@Article{hmt.13.9,
AUTHOR = {Nian Wang, Mingjie Zhang, Sulaiman Alsaleem, Lesley M. Wright, Je-Chin Han},
TITLE = {TURBINE BLADE LEADING EDGE IMPINGEMENT COOLING FROM  NORMAL OR TANGENTIAL JETS WITH CROSSFLOW EFFECT},
JOURNAL = {Frontiers in Heat and Mass Transfer},
VOLUME = {13},
YEAR = {2019},
NUMBER = {1},
PAGES = {1--13},
URL = {http://www.techscience.com/fhmt/v13n1/53143},
ISSN = {2151-8629},
ABSTRACT = {This study investigates turbine blade, leading edge cooling from normal or tangential impinging jets. These jets impinging on a semi-cylindrical,
inner surface are constrained to discharge in a single direction. The downstream jets are affected by the crossflow originating from the upstream jets. 
To understand the thermal flow physics, numerical simulations are performed using the realizable k- turbulence model. Both the experimental and 
numerical results show crossflow is more detrimental to normal impinging jets than the tangential jets. Furthermore, with a significant temperature 
drop across the jet plate, designers must correctly interpret jet impingement results.},
DOI = {10.5098/hmt.13.9}
}