Aerospace Sciences
The aerospace sciences area emphasizes both the theoretical and experimental aspects of aeroacoustics, aero-optics, aerospace systems design, high-lift aerodynamics, low Reynolds-number aerodynamics, low-speed aerodynamics, particle dynamics, flow control, transonic, supersonic and hypersonic flows, and vortex aerodynamics.
Ongoing research projects include:
Accelerated Perturbation Techniques
Acoustics of Fans with Asymmetric Duct Geometry
Active Control of Tip Clearance Flows in Rotating Machinery
Active Separation Control in a Turbo-jet Low Pressure Turbine
Aeroacoustic Phased Array System
Aerodynamics and Aeroacoustics of Nonuniform Flows
Aerodynamics of Micro-Air Vehicles
Airfoil Aerodynamics at Low Reynolds Numbers
Algorithms for Large Number of Equations
Development of a Microfabricated Sonic Anemometer
Direct and Inverse Problems in Hydrodynamics and Hydroacoustics
Direct Computation of Aerodynamically Generated Sound
Experimental Investigation of the Flow Field Physics of High-Lift Systems
Experimental Investigation of Unsteady Aerodynamics and the Sources of Propeller Noise
Flow Bifurcation and Nonlinear Flight Dynamics
Low-Order Dynamical Systems Modeling of Turbulent Shear Flows
Noise Source Modeling and Control of Compressible Turbulent Jets
Turbulence and Acoustics in Propeller Flows
Turbulence and Acoustics in Trailing Edge Flows
Turbulence in the Near Surface Region of the Atmospheric Boundary Layer
Turbulent Structure Modification by Streamlined Devices
Uncertainty: Methodology and Applications
Direct
comments, questions, and corrections to amedept@nd.edu