Assessment of an engine design for icing risk is important at both the design stage and for development and certification testing. Icing must be included with aerodynamic and noise constraints during the design phase to minimize the risk of design change during development, and the compromise tested must be tested at the extremes of the atmospheric icing, and aircraft and engine operating envelopes most appropriate to the particular components. The type of assessment necessary is addressed and illustrated mainly by reference to high bypass ratio turbofans. The approach to identifying critical conditions is presented and areas where research can provide basic data for the development of design methods are discussed.
Engine Icing Criticality Assessment
1990
6 pages
Report
No indication
English
Online Contents | 2017
|Engine Icing Performance Simulation
NTRS | 2011
|Engine Icing Technical Challenges
NTRS | 2011
|Engine Icing Accretion Simulation
NTRS | 2011
|TURBOFAN ENGINE DE-ICING COMPRESSOR AND DE-ICING PROCESS
European Patent Office | 2018
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