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RISShear Layer Development, Separation, and Stability Over a Low-Reynolds Number Airfoil
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The shear layer development for a NACA 0025 airfoil at a low Reynolds number was investigated experimentally and numerically using large eddy simulation (LES). Two angles of attack (AOAs) were considered: 5 deg and 12 deg. ...
Verification and Validation of High-Fidelity Open-Source Simulation Tools for Supersonic Aircraft Aerodynamic Analysis
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Small supersonic vehicle concepts used as research platforms to test new aerospace technologies, such as advanced propulsion systems or large sensor payloads, require major modifications to conventional, large-scale, manned, ...