Quasi 3D Nacelle Design to Simulate Crosswind Flows: Merits and Challenges

Quasi 3D Nacelle Design to Simulate Crosswind Flows: Merits and Challenges

This paper studies the computational modelling of the flow separation over the engine nacelle lips under the off-design condition of significant crosswind. A numerical framework is set up to reproduce the general flow characteristics under crosswinds with increasing engine mass flow rate, which incl...

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Bibliographic Details
Main Authors: Alex Yeung, Nagabhushana Rao Vadlamani, Tom Hynes, Sumit Sarvankar
Format: Article
Language:English
Published: MDPI AG 2019-08-01
Series:International Journal of Turbomachinery, Propulsion and Power
Subjects:
crosswind
nacelle
distortion
shock
boundary layer
quasi 3D design
Online Access:https://www.mdpi.com/2504-186X/4/3/25

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