IMPROVEMENT OF AIRFOIL TRAILING EDGE BLUNTNESS NOISE MODEL

Improvement of airfoil trailing edge bluntness noise model

In this article, airfoil trailing edge bluntness noise is investigated using both computational aero-acoustic and semi-empirical approach.For engineering purposes, one of the most commonly used prediction tools for trailing edge noise are based on semi-empirical approaches, for example, the Brooks, Pope, and Marcolini airfoil noise prediction model

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Validation and verification of the OPI 2.0 System

Richard Abelson1,2, Keith J Lane3, John Rodriguez3, Patrick Johnston3, makita rf1101 Endri Angjeli3, George Ousler3, Douglas Montgomery11School of Computing, Informatics, and Decision Systems Engineering, Arizona State University, Tempe, AZ, 2Statistics and Data Corporation, Tempe, AZ, 3Ora, Inc, Andover, MA, USAPurpose: The Ocular Protection Index

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