it receives regulatory licensing for use. The flow through a high temperature gas reactor involves complex interactions of heat transfer, fluids, and solids.
One method for simulating complex fluid dynamics is called Computational Fluid Dynamics. These simulations have already been used to predict the complex fluid flows found in high temperature gas reactors. Predicting …
Modeling, Simulation And Optimization Of Nuclear Hybrid Energy Systems Using Openmodelica And Raven, Stephen Michael Hills
Modeling, Simulation And Optimization Of Nuclear Hybrid Energy Systems Using Openmodelica And Raven, Stephen Michael Hills
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Nuclear hybrid energy systems (NHES) are a viable option to combine renewable energy sources, such as wind, with a less fluctuating energy source. Given recent development and their inherent safer and modular design, small modular reactors (SMRs), which are smaller versions of a nuclear reactor, can play an instrumental role in complementing renewables and supporting carbon-free power sectors in the coming decades. With increasing population and demand for clean water, Freeze desalination (FD), which uses freezing to separate water from salt, is a possible way to produce clean water while converting excess power from a SMR into stored thermal energy …
Development Of A Variable Extensometer Method For Measuring Ductility Scaling Parameters, Adam J. Smith
Development Of A Variable Extensometer Method For Measuring Ductility Scaling Parameters, Adam J. Smith
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Ductility is the measure of how much a material can stretch before separation. It is usually measured in percent elongation, which is the amount a material stretches divided by its original length before stretching. This is an important property to understand for both the design for performance and safety. A material’s ductility can be influenced by several factors including heat treatment, machining, temperature, and radiation dose. Materials used in nuclear energy facilities are often exposed to all these factors, and it is important to be able to understand ductility at each possible combination.
Ductility is usually characterized through tension tests …
Low-Fidelity Method For Rapid Aerostructural Optimisation And Design-Space Exploration Of Planar Wings, Jeffrey D. Taylor, Doug F. Hunsaker
Low-Fidelity Method For Rapid Aerostructural Optimisation And Design-Space Exploration Of Planar Wings, Jeffrey D. Taylor, Doug F. Hunsaker
Mechanical and Aerospace Engineering Student Publications and Presentations
During early phases of wing design, analytic and low-fidelity methods are often used to identify promising design concepts. In many cases, solutions obtained using these methods provide intuition about the design space that is not easily obtained using higher-fidelity methods. This is especially true for aerostructural design. However, many analytic and low-fidelity aerostructural solutions are limited in application to wings with specific planforms and weight distributions. Here, a numerical method for minimising induced drag with structural constraints is presented that uses approximations that apply to unswept planar wings with arbitrary planforms and weight distributions. The method is applied to the …
Sensitivity And Estimation Of Flying-Wing Aerodynamic, Propulsion, And Inertial Parameters Using Simulation, Jaden Thurgood, Douglas F. Hunsaker
Sensitivity And Estimation Of Flying-Wing Aerodynamic, Propulsion, And Inertial Parameters Using Simulation, Jaden Thurgood, Douglas F. Hunsaker
Mechanical and Aerospace Engineering Student Publications and Presentations
This paper explores the difficulties of aircraft system identification, specifically parameter estimation, for a rudderless aircraft. A white box method is used in conjunction with a nonlinear six degree-of-freedom aerodynamic model for the equations of motion in order to estimate 33 parameters that govern the aerodynamic, inertial, and propulsion forces within the mathematical model. The analysis is conducted in the time-domain of system identification. Additionally, all the parameters are estimated using a single flight rather than a series of shorter flights dedicated to estimating specific sets of parameters as is typically done. A final flight plan is developed with a …
Practical Implementation Of A General Numerical Lifting-Line Method, Cory D. Goates, Douglas F. Hunsaker
Practical Implementation Of A General Numerical Lifting-Line Method, Cory D. Goates, Douglas F. Hunsaker
Mechanical and Aerospace Engineering Student Publications and Presentations
A general numerical lifting-line method provides corrections to overcome the singularities inherent in the lifting-line downwash integrals in certain cases. These singularities have previously limited the scope of lifting-line theory to straight wings not in sideslip; in all other cases, more traditional numerical approaches to solving Prandtl's hypothesis fail to grid converge. However, this general numerical lifting-line method grid converges even for swept wings and wings in sideslip. In the current work, we apply the general numerical lifting-line method to any number of wings with arbitrary geometry. We also provide a dimensional derivation of the basic general numerical lifting-line equations …
3d-Printed Wings With Morphing Trailing-Edge Technology, Benjamin C. Moulton, Douglas F. Hunsaker
3d-Printed Wings With Morphing Trailing-Edge Technology, Benjamin C. Moulton, Douglas F. Hunsaker
Mechanical and Aerospace Engineering Student Publications and Presentations
In recent years, various groups have attempted to improve aircraft efficiency using wings with morphing trailing-edge technology. Most of these solutions are difficult to manufacture or have limited morphing capability. The present paper outlines a research effort to develop an easy to manufacture, fully 3D-printed morphing wing. This approach is advantageous due to the low cost, minimal man-hours required for manufacturing, and speed at which design iterations can be explored. Several prototypes were designed and tested and lessons learned from these iterations have been documented. Additionally, printer settings have been tested and catalogued to assist others attempting to reproduce these …
