Title of article :
Optimization of supersonic nozzle flow for titanium dioxide thin-film coating by aerosol deposition
Author/Authors :
Lee، نويسنده , , M.W. and Park، نويسنده , , J.J. and Kim، نويسنده , , D.Y. and Yoon، نويسنده , , S.S. and Kim، نويسنده , , Hy-Sook Kim، نويسنده , , D.H. and James، نويسنده , , S.C. and Chandra، نويسنده , , S. and Coyle، نويسنده , , Thomas and Ryu، نويسنده , , J.H. and Yoon، نويسنده , , W.H. and Park، نويسنده , , D.S.، نويسنده ,
Issue Information :
ماهنامه با شماره پیاپی سال 2011
Pages :
10
From page :
771
To page :
780
Abstract :
Aerosol deposition (AD) is an efficient technique for customized coating of various substrates. The small particles of AD yield a dense coating layer with small voids. AD is amenable to rapid coating (mass production), thus, it is economically attractive. Low-temperature AD coating is desirable because it minimizes the thermal degradation of the substrate. An optimized low-cost AD coating technique is of significant interest to solar-cell engineers seeking to reduce manufacturing costs. While most previous studies ignore the importance of nozzle geometry on coating performance, this paper examines non-optimized nozzles and commensurate shockwaves using computational fluid dynamics (CFD). The optimized nozzle geometry obtained from CFD can rapidly prototype nozzles. The CFD-designed nozzles with optimized geometry yielded significantly improved coating quality over non-optimized nozzles.
Keywords :
Aerosol deposition , Supersonic nozzle flow , SHOCKWAVE , Nozzle optimization , Computational fluid dynamics
Journal title :
Journal of Aerosol Science
Serial Year :
2011
Journal title :
Journal of Aerosol Science
Record number :
1385991
Link To Document :
بازگشت