Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: part II. Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover

Author: Ozgumus Ozge Ozdemir   Kaya Metin O.  

Publisher: Emerald Group Publishing Ltd

ISSN: 0002-2667

Source: Aircraft Engineering, Vol.79, Iss.3, 2007-05, pp. : 231-237

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract