This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Numerical Optimisation of a Helicopter Engine Inlet Electrothermal Ice Protection System
Journal Article
2019-01-2042
ISSN: 2641-9645, e-ISSN: 2641-9645
Sector:
Citation:
Moser, R. and Roberts, I., "Numerical Optimisation of a Helicopter Engine Inlet Electrothermal Ice Protection System," SAE Int. J. Adv. & Curr. Prac. in Mobility 2(1):265-271, 2020, https://doi.org/10.4271/2019-01-2042.
Language:
English
References
- www.openfoam.com
- https://hiliftpw.larc.nasa.gov/
- Bidwell , C.S. , Mohler , S.R. Jr. 1995
- https://cordis.europa.eu/docs/results/308/308183/final1-dev9101-sandit-final-report-publishable-summary-form.pdf
- Lammers , K. , van’t Hoff , S , Ferschitz , H. , and Wannemacher , M. 2018
Cited By
Recommended Content
Technical Paper | An Ice Shedding Model for Rotating Components |
Technical Paper | Multi-Shot Icing Simulations with Automatic Re-Meshing |
Technical Paper | CFD Analysis of Supercooled Large Droplets in Turbofan Engines |