Numerical Investigation of Pressure Tube Anti-Icing Heat Transfer Collins Aerospace

Format:

Book

Conference/Event

Author/Creator:

Thangavel, Sathish, author.

Contributor:

Bajpai, Shivanshu

Conference Name:

International Conference on Icing of Aircraft, Engines, and Structures (2023-06-20 : Vienna, Austria)

Language:

English

Physical Description:

1 online resource cm

Place of Publication:

Warrendale, PA SAE International 2023

Summary:

This work presents the anti-icing simulation results from a pressure sensing probe. This study used various turbulence models to understand their influence in surface temperature prediction. A fully turbulence model and a transition turbulence model are considered in this work. Both dry air and icing conditions are considered for this study. The results show that at low Angle of Attack (AOA) both turbulence model results compared well and at higher AOA the results deviated. Overall, as AOA increases, the k- SST model predicted the surface temperature colder than the Transition SST model result

Notes:

Vendor supplied data

Publisher Number:

2023-01-1440

Access Restriction:

Restricted for use by site license