Numerical Investigation of Pressure Tube Anti-Icing Heat Transfer

2023-01-1440

06/15/2023

Event
International Conference on Icing of Aircraft, Engines, and Structures
Authors Abstract
Content
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-ꞷ SST model predicted the surface temperature colder than the Transition SST model result.
Meta TagsDetails
DOI
https://doi.org/10.4271/2023-01-1440
Pages
6
Citation
Thangavel, S., and Bajpai, S., "Numerical Investigation of Pressure Tube Anti-Icing Heat Transfer," SAE Technical Paper 2023-01-1440, 2023, https://doi.org/10.4271/2023-01-1440.
Additional Details
Publisher
Published
Jun 15, 2023
Product Code
2023-01-1440
Content Type
Technical Paper
Language
English