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Dynamic analysis of an SDOF helicopter model featuring skid landing gear and an MR damper by considering the rotor lift factor and a Bingham number

Author(s):


Medium: journal article
Language(s): English
Published in: Smart Materials and Structures, , n. 6, v. 27
Page(s): 065013
DOI: 10.1088/1361-665x/aab860
Structurae cannot make the full text of this publication available at this time. The full text can be accessed through the publisher via the DOI: 10.1088/1361-665x/aab860.
  • About this
    data sheet
  • Reference-ID
    10214446
  • Published on:
    01/12/2018
  • Last updated on:
    01/12/2018
 
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