Old Web
English
Sign In
Acemap
>
Paper
>
Experimental characterization of anti-icing system and accretion of re-emitted droplets on turbojet engine blades
Experimental characterization of anti-icing system and accretion of re-emitted droplets on turbojet engine blades
2018
Guillaume Linassier
Morgan Balland
Hugo Pervier
Marie Pervier
David Hammond
Emmanuel Radenac
Keywords:
Atmospheric sciences
Turbojet
Accretion (meteorology)
Drop (liquid)
Icing
Physics
turbojet engine
Environmental science
Mechanics
Correction
Source
Cite
Save
Machine Reading By IdeaReader
9
References
0
Citations
NaN
KQI
[]