Comparison Of Theoretical And High-Fidelity Aerostructural Solutions, Jeffrey D. Taylor, Douglas F. Hunsaker
Comparison Of Theoretical And High-Fidelity Aerostructural Solutions, Jeffrey D. Taylor, Douglas F. Hunsaker
Mechanical and Aerospace Engineering Student Publications and Presentations
As contemporary aerostructural research in aircraft design trends toward high-fidelity computational methods, aerostructural solutions based on theory are often neglected or forgotten. In fact, in many modern aerostructural wing optimization studies, the elliptic lift distribution is used as a benchmark in place of theoretical aerostructural solutions with more appropriate constraints. In this paper, we review several theoretical aerostructural solutions that could be used as benchmark cases for wing design studies, and we compare them to high-fidelity solutions with similar constraints. Solutions are presented for studies with 1) constraints related to the wing integrated bending moment, 2) constraints related to the …
Characterization Of The Common Research Model Wing For Low-Fidelity Aerostructural Analysis, Jeffrey D. Taylor, Douglas F. Hunsaker
Characterization Of The Common Research Model Wing For Low-Fidelity Aerostructural Analysis, Jeffrey D. Taylor, Douglas F. Hunsaker
Mechanical and Aerospace Engineering Student Publications and Presentations
A characterization of the Common Research Model (CRM) wing for low-fidelity aerostructural optimization is presented. The geometric and structural properties are based on the CAD geometries and finite-element models for the CRM wing and the undeflected Common Research Model Wing (uCRM). Three approximations are presented for the elastic axis from previously-published studies on wing boxes similar to the uCRM, and approximations of the flexural and torsional rigidity are presented from a previously-published study using the uCRM wing. The characterization presented in this paper is intended to be used within low-fidelity aerostructural analysis tools to facilitate rapid design optimization and exploratory …
Open Source Software Problems In Heat Transfer To Explore Assumptions And Models, Benjamin Pepper, Amir Behbahanian, Nick Roberts
Open Source Software Problems In Heat Transfer To Explore Assumptions And Models, Benjamin Pepper, Amir Behbahanian, Nick Roberts
Course Materials
Energy2D software can be downloaded here: http://energy.concord.org/energy2d/
After opening the application, choose File -> Open and select one of the .e2d files available for download here under additional files. Click the Run button to get started.
The main download has a document that provides a detailed description of the adaptation of a freely available software program, Energy2D, for problems focused on the exploration and limitations of assumptions made in models commonly used in an undergraduate heat transfer course. The motivation for creating homework problems that use Energy2D is to explore the accuracy and limitations of the models used in heat …
The Earliest Drawings Of Dogs, Myles Bradley
The Earliest Drawings Of Dogs, Myles Bradley
Fall Student Research Symposium 2020
The oldest depictions of dogs ever found are over 8,000 years old, found carved into a cliff in the desert of Saudi Arabia. Studies show, however, that dogs are found coexisting with humans as far back as 30,000 years ago. If this is the case, "Why does it take so long for dogs to appear in human artwork?" Dogs have certainly been an integral part of human society for almost as long as they've been around, so what do these early images reveal about the ancient relationship between dogs and man? This paper explores possible answers to both of these …
Static Heat Exchanger For The Wireless Charging Of Electric Vehicles, James Mullen
Static Heat Exchanger For The Wireless Charging Of Electric Vehicles, James Mullen
Fall Student Research Symposium 2020
The USU College of Engineering partnered with the Aspire NSF Engineering Research Center to develop wireless charging pads for electric vehicles. These concrete pads, when placed in roadways, charge the batteries of electric vehicles that pass over them. As the pads charge vehicles, they produce excessive thermal energy (heat), which dissipates slowly through the surrounding concrete. This excess heat reduces the efficiency of the charging apparatus and can damage the imbedded electrical components. To manage the pad temperatures, the USU Nanoscale Thermal Energy Lab proposed to submerge the heat-generating elements in a Phase Change Material (PCM). As a solid, a …
The Dog As A Trend In Art, Whitney Stewart
The Dog As A Trend In Art, Whitney Stewart
Fall Student Research Symposium 2020
I have always believed that art is one of the biggest forms of communication and signs of cultural assimilation and it has been throughout history. I choose to explore the role that dogs play in this theme. From changes in the symbolism of the dog and the ethics of breeding, art reveals a lot about our furry friends. While I learn much about dogs by themselves, the way we represent them also says a lot about our society. Do we see animals as more than us in some way and less in others? Is a dog painting really about the …
Data From: Computational Fluid Dynamics Benchmark Validation Experiment Of Plenum-To-Plenum Flow Through Vertical Heated Parallel Channels, Austin W. Parker, Barton L. Smith
Data From: Computational Fluid Dynamics Benchmark Validation Experiment Of Plenum-To-Plenum Flow Through Vertical Heated Parallel Channels, Austin W. Parker, Barton L. Smith
Browse all Datasets
This research is focused on the thermal mixing region of parallel jets entering an upper plenum. The highly-coupled thermal-fluid physics are relevant to plenum-to-plenum flow in High Temperature Gas Reactors such as thermal striping phenomena. Experimentally measured boundary conditions and system response quantities for use in Computational Fluid Dynamics were tabulated and published for public use.
