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Correlation-Based Riblet Model for Turbomachinery Applications
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An empirical riblet model for manufactured V-shaped and trapezoidal riblets which is suitable for turbomachinery application is presented. The implementation of the riblet effect employs a correlation-based correction for ...
Modeling Vortex Generating Jet Induced Transition in Low Pressure Turbines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The current design of lowpressure turbines (LPTs) with steadyblowing vortex generating jets (VGJs) uses steady computational fluid dynamics (CFD). The present work aims to support this design approach by proposing a new ...
Correlation Between Pressure Recovery of Highly Loaded Annular Diffusers and Integral Stage Design Parameters1
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Exhaust diffusers significantly enhance the available power output and efficiency of gas and steam turbines by allowing lower turbine exit pressures. The residual dynamic pressure of the turbine outflow is converted into ...
Transition Modeling for Vortex Generating Jets on Low Pressure Turbine Profiles
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Steady blowing vortex generating jets (VGJ) on highlyloaded lowpressure turbine profiles have shown to be a promising way to decrease total pressure losses at low Reynoldsnumbers by reducing laminar separation. In the ...
A Theory on the Onset of Acoustic Resonance in a Multistage Compressor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A novel theoretical model of the internal flow field in multistage axial compressors based on an eigenvalue approach is developed, in order to predict the onset of acoustic resonance in aircraft engines. Using an example ...
Direct Numerical Simulation Based Analysis of RANS Predictions of a Low-Pressure Turbine Cascade
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The state-of-the-art design of turbomachinery components is based on Reynolds-averaged Navier–Stokes (RANS) solutions. RANS solvers model the effects of turbulence and boundary layer transition and therefore allow for a ...