Investigation of Engine–Airframe Vibration Due to Main Rotor Hub Loads Using a Substructuring Framework
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DOI: 10.4050/jahs.64.042001
Abstract: This paper presents a methodology to analyze the coupled structural dynamic response of an elastic airframe and engines of a helicopter in response to main rotor hub loads. Transfer functions of individual components (airframe, engine,… read more here.
Keywords: response; mount; airframe; using substructuring ... See more keywords