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- W1627308776 abstract "This paper reports current stage of the research whose aim is to apply computer aided testing and modelling technique in order to aid the helicopters structural dynamics properties investigation methodology. The considered approach might be useful for application to helicopters design formulation, prototyping and modification, technical state monitoring and prediction, and assembly quality control. The state of the art of the helicopters structural dynamics investigations is surveyed and some results application directions are discussed. The main results and general conclusions of the standard ground modal testing of the PZL Sokol helicopter is presented. The preliminary results of the displacement and strain modal testing of a prototype helicopter separate tail boom is described. This testing was performed with aim of investigation of the standard modal analysis approach enhancing with strain modal testing and selection of the response only measurement data identification method. Some technical problems encountered during experimental work are addressed. The results of application of the theoretical structural dynamics behaviour modelling with use of the FE technique as a supplement to the experimental techniques are considered. Finally the in-flight modal testing procedure which is about to start is characterised." @default.
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- W1627308776 date "1998-02-01" @default.
- W1627308776 modified "2023-09-26" @default.
- W1627308776 title "Strain Modal Testing of a Helicopter Tail Boom" @default.
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