Leading multi-disciplinary team in exploring the unique physics of the Transonic Truss Braced Wing (TTBW) configuration to assess best market fits in commercial and military applications. Plan and mentor research teams in multidisciplinary assessment of technologies on a variety of future concept vehicles for vehicle feasibility, manufacturer and airline economics, and environmental sustainability,Coordinate research and technology assessments of Advanced Concepts to inform Product and Strategy decision makers.

Responsible for synthesizing conceptual commercial airplanes which are safe, technically-feasible, profitably-manufactured, and economically superior from program and customer requirements• Designed possible competitor airplane products and communicated the strategic impacts to influence applicable product and technology plans in the $2+ billion-dollar R&D portfolio • Benchmarked existing airplane passenger cabins to define key performance metrics and requirements for future Boeing cabin architectures • Led multi-disciplinary team of 20+ individuals among 6+ different functional groups across three sites to complete trade study plan for future airplane development program• Trained other engineers in new airplane CAD modelling tools to define full-digital airplane master geometry which improved data quality by 5% and condensed airplane layout time by 10%

Responsible for planning and leading component-level studies to inform aircraft vehicle designs which meet customer and program requirements • Presented design recommendations of 25+ trade studies to program management after coordinating among structures, payloads, aerodynamics, mechanical systems, and manufacturing engineering teams• Lead conceptual development of an airplane fuselage design which was 10% lighter weight, 5% lower cost, 20% faster build-time with identified technology and architecture risks• Proposed cost-reduction design changes to 787 chief engineer ranging from $5,000 to $250,000 per unit which improved program profitability, build quality, and assembly time• Facilitated accelerated collaborative design studies using Agile methodologies to deliver more complete design recommendations in 50% less flow time• Reviewed technology projects for design incorporation by quantifying uncertainty in design metric benefits with appropriate risk profile with subject matter expert inputs

Participant in reviewing and advising on improvement the Mechanical Engineering curriculum and internship experiences for the upcoming future engineers from the program.

Selected into early-career rotation program of three 6-month engineering assignments in Boeing Flight Sciences• Weight Engineer: recommended structural design changes for the 777X vertical fin, resulting in 2% weight reduction and raised unknown weight risks • Loads engineer: estimated static and dynamic loads for airplane design changes to enable 1.5% fuel burn improvement of 777-300ER / 777-200LR • Aerodynamic engineer: assessed high speed and low speed airplane performance impacts for proposed design changes to the 777X airplane family

Responsible to support multi-disciplinary analysis, participate in trade studies, and document airplane vehicle designs • Performed a multi-point optimized design space visualization enabling lead engineers to determine a recommended airplane vehicle design change, reducing their study time by 3 months • Developed training for MDAO vehicle sizing software and airplane CAD model software, improving the proficiency of airplane design engineers

Developing parametric modeling tools to perform aircraft design tradeoff studies including: aircraft geometry, aerodynamic loads, structural arrangement, structural analysis,and manufacturing.

Supported engineers in fatigue crack analysis for the mature T-38 Talon aircraftMaintained documentation of critical structural components for fatigue crack analysisAssisted in aircraft performance analysis studies on the T-38 aircraft using CFD software and other tools Programmed a six degree of freedom code to determine aerodynamic coefficients from wind tunnel data for a flight simulator