141-150 of 278 results
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REU Site: Exploring Aerospace Research at the Intersection of Mechanics, Materials Science, and Aerospace Physiology
PI Foram Madiyar
CO-I Alberto Mello
This Project is founded by National Science Foundation, under REU site. This project aims to educate students and promote scientific research in materials and aerospace science that encompasses not only building lighter and smarter materials for aerospace applications but also understanding the impact of the space environment on physiological and biological changes.
This Site will focus on multidisciplinary research in aerospace engineering, chemistry, and applied space biology with a goal of improving future space materials science and human diagnostic technology by exposing students to the challenges in these areas and the research going on to solve them. Undergraduate students for a ten-week summer will be recruited for the program. The student recruitment will start in Nov 2021 and the first summer research will be held in the period of May 16 to July 18, 2022.
The ERAU-REU program is dedicated to the ideals of diversity, equity, accessibility, and inclusion and we ensure a safe and comfortable environment for all scholars. Please contact us if you have any questions or concerns about the housing accommodations or other aspects of the program.
Students from underrepresented groups in the sciences, veterans, disabled, or are early in their undergraduate coursework (rising sophomores or juniors) are especially encouraged to apply.
Research Areas:
1 - Additive Manufacturing of Shape-Stabilized Phase-Change Materials (PCMs)
Mentor: Prof. Sandra Boetcher (https://faculty.erau.edu/Sandra.Boetcher)
The goal of the proposed research is to manufacture shape-stabilized PCMs via additive manufacturing.
2 - Space Radiation: Study of Intracellular Reactive Oxygen Species
Mentor: Prof. Hugo Castillo (https://faculty.erau.edu/Hugo.Castillo)
The goal of this project is to produce a standardized technique to measure the intracellular concentration of ROS in different species of bacteria and yeast, in relation to chronic exposure to sub-lethal doses of ionizing radiation using a low-dose gamma irradiator allowing to quantify the oxidative stress status of the cell concerning DNA damage.
3 - Investigating Micro- and Nano-Plastics in the Confined Environment of Space Flight.
Mentor: Prof. Marwa El-Sayed (https://faculty.erau.edu/Marwa.ElSayed)
The proposed study aims to characterize atmospheric MNP in indoor environments. The goals of the study are 1) identification of the sizes, shapes and size distribution of MNP in the atmosphere, 2) characterization of the chemical composition of atmospheric MNP, 3) determination of the degradation processes and 4) identification of the health issues associated with these particles.
4 - Investigation of Space Biomechanics and Additive Manufacturing of the Orthopedics
Mentor: Prof. Victor Huayamave (https://faculty.erau.edu/Victor.Huayamave)
The participants will learn about (1) current state of space biomechanics research, (2) segmenting anatomical images to develop finite element models, and (3) 3D printed components using additive manufacturing. The computational pipeline will be introduced to the predictive power of the FEM to assess the structural integrity of the hip joint under microgravity conditions.
5 - Fabrication of a Flexible, Stretchable, and Self-Healable Platform for Aerospace Applications
Mentors: Prof. Foram Madiyar, Prof. Daewon Kim (https://faculty.erau.edu/Foram.Madiyar, https://faculty.erau.edu/DaeWon.Kim)
The goal of this project is to investigate the use of polymers not only having tunable electrical and thermal properties, but also reversible bond chemistry that imparts materials high stretchability, exceptional toughness, and self-healability.
6 - On-Site Biomarker Sensing using Flexible Transistors on Skin
Mentor: Prof. Foram Madiyar (https://faculty.erau.edu/Foram.Madiyar)
The goal of the project is to design a wearable technology for the real-time screening, diagnosis and multiplex detection of different biomarkers.
7 - Biofidelic Piezoresistive Nanocomposite Multiscale Analysis
Mentor: Prof. Sirish Namilae (https://faculty.erau.edu/Sirish.Namilae)
In the proposed research, we will further engineer the electro-mechanical response of the structure through (a) varying the constituents in the silicone matrix and (b) engineering the interface mechanical properties in the core layer.
