학회 연락처
- +82-2-563-0935
- +82-2-558-2230
- submission@kssse.or.kr
- https://www.kssse.or.kr/
KISE Journal of Korean Institute of Surface Engineering 2015;48(6):260-268. Published online: Nov, 30, -0001
DOI : 10.5695/JKISE.2015.48.6.260
The thermal barrier coating (TBC) for inner wall of liquid-fuel rocket combustor consists of NiCrAlY as bonding layer and
키워드 Inner Wall of Liquid-fuel Rocket Combustor;Thermal Barrier Coating;Electrodeposition;Ni-P/Cr;Annealing;Band Layer;