Coin Recovery Ii, Carly Lofthouse
Coin Recovery Ii, Carly Lofthouse
Undergraduate Honors Capstone Projects
Western Metals Recycling (WMR), a subsidiary of NUCOR Steel, is a metals recycling company with a location in Plymouth, Utah. At Plymouth, a 50 NT/hr. non-ferrous recovery plant uses eddy current technology to generate a non-ferrous product called zorba. Zorba is a mix of aluminum, copper, brass, zinc, printed circuit boards, coins, lead, and the like. (Figure 1) The market value of zorba varies but generally ranges from $0.30 to $0.50 per pound. The value of the coins (not including pennies) is much higher than zorba price. The team's objective is to upgrade and optimize the existing trommel equipment to …
Molecular Mechanisms And Design Of Hydrogen-Bonded Materials For Thermal Applications, Jinlong He
Molecular Mechanisms And Design Of Hydrogen-Bonded Materials For Thermal Applications, Jinlong He
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Heat transfer at the nanoscale plays an important role in determining the reliability and performance of many innovative advanced materials technologies such as nanoelectronics, semiconductor, biomedical devices, polymers, and composites. Extensive efforts have been made to design materials with extraordinary thermal properties. However, fundamental understanding of heat transfer in many of these materials is still not lacking, because the thermal transport processes are governed by several factors including molecular morphology and chemical bonding. Among these factors, the atomic bonding between two dissimilar materials or within single materials is of particular interest due to its ubiquity and importance in physical processes. …
Modeling And Simulation Of A Supercritical Co2-Liquid Sodium Compact Heat Exchanger For Sodium Fast Reactors, Hailei Wang, Sean M. Kissick
Modeling And Simulation Of A Supercritical Co2-Liquid Sodium Compact Heat Exchanger For Sodium Fast Reactors, Hailei Wang, Sean M. Kissick
Mechanical and Aerospace Engineering Faculty Publications
The study focuses on modeling and simulations of sodium-sCO2 intermediary compact heat exchangers for sodium-cooled fast reactors (SFR). A simplified 1-D analytical model was developed in companion with a 3-D CFD model. Using classic heat transfer correlations for Nusselt number, some simulation results using the 1-D model have achieved reasonable match with the CFD simulation results for longer channels (i.e., 40 cm and 80 cm). However, for short channel (10 cm) when axial conduction within the sodium fluid is significant, the 1-D model significantly over-predicted the heat transfer effectiveness. By incorporating the temperature-jump model, the 1-D model can extend its …
Minimum Induced Drag For Tapered Wings Including Structural Constraints, Jeffrey D. Taylor, Douglas F. Hunsaker
Minimum Induced Drag For Tapered Wings Including Structural Constraints, Jeffrey D. Taylor, Douglas F. Hunsaker
Mechanical and Aerospace Engineering Student Publications and Presentations
LIFTING-LINE theory [1,2] is the foundation for much of our understanding of finite-wing aerodynamics. Solutions based on lifting-line theory are widely accepted and have been shown to be in good agreement with CFD [3-10]. From Prandtl’s analytic solution to the classical lifting-line equation [1,2], the wing section-lift distribution can be expressed as a Fourier series of the form [11]
bL~ (θ)/L = (4/π)[sin(θ) + Σ∞n-2 Bnsin(nθ)]; θ = cos-1(-2z/b) (1)
where b is the wingspan, L~ is the local wing section lift, L is the total wing lift, z is the spanwise …
Minimising Induced Drag With Weight Distribution, Lift Distribution, Wingspan, And Wing-Structure Weight, Warren F. Phillips, Douglas F. Hunsaker, Jeffrey D. Taylor
Minimising Induced Drag With Weight Distribution, Lift Distribution, Wingspan, And Wing-Structure Weight, Warren F. Phillips, Douglas F. Hunsaker, Jeffrey D. Taylor
Mechanical and Aerospace Engineering Student Publications and Presentations
Because the wing-structure weight required to support the critical wing section bending moments is a function of wingspan, net weight, weight distribution, and lift distribution, there exists an optimum wingspan and wing-structure weight for any fixed net weight, weight distribution, and lift distribution, which minimises the induced drag in steady level flight. Analytic solutions for the optimum wingspan and wing-structure weight are presented for rectangular wings with four different sets of design constraints. These design constraints are fixed lift distribution and net weight combined with 1) fixed maximum stress and wing loading, 2) fixed maximum deflection and wing loading, 3) …
Benchmarking Of A Mobile Phone Particle Image Velocimetry System, David Armijo
