2015
DOI: 10.1007/s13272-015-0173-0
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Structural modeling and validation of an active twist model rotor blade

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Cited by 3 publications
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“…Therein, the dynamic stress intensity of the blade is mainly affected by blade vibration characteristics and unsteady airflow exciting force [11,12]. Hoffmann et al [13] applied the finite element method to compute self-vibration frequencies and vibration modes of blades, wherein computation programs included DLR's rotor simulation code S4 and ANSYS. Then, experimental methods were used to measure self-vibration frequency of the blade at different orders under nonrotation and rotation states, wherein the effectiveness of numerical modeling was verified.…”
Section: Introductionmentioning
confidence: 99%
“…Therein, the dynamic stress intensity of the blade is mainly affected by blade vibration characteristics and unsteady airflow exciting force [11,12]. Hoffmann et al [13] applied the finite element method to compute self-vibration frequencies and vibration modes of blades, wherein computation programs included DLR's rotor simulation code S4 and ANSYS. Then, experimental methods were used to measure self-vibration frequency of the blade at different orders under nonrotation and rotation states, wherein the effectiveness of numerical modeling was verified.…”
Section: Introductionmentioning
confidence: 99%