- Develop CFD-based computational aerodynamic database for Spaceship Delta using Pointwise and FUN3D. Develop and scope corresponding transonic wind tunnel test to collect experimental data and mature aero model in conjunction with CFD data.- Create Monte Carlo simulations using Matlab to generate and analyze spacecraft trajectories throughout boost and re-entry phases of flight, with speeds ranging from subsonic to supersonic. Analyze trajectory data against mission requirements to mature flight envelope for Spaceship Delta.- Conduct wide variety of aero performance trade studies. Subject matter includes fastener excrescence drag analysis, weight reduction analysis, and flight path angle analysis. Document study results and present recommendations to chief engineers and program management.- Evaluate internal R & D proposals, allocate departmental budget, and track performance for approximately 50 employees as Process Improvement Focal for the Flight Sciences Directorate.

- Supported the Space Launch System and Transonic Truss-Braced Wing programs as an experimental aerodynamicist in NASA Langley's Configuration Aerodynamics Branch.- Conducted subsonic, transonic, and supersonic wind tunnel tests for aircraft, rotorcraft, and launch vehicles. Designed wind tunnel test articles, worked with model vendors, and developed test matrices leading up to tunnel entry.- Analyzed wind tunnel test data using Matlab and Python, generated aerodynamic databases, quantified uncertainties, and reported results to relevant parties. Experienced at performing buffet analysis, pressure-sensitive paint analysis, surface pressure port analysis, and traditional force and moment testing.- Performed ground effect, icing, and repeatability analysis for a variety of different aircraft configurations- Author and co-author on AIAA publications documenting wind tunnel test analysis. Selected papers include "Experimental Identification of Bistable Flow State on the Space Launch System at Liftoff Conditions" and "Cross-Validation of Computational and Experimental Distributed Surface Pressures on the Space Launch System".

- Aerodynamics group member within Boeing Flight Sciences with a primary focus in exhaust system aerodynamic design and analysis. Provided aerodynamic analysis and support for a wide variety of commercial and military programs.- Designed and iterated through different nozzle designs using surface-based modeling in CATIA to optimize engine performance of future Boeing aircraft.- Prepared geometry, generated meshes, and performed CFD analysis on exhaust systems using ICEM and CFD++. Post-processed engine performance results and generated plots and figures using Tecplot, Matlab, and Python.- Performed CFD analysis on auxiliary power unit designs to predict performance qualities under icing conditions- Supported flight/ground test operations by travelling to witness and document a variety of different engine tests including nacelle leakage and area measurement testing to support certification and development efforts- Collaborated regularly with major engine companies to satisfy nozzle design requirements and meet performance goals; prepare CFD figures and data for presentation during conference calls and meetings.

- Worked directly with clients by providing low speed wind tunnel test support for a wide variety of aerodynamic models including airplanes, UAVs, cars, engines, and spacecraft- Collaborated with aircraft, car, and space companies to assist with test planning and execution as an expert with data reduction and test design. Supported over 100 different wind tunnel tests- Used in-house software programs combined with several other programming languages including Matlab, Visual Basic, and Python in the acquisition and reduction of subsonic wind tunnel test data- Installed and calibrated instrumentation for wind tunnel data acquisition including electronic pressure modules, strain gauges, and load cells. Wrote and edited LabView VIs to ensure accurate data acquisition- Troubleshooted a wide variety of different issues that could arise during testing. Implemented innovative solutions or workarounds safely and efficiently to keep the test on scheduleWorked 15-20 hrs/week throughout the school year, and 40-50 hrs/week in the summer.

-Team finished 1st Place Overall at 2019 Spaceport America Cup-Developed and tested plasma actuator system in the nosecone of the SARP rocket as part of the Payload team; goal of system to reduce overall drag on rocket by preventing flow separation during ascent-Modeled nosecone and rocket drag coefficient and pressure distribution using CFD solvers (Fluent, STAR-CCM+)-Supported low speed wind tunnel test of scale model of rocket; correlated wind tunnel results to CFD data to help refine the eventually placement of the plasma actuator system-Designed, assembled, and validated Arduino-based hardware/software interface with heat flux sensors and temperature sensors to measure and log flow quality data during ascent

- Responsible for coordinating meetings, preparing reports in Microsoft PowerPoint and Word, and managing a team of students throughout the research, design, and construction phase of the ignition systems for the SARP rocket.- Use SolidWorks to model a variety of diferent systems and subsystems for the SARP rocket.Parts modeled include fuel grain spinners, pre-burners, and different igniter geometries and designs.- Collect and analyze data by formulating test plans and testing different iterations of igniters in order to optimize the design- Rocket ignited successfully as a member of the ignition team as the SARP rocket received 2nd place at the 2017 Spaceport America Cup, and 1st place at the 2018 Spaceport America Cup

- Spring 2019 internship; assisted in development and commercialization of GearSim, a landing gear and ground loads simulation and analysis software developed in Matlab/Simulink- Researched and improved GearSim aircraft carrier landing modeling and simulation capabilities. Presented findings as co-author of technical paper titled "Carrier Landing Simulation using Detailed Aircraft and Landing Gear Modeling" (AIAA 2020-1138) at the 2020 AIAA Scitech convention.- Debugged software, suggested and implemented GUI and code improvements to improve user experience and software stability- Performed literature review of aerodynamics, ground loads, and arrested carrier landing research papers to develop and enhance various features within in the software- Wrote and developed user guides and training presentations to teach users and potential clients of many different skill levels how to use the software

-Summer 2018 Internship; worked with Matlab, Excel, XFLR5, XFOIL, and other proprietary flight performance analysis tools to compare transonic and subsonic aerodynamic data from both CFD and wind tunnel testing for the MQ-25 and Gremlins programs-Analyzed aircraft performance anomalies and provided conclusions and recommendations to the company on how to resolve the discrepancies -Authored subsonic wind tunnel test report for the Gremlins program-Communicated findings from projects and studies through a series of manager-reviewed internal memos and reports. Presented these findings to team member and company executives at the conclusion of the internship

- Assisted customers in person, over the phone, and various schools in Washington for on-site assembly of product- Oversaw set-up/takedown of various displays in the store, assisted in stockroom- Performed cashier duties and managed various customer requests/complaints- Frequently stayed past normal work hours in order to ensure that all customers were accounted for and all closing procedures were followed correctly- Set store record for number of customers signed up for text alerts in a single day, showing aptitude in sales and customer interaction