Benchmarking Of A Mobile Phone Particle Image Velocimetry System, David Armijo
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
One of the most important tools in a fluid dynamics laboratory is a particle image velocimetry (PIV) system. This system can measure the speed of a fluid flow simply by taking high-speed images of the motion of the fluid, then applying PIV cross-correlation software to calculate speed from the resulting images. The mI-PIV project is in the process of designing a new method of performing PIV by putting the cross-correlation software on a mobile phone application, called mobile Instructional PIV (mI-PIV). This system is an innovative stepping stone in making PIV systems more widely available. It is designed to be …
Thermal Modeling And Analysis Of Roadway Embedded Wireless Power Transfer Modules, Arden N. Barnes
Thermal Modeling And Analysis Of Roadway Embedded Wireless Power Transfer Modules, Arden N. Barnes
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Wireless charging of electric vehicles is a developing technology which potentially increases efficiency and safety. It also allows for charging vehicles while they are moving by having charging stations embedded in the roadway. Because roadways are thermally insulating, it is important to know how the heat from the charging stations will move through the roadway, which will allow further research into whether the heat will cause damage to the components in the station or to the roadway. This thesis studies the way the heat moves through concrete with wireless charging coils embedded in it. This is accomplished by measuring the …
Optimization Of Aileron Spanwise Size And Shape To Minimize Induced Drag In Roll With Correlating Adverse Yaw, Joshua R. Brincklow
Optimization Of Aileron Spanwise Size And Shape To Minimize Induced Drag In Roll With Correlating Adverse Yaw, Joshua R. Brincklow
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Most modern aircraft make use of modifying the main wing in flight to begin a roll. In many cases, this is done with a discrete control surface known as an aileron. The lift, drag, and moments for the wing are affected in part by the location and size of the ailerons along the length of the wing. The lift, drag, and moments can be found using a lifting-line theory that considers the circulation in airflow from many small sections of the wing. To minimize the drag due to lift on the wing, the ailerons must be optimized for the best …
Fluted Films Caused By Gravity Driven Water Drainage From Vertical Tubes, Matthew B. Jones
Fluted Films Caused By Gravity Driven Water Drainage From Vertical Tubes, Matthew B. Jones
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
When a stationary mass of water in a vertical tube is suddenly released, it creates a variety of artistic shapes and behaviors as it escapes the tube exit. As the descending water accelerates in the tube, friction along the tube wall slows the outer radius, resulting in a moving film entrained on the tube that trails the main body of water. When this film exits the tube, surface tension, gravity, and inertia interact to cause the film to create a wide variety of shapes, including jets, tubes, water bells, champagne glasses, and bubbles; rich forms that appear in other natural …
Pitched Baseballs And The Seam Shifted Wake, Andrew W. Smith
Pitched Baseballs And The Seam Shifted Wake, Andrew W. Smith
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
An experiment was conducted to investigate the effect that seams have on the way a baseball moves through the air. An examination of the airflow around a baseball led to the understanding that when seams are in certain areas on the baseball's surface the airflow changes. A subsequent experiment was performed which showed that when these changes in airflow were on one side of the baseball more than the other, the ball moved away from the side with the seams. This movement is in a different direction than the movement direction caused by a ball's spin. These experiments were done …
Transient Thermal Modeling Of Bioprocessing Equipment, Cody M. Cummings
Transient Thermal Modeling Of Bioprocessing Equipment, Cody M. Cummings
All Graduate Theses and Dissertations, Spring 1920 to Summer 2023
Bioprocessing is leveraging cells to produce high value, lifesaving products. Precise environmental control is needed to maintain integrity of the bioprocessing production process. Temperature control requires both appropriate equipment choice and correct control parameter selection. To aid in the equipment selection process, enable better understanding of equipment capacity, and enable optimization of control parameters, a transient thermal model of both heat transfer characteristics and control systems was created in silico.