Development and Validation of a New Boundary Condition for Intake Analysis with Distortion

The design of an intake for a gas turbine engine involves CFD-based investigation and experimental assessment in an intake test rig. In both cases, the engine is represented by a mass flux sink, usually positioned a few fan radii aft of the real fan face. In general, this approach is sufficient to a...

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Bibliographic Details
Main Authors: Foad Mehdi Zadeh, Jean-Yves Trépanier, Eddy Petro
Format: Article
Language:English
Published: Wiley 2013-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2013/284206
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