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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.05.069
Abstract: Abstract Trailing edge mixing flows associated with coolant injection are complex, in particular at transonic flows, and result in significant aerodynamics losses. A series of tests and calculations on a high-pressure turbine vane cascade with…
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Keywords:
trailing edge;
mach;
edge injection;
injection ... See more keywords