Investigations relating to factors influencing the effectiveness of an aero-engine intake thermal anti-icing system

Thermal anti-icing systems are commonly used to protect aircraft leading edges from a potentially hazardous build-up of ice. Such systems have proven reliable in service and are relatively cheap and efficient. Typically, hot air is tapped from the engine compressor and ducted (via a regulation and c...

Full description

Saved in:
Bibliographic Details
Main Author: S.J. Riley
Format: Default Thesis
Published: 1991
Subjects:
Online Access:https://hdl.handle.net/2134/7201
Tags: Add Tag
No Tags, Be the first to tag this record!