Design of mistuning patterns to control the vibration amplitude of unstable rotor blades
Sign Up to like & getrecommendations! Published in 2018 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2018.06.034
Abstract: Abstract Flutter onset is one of the major causes for increased vibration levels in low pressure turbine (LPT) rotor blades. This paper describes the design process and the experimental testing of intentional mistuning patterns specifically… read more here.
Keywords: vibration; mistuning patterns; intentional mistuning; rotor blades ... See more keywords