Mechanical Engineering Commons^™

Biological Agent Dispersal And Containment, Austin Williams, Ryker Hacking, Weston Craig

Mechanical and Aerospace Engineering

Purpose

• Model the flow of airborne anthrax surrogate particles through a training facility

• Design a training facility that will safely contain all the released particles

• Determine final location of the particles within the testing facility

• Determine most influential factors for particle containment

Importance

• Training for a bio-terrorist threat

• Researching airborne flow of particles is necessary to prepare for a potential threat

• Response plans depend on timely determination of the containment zone

Diffraction Efficiency Measurement Instrument: Demi, Usu Department Of Mechanical And Aerospace Engineering

Mechanical and Aerospace Engineering

• We designed an automated system to do help QC technicians who currently check the efficiency of VPHGs by hand.

• Why should your reader be interested?

VPHGs are used in lab equipment and medical instruments and more. The largest VPHGs (like the ones the DEMI tests) are used in giant telescopes and other astronomical applications.

Autonomous Fixed Wing Drone, Glen Wright, Case Haws, Duke Madson, Chandler Oaks, Cory Christensen, Ryan Mears, Mike Wells

Mechanical and Aerospace Engineering

Design an autonomous system for a fixed wing drone in order to fly a repeatable pattern for testing of RF communication equipment.

• Requirements:

– Fly a repeatable pattern

– 2 km range

– Transmit Telemetry points

– Switch between manual and autonomous

• Goals:

– Create a platform compatible with the second phase of the project

– Allow for autonomous takeoff and landing procedures

– Create a platform compatible with a host of airframes

Heated Chamber Capable Of Purging/Scrubbing Twelve Or More Gas Analyzers Of Co2 And H20 For Calibration, Cole Watson, Oliver Hulme, Trevan Cottle

Mechanical and Aerospace Engineering

• Build ergonomically friendly chamber capable of purging 12 or more Gas Analyzers to keep up with current demand.

• Designed shelfing to fit all three Campbell Scientific, Inc. (CSI) gas analyzers: EC150, EC155, and Irgason.

• Chamber has uniform air temperature that will be regulated to not go above 50 ℃.

• CSI Datalogger is used to collect analyzer data and control electronics from outside the chamber.

• Chamber is durable and easily moved.

Autoliv Flexible Windshield Reaction Surface, Perry Simpson, Jacob Bowman, Joshua Christensen, Ethan Moore

Mechanical and Aerospace Engineering

Summary: Currently Autoliv is testing airbags against a flat steel plate. Testing against a steel plate doesn’t provide accurate airbag rebound data. Autoliv also does most of the development in series with automotive companies. They do initial designs but cannot get accurate tests until test vehicles are built.

Problem: Create a fixture that will bend a surface to replicate the curvature of any windshield desired resulting in more accurate airbag rebound data.

Why: Solving this problem will result in higher accuracy and precision in airbag performance systems. The new test fixture will provide a better representation of how the airbag …

Ganging Multiple Mechanical Sun Trackers, Katie Clark, Ben Hansen, Ben Hill, Cody Kelley, Chris Twede

Mechanical and Aerospace Engineering

The scope of this project was to design a mechanical solar tracker that implemented the algorithm/patent developed by Dr. Nicholas Flann. The solar tracker needed to be able to gang with other units using a single motor. The designed tracking unit is intended to:

• Rotate 350 degrees

• Use 3 seasonal tracks to follow the sun

• Be adjustable for wind and snow loads

• Be constructed from readily available materials

Mini Rad-Dx Product Update, Tyler Child, Bradly Payne, Colton Smart, Morgan Ward

Mechanical and Aerospace Engineering

Improve Current model by:

• Redesigning case to accommodate 3 – AA batteries

• Improve ingress protection to IP67

• Make device look more Rugged

• Eliminate one of the two LCD screens

• Design for injection molding production

• Develop a mobile app

Direct Pedal Actuation, Tyler Fallentine, Mitch Peterson, Bryce Fisher, Sam Hartvigsen, Alexander Bird

Mechanical and Aerospace Engineering

Problem Description:

• The Team shall deliver a working prototype for direct pedal actuation of the brake and throttle for use in remote control of a vehicle.

• The delivered design shall:

• Measure 15 in. by 9 in. by 13 in.

• Fit in 90% of tested vehicles.

• Meet force, speed, back drive force, etc.

• Install in under 10 minutes.

Small Satellite Reaction Wheel, Corey Creager, Kalan Juhasz, Jeremy Wiser, Jake Laub, Christopher Wartena

Mechanical and Aerospace Engineering

• A reaction wheel uses torque to control the attitude of a satellite.

• The requirements specify a torque, a momentum, and a confined volume.

