Student : Nate Falkiewicz
Sponsor : Michigan/AFRL Collaborative Center in Control Sciences
Hypersonic vehicle design and simulation require an interdisciplinary approach due to complex physics and coupling between aerodynamics, aerodynamic heating, heat transfer, elastic airframe, flight control, and propulsion. The focus of this project is the investigation of the effect of aerodynamic heating on the vehicles structural dynamics and aero-elastic response. Due to the low-order form required for control system design, reduced-order models are utilized within the aero-thermoelastic framework. The major contributions to date are:
Investigated the use of proper orthogonal decomposition for reduced-order thermal solution with arbitrary time-dependent boundary conditions
Developed aerothermoelastic simulation framework with reduced-order aerothermal, heat transfer, and structural dynamic models
Applied framework to hypersonic vehicle control surface and assessed impact of aero-thermo-elasticity on transient lift, drag, and necessary control input
Control surface displacements at Mach 8, 3° angle of attack from 0 – 200 s under unsteady aerodynamic and thermal loads.