Physical Insights, Steady Aerodynamic Effects, and a Design Tool for Low-Pressure Turbine Flutter

The successful, efficient, and safe turbine design requires a thorough understanding of the underlying physical phenomena. This research investigates the physical understanding and parameters highly correlated to flutter, an aeroelastic instability prevalent among low pressure turbine (LPT) blades in both aircraft engines and power turbines. The modern way of determining whether a certain cascade of LPT blades is susceptible to flutter is through time-expensive computational fluid dynamics (CFD) codes. These codes converge to solution satisfying the Eulerian conservation equations subject to the boundary conditions of a nodal domain consisting fluid and solid wall particles. Most detailed CFD codes are accompanied by cryptic turbulence models, meticulous grid constructions, and elegant boundary condition enforcements all with one goal in mind: determine the sign (and therefore stability) of the aerodynamic damping. The main question being asked by the aeroelastician, ``is it positive or negative?'' This type of thought-process eventually gives rise to a black-box effect, leaving physical understanding behind. Therefore, the first part of this research aims to understand and reveal the physics behind LPT flutter in addition to several related topics including acoustic resonance effects. A percentage of this initial numerical investigation is completed using an influence coefficient approach to study the variation the work-per-cycle contributions of neighboring cascade blades to a reference airfoil. The second part of this research introduces new discoveries regarding the relationship between steady aerodynamic loading and negative aerodynamic damping. Using validated CFD codes as computational wind tunnels, a multitude of low-pressure turbine flutter parameters, such as reduced frequency, mode shape, and interblade phase angle, will be scrutinized across various airfoil geometries and steady operating conditions to reach new design guidelines regarding the influence of steady aerodynamic loading and LPT flutter. Many pressing topics influencing LPT flutter including shocks, their nonlinearity, and three-dimensionality are also addressed along the way. The work is concluded by introducing a useful preliminary design tool that can estimate within seconds the entire aerodynamic damping versus nodal diameter curve for a given three-dimensional cascade.

Design of Antibacterial Prochelators to Target Drug-Resistant Bacteria

Transition metals such as iron and copper are valued in biology for their redox activities because they are able to access various oxidation states. However, these transition metals are also implicated in a number of human disease states and play a role in bacterial infections. The ability to manipulate and monitor metal ions has vast implications on the fields of biology and human health. As such, the research described here covers two related goals: to manipulate metals in specific biological circumstances and to visualize this disturbance in cellular metal homeostasis.

Antibiotic resistance necessitates the development of drugs that exploit new mechanisms of action such as the disruption of metal homeostasis. In order to manipulate metals at the site of bacterial infection, two prochelators were developed around a β-lactam core such that the active chelator is released in the presence of bacteria that produce the resistance-causing β-lactamase enzyme. Both prochelators display enhanced activity toward resistant bacteria compared to clinical antibiotics.

Fluorescent sensors are a powerful tool for detecting small concentrations of biological analytes. Two analogs of a ratiometric fluorescent sensor were designed and synthesized to monitor cellular concentrations of copper and iron. These sensors were found to operate as designed in vitro; however the fluorescence intensity necessary for quantification of cellular metal pools has not yet been achieved.