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Control of Flow Past an Airfoil Section Using Rotating Cylinders
The flow past a NACA 0024 airfoil with a leading edge rotating cylinder is simulated numerically using the ANSYS CFX software. To delay the boundary layer separation from the airfoil surface, different configurations for ...
Prediction of Turbulence Statistics in a Model Dump Combustor Using Artificial Neural Networks
The flowfield characteristics downstream of an axisymmetric suddenexpansion dump combustor model are important to designers of gas turbines and liquid-fuel ramjets ducted rockets. Many experimental techniques such as Laser ...