Solar Array Deployment Test Gravity Offloader System, Braden Call, Matthew Calvin, Chris Debenham, Christian Marriot, Mason Onkes

Mechanical and Aerospace Engineering

• Space Dynamics Lab (SDL) has started to develop larger satellites and larger solar arrays are required to power the spacecrafts. These larger arrays are harder to test

• Larger solar panels need their weight from gravity offloaded to prevent damage to their joints. The joints are not designed to hold their own weight

• Space Dynamics Lab requested our design be able to function in a vacuum to simulate the microgravity environment as closely as possible.

• While gravity offloading systems have been designed in the past, a vacuum-compatible and passive design brings a new and unique challenge

Usu Mars Rover Team, Usu Department Of Mechanical And Aerospace Engineering

Mechanical and Aerospace Engineering

The University Rover Challenge capstone project presents university students the opportunity to design, fabricate and test a rover to compete in the annual international Mars Society URC Competition held in Hanksville, Utah. The URC Competition consists of four separate missions including Extreme Retrieval & Delivery, Equipment Servicing, Science, and Autonomous Traversal. Each mission requires advanced subsystems onboard the rover to accomplish mission tasks in a timely manner.

The 2020 USU URC team is divided up into four subteams to accomplish each mission including Power/Drive, Navigation/Communications/Autonomy, Operations, and Science. Admission to the URC Competition is highly competitive since the competition is …

Westech Process Control, William Clarke, Ammon Mccarthy

Mechanical and Aerospace Engineering

The WesTech Engineering company is looking into utilizing MatLab Simulink to increase productivity.

Zagg Innovation Program: Led Focusing Case, Kyle Douglas, Travis Halverson, Derek Wilkins, Jessica Williams

Mechanical and Aerospace Engineering

Background: The ZAGG Innovation Program has the goal of creating innovative concepts and products for the telecommunication and consumer electronic retail channels.

Chosen Product: After deliberating over 30 generated product ideas with ZAGG representatives, the team chose to develop a phone case that would focus a cellphone camera flash into a practical flashlight beam.

Product Goals:

• Decrease beam angle and light increase projection distance

• Durability to withstand regular use and drops

• Keep the product as simple as possible, with minimal added bulk and parts

• Case will not obstruct the field of view of …

Experimental Evaluation Of Strength Degradation Temperature For Carbon Epoxy Filament Wound Composite, Jai Krishna Mishra, Surya Prakash Rao Ch Dr, Subhash Chandra Bose P Dr, Kishore Nath N Dr, Rama Rao Golla Mr

International Journal of Aviation, Aeronautics, and Aerospace

Polymeric composites have been widely used in various structural and thermal aerospace applications. Polymeric composites having high strength and high modulus reinforcement are ideally suited for lot of critical aerospace applications as structure is designed with high specific strength and high specific modulus. In case of launch vehicles/ missile one such application is design and manufacturing of solid rocket motor casing with polymeric composites as it give high performance and reduces inert weight of propulsion system. The high specific strength and high specific modulus of composite materials makes it ideal choice for designing the composite rocket motor case (CRMC). These …

Portable Leak Test System, Tyler Pulli, Joseph Arnell, Luke Osterhout, Dustyn Roberts

Mechanical and Aerospace Engineering

Idaho National Laboratories requires an airtight seal on transportation casks to ship radioactive material. To ensure that the cask is air-tight, a system needs to be designed to measure whether air is leaking out of the seal and determines if the cask passes or fails.

Test Dummy Positioning For Autoliv Ogden, Ut, Dianne Althouse, John Garrett, Ty Johnston, Ridge Jones

Mechanical and Aerospace Engineering

• The Team shall deliver a proof of concept prototype to Autoliv for its use in positioning test dummies for Out-of-Position (OOP) airbag testing

• This is to improve set-up timing and accuracy without operator to operator variation.

• The device should work for the placing of three-year-old, six- year-old, and 5th percentile female test dummies.

• There are two OOP: head on IP (instrumentation panel) and chest on IP.

Peridynamic Approaches For Damage Prediction In Carbon Fiber And Carbon Nanotube Yarn Reinforced Polymer Composites, Forrest E. Baber

Theses and Dissertations

Aerospace structures are increasingly utilizing advanced composites because of their high specific modulus and specific strength. While the introduction of these material systems can dramatically decrease weight, they pose unique certification challenges, often requiring extensive experimental testing in each stage of the design cycle. The expensive and time-consuming nature of experimental testing necessitates the advancement of simulation methodologies to both aid in the certification process and assist in the exploration of the microstructure design space.