8 – Fractography using Scanning Electron Microscopy
Prof. Alberto Mello (https://faculty.erau.edu/Alberto.Mello)
This research aims to cover scanning electron microscope (SEM) operation, including energy dispersive spectroscopy (EDS) and stress analysis. The student will cut and prepare fractured specimens, observe the crack surface under SEM to identify the local pit formation at the plate edge, find the point of crack initiation, and determine the propagation path.
9 - Investigation of Photoresponsive and Thermally Stable Monomeric Structures for Space Applications
Mentor Prof. Javier Santos (https://faculty.erau.edu/Javier.SantosPerez)
The goal of the project is to investigate the photoresponsive and thermally stable monomeric structures to sense damage, fractures, and changes to space infrastructures.
10 - Investigating Methods to Minimize the Gap between Pre and Post-Space Flight Syndrome
Mentor: Prof. Christine Walck (https://faculty.erau.edu/Christine.Walck)
We propose to design an optimized lower extremity force acquisition system (LEFAS) that integrates with a lower-body negative pressure (LBNP) box and subject-specific protocols for improved fitness results by taking a computationally simulated optimization approach.
Categories: Faculty-Staff
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JET-AIRFRAME INTERACTIONS FOR NOISE SUPPRESSION
PI Reda Mankbadi
JET-AIRFRAME INTERACTIONS FOR NOISE SUPPRESSION
The Embry‑Riddle team developed a passive noise suppression technology utilizing the interactions of the airframe with the jet plume. In this technology, the flat surface of the airframe adjacent to the jet plume is modified to create a slightly wavy surface instead. Such design modification can be applied to the existing design concepts with engine mounted under the wing, as well as, the top-mounted engine configurations.
The near-field perturbations are reflected by the wavy surface to create an excitation wave to amplify the jet and the shear layer instability. The wavy-surface parameters are designed such that the excitation frequency is the harmonic of the fundamental frequency responsible for the peak noise. Through nonlinear fundamental-subharmonic interaction, the sound source and its radiated far-field noise are reduced.
To verify this concept, high-fidelity simulations of a supersonic rectangular jet in the vicinity of the airframe surface were carried out. Results show that when the flat airframe surface is reduced by a wavy one, the radiated sound was reduced by 3.7dB for top-mounted engine, and by 2.6dB for under-airframe engine.
Implemntation of wavy surface design to suppress jet-surface interaction noise.
(Left) Top-mounted engine configuration, (Right) Conventional enginr-under airframe design
Acoustic spectra at the far-field observer 42 diameters away from the nozzle exit
(Left) Engine mounted on top of airframe, (Right) Engine mounted under the wing
Categories: Faculty-Staff
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Fundamental Experimental and Numerical Combustion Study of H2 Containing Fuels for Gas Turbines
PI Scott Martin
This project is a University Turbine Systems research grant funded by the Department of Energy. In collaboration with the University of Central Florida, Purdue University and the University of New Mexico, Embry‑Riddle will develop fundamental data and modeling of H2 and NH3 fuels for gas turbine power plants.
Categories: Faculty-Staff
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Human Factors Awareness Training for FAA Aviation Safety Specialists Within Aircraft Certification and FAA Flight Standards
PI Scott Martin
In this project, which is funded by the FAA, Embry‑Riddle and Kent University will develop training for individuals within the FAA’s Aviation Safety Flight Standards Service who have expertise and job responsibilities related to the evaluation of aircraft systems design, maintenance, operations, procedures and pilot performance.
Categories: Faculty-Staff
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Modeling Plume Afterburning Shutdown With a Double-Conditioned CMC
PI Scott Martin
This project will develop the double conditioned Conditional Moment Closure (CMC) turbulent combustion model for afterburning shutdown of hypersonic rocket exhaust plumes.
This is an Army Sequential Phase II STTR program in collaboration with Reaction Systems Inc., University of Central Florida and Propulsion Systems Inc. This project will develop the double conditioned Conditional Moment Closure (CMC) turbulent combustion model for afterburning shutdown of hypersonic rocket exhaust plumes.
