Preliminary Investigation of the Impact of Flight-Path Variability of Icing Conditions Upon the Critical Ice Shape Cranfield University

Format:

Conference/Event

Author/Creator:

Stanfield, Robin A., author.

Conference Name:

2007 SAE Aircraft and Engine Icing International Conference (2007-09-24 : Seville, Spain)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2007

Summary:

The Cranfield Icing Research Tunnel was used to carry out a preliminary study whose objective was to identify whether or not the introduction of flight-path variability could generate accretions notably different to the critical ice shape. A reference (critical) ice shape was generated under conditions obtained from Appendix C before variability was applied, firstly to LWC and secondly to temperature. The approach is presented and selected results are introduced in this paper. Results show that ice accretions produced under variable conditions can be notably different to the reference profile, and are potentially more detrimental aerodynamically

Notes:

Vendor supplied data

Publisher Number:

2007-01-3333

Access Restriction:

Restricted for use by site license