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Aerodynamic Performance Evaluation of Subsonic Compressor Cascade Blade With Leading-Edge Damage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Material loss at the leading edge of in-service gas-turbine engine blades is detrimental to the aerodynamic performances of compressors. In this study, computational simulations and experiments using pneumatic probes were ...
Runup of Laboratory-Generated Breaking Solitary and Periodic Waves on a Uniform Slope
Publisher: American Society of Civil Engineers
Abstract: In this article, we demonstrate that the normalized runup heights, R/H (R = runup height; H = incident wave height), for breaking solitary and periodic waves can be characterized by a single dimensionless parameter, called ...