Support new aircraft program development and in service aircraft in all thermodynamics related issues.
These include aircraft ice/fog protection systems performance, zonal pressure, temperature and flowrate analysis, avionics cooling, and general thermal analysis of systems and structures.
It requires understanding of the systems that are being analyzed and how they interface with the aircraft and other aircraft systems.
It also requires communicating with internal systems/structures groups, system suppliers, and flight test teams to resolve issues, plan tests, analyze and certify modifications.
More specifically, this position is to help the Global 7000 / 8000 thermodynamic team support the activities related to bleed air systems (wing ice protection system, environmental control system, ducting system, etc.).