Categories: Faculty-Staff
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The impact of corporate social responsibility communication on corporate reputation
PI Doreen McGunagle
CO-I Dixie Button
The goal of this research project is to analyze the ethics of social media used by U.S. airlines. In particular, how the four major carriers, Southwest Airlines, Delta, United, and American Airlines Group, stack up against each other in terms of privacy and the ethical use of information obtained via social media sites such as Facebook.
Corporate social responsibility (CSR) is increasingly more important for firms in today’s global marketplace and effective communication of CSR initiatives is vital toward enhancing a company’s reputation and its sales revenues. With this consideration, the reputations of firms in the Aerospace and Defense (A & D) industry worldwide, in conjunction with their use of social media were examined to validate a link between the use of social media to communicate CSR activities and a firm’s reputation ranking.
Methodology involved a qualitative content analysis of the online and social media presence of the top 20 A & D companies from the Deloitte Toche Tohmatso Limited (DTTL) 2014 Global A & D financial performance study. Data from six indicators of CSR: environment, community relations, diversity, employee relations, human rights, and client comments was examined.
According to the findings, firms utilizing social media for CSR communication should expect improved reputation ratings. All top 20 A & D companies publish at least four CSR indicators on social media platforms. The conclusion reached is that while CSR content via social media can lead to higher reputation ratings, companies need to strategically choose the ideal number of CSR indicators, to position themselves in the global marketplace.
Categories: Faculty-Staff Graduate
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Seaplane design analysis: Focus on structure factor optimization
PI Alberto Mello
CO-I Soham Bahulekar
CO-I Sergio Butkewitshch
CO-I Wesley Queiroz
In this work, a design optimization is being investigated considering possible hydrodynamic and structural advantages aiming to reduce the structure weight factor, with a trade-off between fluid dynamics and structural aspects.
Seaplanes are known to have mandatory design characteristics that lead to disadvantages in comparison to landplanes what limit their use as regular passenger commuters. The main design points to consider are that seaplanes have higher structure weight factor due to hull with its specific shape that creates higher drag than the fuselage of a landplane. They also have higher trim drag because of the need of placing the propellers far from the water surface. All these drawbacks reduce payload capability of seaplanes. In this work, a design optimization will be investigated considering possible hydrodynamic and structural advantages aiming to reduce the structure weight factor, with a trade-off between fluid dynamics and structural aspects, increasing payload capability. An optimized structure may lead to a more effective use of seaplanes as cargo or passenger commuters. A SEAMAX M-22 currently being assembled in the ERAU Research Park hangar will be used for result comparisons.
Categories: Graduate
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Behavior of superalloys subjected to fatigue loads under high temperature
PI Alberto Mello
CO-I Paulina De La Torre Morales
CO-I Open Position - New students are welcome
This study is evaluating what initial conditions can activate cubic slip planes, then the level of accommodation and strain homogenization within the grain, and how a given initial condition affects the material behavior when subjected to operational cyclic loads under high temperature.
Ni-based super alloys are widely used in turbine engines mainly due to its high strength and fatigue resistance at elevated temperatures. One hypothesis to explain its atypical characteristic among metals is that a cross-slip mechanism is in place. The activation of {100} cubic slip systems along of the octahedral slip planes {111} in Ni-based superalloys has been verified when under high strain and temperature. The material would exhibit a more homogeneous strain distribution and less strain localization. We seek for the ideal precondition that will improve the endurance of Ni-based superalloy (IN 718) samples subjected to operational loading. We evaluate the initial conditions that activate cubic slip planes, the level of accommodation, and strain homogenization within the grain. With focus on the deformation mechanism, the sample microstructure can be fully characterized by electron backscatter diffraction (EBSD) and the slip systems, after the applied pre-condition, can be tracked via digital image correlation (DIC).
Accomplished tasks:
(a) samples’ manufacturing, (b) sample polishing and preparation, (c) furnace installation and operational tests, (d) development of laboratory procedures, equipment and microscopes (optical and SEM), (d) calibration and controller fine tuning for the MTS tensile testing machine, and (e) fatigue test with several specimens, including control samples and modified pre-conditions
Next steps:
Characterization of the microstructure of tested specimens under special conditions via EBSD to identify the slip planes and confirm or not the activation of cubic slip systems.
