Numerical investigations of the separated transitional flow over compressor blades with different loading distributions
Sign Up to like & getrecommendations! Published in 2020 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2020.106113
Abstract: Abstract Large eddy simulations (LESs) were conducted to investigate the separated flow transition process over two compressor blades with different loading distributions at Reynolds numbers (Re) of 1.5×105 and 0.8×105. The baseline airfoil (V103-B) was… read more here.
Keywords: blades different; flow; compressor blades; loading distributions ... See more keywords