Peridynamic (PD) theory, originating from Sandia National Lab’s in the early 2000’s, is a nonlocal continuum-based method that reformulates the equation of motion into an …

Characterizing Premixed Syngas Combustion In Micro-Channels, Sunita Pokharel

Graduate Theses, Dissertations, and Problem Reports (ETD)

Increasing demands in the next-generation portable power-generation devices such as unmanned aerial vehicles (UAV), microsatellite thrusters, micro-chemical reactors and sensors calls for fuels with high specific energy and low emissions to meet the current demand of green energy. Fuel-lean synthesis gas (syngas) meets both these requirements exhibiting a promising route to a clean and green environment. Thus, it is of critical importance to characterize syngas combustion and understand its properties in the micro-combustion industry. In addition to complicated flame dynamics in microscale systems, varying the syngas-fuel mixture composition as well as the boundary conditions and geometry of a combustor significantly …

Impact Of Isolated Atmospheric Aging Processes On The Cloud Condensation Nuclei Activation Of Soot Particles, Franz Friebel, Prem Lobo, David Neubauer, Ulrike Lohmann, Saskia Drossaart Van Dusseldorp, Evelyn Mühlhofer, Amewu A. Mensah

Mechanical and Aerospace Engineering Faculty Research & Creative Works

The largest contributors to the uncertainty in assessing the anthropogenic contribution in radiative forcing are the direct and indirect effects of aerosol particles on the Earth's radiative budget. Soot particles are of special interest since their properties can change significantly due to aging processes once they are emitted into the atmosphere. Probably the largest obstacle for the investigation of these processes in the laboratory is the long atmospheric lifetime of 1 week, requiring tailored experiments that cover this time span. This work presents results on the ability of two types of soot, obtained using a miniCAST soot generator, to act …

The Investigation Of Noise, Vibrations And Emissions Of Aero-Gas Turbine Combustion With Synthetic Kerosene Fuels, Margaret Kilpatrick

Honors College Theses

Climatic changes from aviation emissions are complex and include effects of greenhouse gases such as: CO2, NOx, and aerosols. For that reason, the objectives of this study were to investigate the noise, vibrations and emissions characteristics of synthetic kerosene combustion in an aerospace gas turbine to reduce the engine’s environmental impact. Sustainably produced synthetic kerosene is known for having low soot emissions due to little to no aromatics (compounds that create particle pollutants), and for being a sustainable alternative fuel source to imported oil. The noise and sound levels were collected using Bruel & Kjaer microphones to measure various mid …

Multiscale Modeling Of Fracture In Quasi-Brittle Materials Using Bifurcation Analysis And Element Elimination Method, Keyvan Zare Rami

Department of Civil and Environmental Engineering: Dissertations, Theses, and Student Research

Analyzing the fracture of heterogeneous materials is a complex problem, due to the fact that the mechanical behavior of a heterogeneous material is strongly dependent on a variety of factors, such as its microstructure, the properties of each constituent, and interactions between them. Therefore, these factors must be effectively taken into account for accurate analysis, for which the multiscale method has been widely used. In this scheme, the computational homogenization method is used to obtain the effective macroscopic properties of a heterogeneous material based on the response of a Representative Volume Element (RVE). The growth of damage in an RVE …

Pulsed Detonation Engine Nozzle Design And Analysis, Rahul Kumar

Mechanical and Aerospace Engineering Dissertations - Archive

For a hypersonic flight mission, different flight regimes have been recognized. The successful and efficient operation of the aircraft to traverse through all the flight regimes requires the integration of various propulsion cycles into a single flow path. Using the phenomenon of detonation initiation and propagation, a multi-mode detonation based propulsion concept was proposed for hypersonic flight. Of the different modes proposed, it was recognized that the efficient operation of Normal Detonation Wave Engine (NDWE) mode and Oblique Detonation Wave Engine (ODWE) mode played an important role as they delivered thrust at critical parts of the trajectory. For this study, …

Improving Compressive Strength Of High Modulus Carbon-Fiber Reinforced Polymeric Composite With Varying Modulus Fibers, Sarvenaz Ghaffari

Mechanical and Aerospace Engineering Dissertations - Archive

There has been a strong demand in using high-modulus (HM) carbon-fiber composites potentially enabling lightweight aircraft structures with significant weight savings. However, extremely low fiber-direction compressive strength has been a well-recognized weakness of the HM composites, preventing their implementation in aircraft platforms. Fiber-direction compressive strength of HM and intermediate-modulus (IM) carbon fiber-reinforced polymers (CFRP’s) is presumably governed by microstructural stability. However, strong decrease in fiber-direction compressive strength of HM carbon-fiber composites, compared to their intermediate modulus (IM) counterparts, contradicts predictions from available microstructural buckling theories. A recent work demonstrated that significant improvement in the fiber-direction compressive strength of HM carbon-fiber …

Numerical Study Of Detonation Flame Arrestor Performance And Detonation Interaction With The Arrestor Element, Hoden Ali Farah

