Fluid flow studies of the F-5E and F-16 inlet ducts

The intake represents the front of a complex aerodynamic system. The shape of the intake diffuser follows the contours of the aircraft for external aerodynamic reasons. However the meandering shape can result in unwanted secondary flow or swirl build up at the Aerodynamic Interface Plane (AIP), resu...

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Bibliographic Details
Main Author: Imran Halimi Ibrahim
Other Authors: Ng Yin Kwee
Format: Theses and Dissertations
Language:English
Published: 2009
Subjects:
Online Access:https://hdl.handle.net/10356/14581
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Institution: Nanyang Technological University
Language: English

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