Categories: Faculty-Staff
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Influence of cold expansion and aggressive environment on crack growth in aluminum alloy
PI Alberto Mello
CO-I Christopher Leirer
CO-I Ken Shishino
CO-I Open Position - New students are welcome
This research aims to establish the effect of hole cold expansion on fatigue life of pre-cracked material under aggressive environment.
This research investigates the relationship between crack propagation and secondary crack initiation in aluminum alloys with cold worked holes subjected to cyclic loads to determine the impact on fatigue life of joints in presence of aggressive environment. We work with experiments and analysis of fatigue life of bolted joints with coldworked holes in presence of galvanic corrosion. This investigation is examining the effect of local plastic deformation and localized galvanic corrosion on small cracks and fatigue life of bolted joints. The benefits of cold work are well known and its application is widely used in new and repaired structures, even in crack arrester holes. However, coldworked holes are usually fastened to dissimilar materials, what may induce localized galvanic corrosion. When applied in the field, damaged material removal in a cold work procedure may be limited to a maximum allowable diameter for reaming and finishing, what may leave micro/small cracks on the strained region. To completely understand the effect of initial cracks as a function of initial plastic deformation level in a coldworked hole it is necessary to fully evaluate strain distribution during and post cold work with microscopic detail. In a first approach, we have analyzed (FEM and classic analysis) and measured strain distribution during the process using digital image correlation (DIC). In the next step, we have tested specimens under fatigue. Pre cold work induced micro cracks was monitored in-situ via digital optical microscopy. In sequence, the coldworked holes were filled with a dissimilar material fastener in saline environment and the impact of galvanic corrosion on crack growth rate was determined for AA 2024-T3.
In a next step, we will further investigate the formation of critical secondary cracks. The probable cause could be a local corrosion around cathodic precipitates, but a detailed study is necessary to confirm this hypothesis. The tested samples must be prepared for use in scanning electron microscope (SEM) to identify the local pit formation at the plate edge, find the point of crack initiation, and determine the propagation path. Using striation counting technique, we may be able to estimate the number of cycles to failure and, consequently, the time necessary for the crack initiation under aggressive environment. Additionally, we will plan to use and analyze a special ceramic coating to mitigate galvanic corrosion effect on loaded components.
Categories: Graduate
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Damage Control Measures in Composites: Focus on Damage Tolerance of Aerospace Structures
PI Alberto Mello
CO-I Kais Jribi
CO-I Doug Neill (C.E.S. LLC)
CO-I Jon Gosse (C.E.S. LLC)
The focus of this research is to provide advanced methods and tools to address damage tolerance in composite structure
This study is in partnership with Computational Engineering Software, LLC (http://icmedesign.com).
Critical damage within metallic structure usually takes the form of cracks. The main issue is continued growth of the cracks as a function of in-service loading conditions. Often crack growth due to cyclic loading is of interest. Damage within composite structure has a higher number of factors to represent how critical the damage is. It must be considered that:
- Single cracks rarely exist in composite laminates, if they exist do it is usually as a delamination between adherents.
- Damage usually manifests itself as a network of inter-connected delaminations and transverse cracks.
- Unlike metals, Fracture mechanics is generally not applicable to laminated damage. The Mode I, Mode II and Mode III single crack failure modes require satisfaction of similitude to be realized in composite structures.
The main question to be answered is this study is when will the damage perimeters begin to grow under operational cyclic load. To do that, we expect to accomplish the following main steps:
Obtain limiting critical values for one or more material systems.
Develop a sequence of tests to simulate damage and then measure limits to catastrophic failure in compression and/or tension.
Model each of the test articles and apply the Onset approach to predict whether (for a given applied loading environment) the damage will or will not begin to propagate.
Compare prediction of the onset of propagation to measured ultimate failure. The criterion of success is that the numerical methodology can conservatively, but realistically predict a load level below which propagation does not occur.
Categories: Graduate
141-150 of 278 results