Mechanical and Aerospace Engineering Dissertations - Archive

A numerical study of detonation propagation and interaction with a flame arrestor product in a combustible gas/vapor transport pipeline system is conducted. The flame arrestor element is modeled as a porous medium using the Forchheimer equation, which is incorporated in the governing conservation equations as a momentum sink. The Forchheimer porous medium model is then used to model the flow through a representative four-inch detonation flame arrestor and is validated with experimental data. The detonation propagation simulation is modeled with the Reynolds averaged Navier-Stokes (RANS) equations extended for reacting flow. A 21-step chemical kinetic mechanism with 10 species is used …

Numerical Study Of High–Frequency Fluidic Valve Injectors For Detonation Engine Applications, Sushma Yalavarthi

Mechanical and Aerospace Engineering Dissertations - Archive

The feasibility of fluidic valves for use in detonation-based engines was studied numerically. The fluidic valve acted by shutting off reactant flow through the high pressure behind detonation waves propagating past the valve opening. The valve which featured a plenum cavity was mounted to the side of a pulsed detonation engine, an arrangement that allowed the valve to be characterized under a sustained operation. A series of different cavity lengths were studied. Further, a numerical study of the high-frequency fluidic valve was conducted by using a two-dimensional reactive Euler solver. A 19–step elementary mechanism was employed for the stoichiometric oxyhydrogen …

Dynamics Of A Pulse Detonation Engine Driven Linear Power Generator, Umang Umeshkumar Dighe

Mechanical and Aerospace Engineering Dissertations - Archive

The dynamics of a pulse detonation engine driven linear power generator were studied. For an ideal pulse detonation engine, the thrust generated is in the form of a piecewise function given by the Endo-Fujiwara model. Nonlinear electromagnetic damping is also introduced in the system due to the rare earth permanent magnets present in the linear generator architecture. Various linear generator topologies were studied using static magnetic analysis. Two configurations of a single degree-of-freedom oscillator system, one with a linear spring restoring force and another with geometric nonlinear spring restoring force, were investigated to study any potential advantages of using nonlinear …

Droplet-Based Microextraction Of Dna Enabled By Electrowetting-On-Dielectric Digital Microfluidics, Shubhodeep Paul

Mechanical and Aerospace Engineering Dissertations - Archive

In recent years there have been significant advances in micro/nanotechnologies employing miniaturized platforms to achieve efficient sample pre-processing, separation, and quantification processes. The idea of bringing several lab-scale protocols on to a single chip, i.e., a lab-on-a-chip (LOC) device along with automation, is a reality now. Miniaturization of biochemical operations usually handled in a laboratory has numerous advantages, such as cost effectiveness, multiplexing, assay speed, and sensitivity. Microfluidic technologies used in LOC devices can manipulate tiny volumes of samples and reagents to perform on-chip protocols with minimal human intervention. Electrowetting-on-dielectric (EWOD)-based digital microfluidics (DMF) is one of the LOC platforms …

Assessment Of Material State In Composites Using Global Dielectric State Variable, Vamsee Vadlamundi

Mechanical and Aerospace Engineering Dissertations - Archive

Composites are heterogeneous in nature and a fundamental understanding of the material response to applied mechanical, thermal, electrical and other multi-physical fields is required to efficiently design and synthesize the material system and demands attention to long-term behavior in particular. Unlike metals, composites are designed to develop distributed damage and initiation of a single microscopic crack does not individually affect the strength/life of these materials. Therefore, the primary interest is not in single local events but in the process of interaction of multiple events that have a collective global effect on the material behavior. The interaction of these local events …

Development And Testing Of A Control Strategy For Dynamic Cooling At Rack Level In Data Centers, Amrutha Valli Rachakonda

Mechanical and Aerospace Engineering Theses - Archive

Cooling is a critical part of data center’s infrastructure, and with ongoing demands in data processing and storage, thermal management issues are of great concern. Some imperative methods of removing heat are either using air or liquid (preferably water or refrigerant). When high power density modules are involved, liquid cooling addresses some of the problems faced by air cooling as liquid coolants have higher thermal capacitance. Also, in the case of multi-chip modules, a non-uniform heating due to multi-core generates hot-spots and increases temperature gradients across the module. A dynamic cold plate along with a self-regulated flow control device was …

Autonomous Carrier Landing Of A Fixed-Wing Uav With Airborne Deck Motion Estimation, Metin Kus

Mechanical and Aerospace Engineering Theses - Archive

This study focuses on the design, implementation, and evaluation of an autonomous carrier landing system featuring an airborne deck motion estimation module. The three-dimensional dynamics of a fixed-wing UAV with the actuator and engine dynamics are considered. A carrier motion model that accounts for the perturbations caused by various sea states is built. An airborne measurement system, which is composed of a calibrated camera and light-emitting beacons, is utilized to detect several coplanar target points on the moving carrier deck. The known correspondence between the locations of the target points and their coordinates on the focal plane of the camera …