-
Hypersonic Boundary Layer Shock-Wave Interaction Aerothermal Lead #7!mK3q
Sandias Aerothermodynamics Group @8$pT4w
Predict boundary layer separation under Mach 6.5 shock interactions, model active transpirational cooling flow rates, and evaluate localized... -
Military Fast Jet Fly-By-Wire Actuator Servo Specialist ^8#zR2m
Fylde Aerospace Avionics #7$qP3k
Design high-bandwidth direct-drive electro-hydraulic actuator servo loops, evaluate gain-margin limits, and execute hardware-in-the-loop str...