Andres Garzon Email & Phone Number

Seattle, Washington, United States

Reno, Nevada, United States

• Defined strategies for development and application of sustainable technologies• Worked with GE on emissions and emissions’ standards for supersonic aircraft• Led the initiative to define a new standard for 100% synthetic paraffinic kerosene• Led the execution of the carbon neutral strategy for the AS2 fleet via reforestation and carbon sequestration projects, and the ensuing carbon negative operation via sustainable fuels technologies• Led the initiative to plan and build a sustainable aviation fuels plant, exploring different feedstocks and processes for low carbon intensity fuels• Member of ICAO CAEP groups in support of the sustainable reintroduction of supersonic flight via ICCAIA and IBAC: WG1 - noise, WG3 – engine emissions, FTG – Fuels, MDG/FESG – Modeling of environmental impact

Reno, Nevada, United States

• Defined Boom Management System (BMS) for supersonic operations both overwater and overland. This system was responsible for ensuring that no boom reached the land, using Mach Cutoff for overland operations and route planning for unrestricted supersonic flight overwater• Down selected and signed high fidelity weather data supplier for systems development• Developed the CONOPS and preliminary architecture for the Boom Management System including the airborne BMS and the ground BMS• Defined level 0 requirements with avionics, software and human factors IPTs

Reno, Nevada Area

• Supported planning, schedule, risk management, and supplier coordination• Developed program metrics for the IPTs and Program Integration team• Supported preliminary implementation of EVMS• Authored AS2 program requirements documents including the AS2 Concept of Operations (CONOPS) and AS2 Market Requirements and Objectives

Reno, Nevada Area

• Coordinated engineering activities in the preliminary design of the AS2 supersonic business jet between Aerion and its industrial partners, Airbus initially and later Lockheed Martin• Developed Statement of Work and deliverables with industrial partners• Managed program schedule, risk items and work packages with industrial partners• Defined the range requirements for the AS2 SBJ using data analytics from worldwide GA operations• Actively led technical efforts in structural design, systems configuration, and flight sciences• Supported technical engagement with prospect engine suppliers in Europe and North America• Supported flight sciences activities, including continued development of propulsion integration and high-speed wind tunnel tests

Reno, Nv

• Built the core aero group at Aerion• Principal investigator for Aerion and NASA flight testing for supersonic natural laminar flow robustness using NASA’s F15. Developed a boundary layer transition robustness correlation from flight experiments results and prior art• Principal investigator for Aerion flight testing for transonic natural laminar flow on a Cessna CJ1. Test designed included CFD modeling and flight test correlations • Developed internal capability for sublimation technique in transition detection• Supported the ETW laminar flow test campaign for supersonic wing design• Performed post-test analysis and data processing of the Aerion NLF wing rocket sled test. Performed CFD test results analysis to estimate unsteady heat transfer from aerodynamic heating and radiation from rocket plume• Managed low speed wind tunnel tests and low speed high lift device research for the AS2 NLF wing including numerical analysis• Authored multiple engineering and test reports and conference papers

Reno, Nevada, United States

• Developed auxiliary air inlet concept for low-speed operation of the Aerion supersonic business jet• Designed high performance supersonic inlet and nozzle for the Aerion supersonic business jet• Completed multiple CFD analysis campaigns under the supervision of the Chief Engineer in support of various high speed and low speed test activities. CFD Configuration build up and stability predictions• Supported multiple wind tunnel test campaigns at the UWAL low speed wind tunnel

Ms, Fluid Dynamics Aerospace

Research on laminar-turbulent transition on boundary layers at hypersonic speed. Developed correlation for roughness Induced transition.

D.E.A., Fluid Mechanics, Applied Physics

B.S., Mechanical Engineering

Master Of Engineering - Meng, Engineering Physics/Applied Physics