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Detection of Laminar Flow Separation and Transition on a NACA 0012 Airfoil Using Surface Hot Films
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A method for mapping the separation and transition of flow over a slowly pitching airfoil with high angular resolution is presented. An array of surfacemounted hotfilm sensors is used to record simultaneous corresponding ...
Effect of Orifice Geometry on the Development of Slightly Heated Turbulent Jets
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Passive scalar (temperature) mixing with different orifice geometries is considered at low Reynolds number. The kinetic energy dissipation rate shows that the three jets achieve a selfsimilar state quickly compared to a ...
Localization of Flow Separation and Transition Over a Pitching NACA0012 Airfoil at Transitional Reynolds Numbers Using Hot Films
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Separation and transition of flow over a pitching airfoil at transitional Reynolds Number are analyzed experimentally. The method is based on a windowed correlation between hotfilm sensor signals taken simultaneously or ...
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