DAMAGE ASSESSMENT OF HELICOPTER BLADE BASED ON CANTILEVER BEAM DISPLACEMENT MODEL
Keywords：Helicopter bladeDamage assessmentCantilever beamFinite element method (FEM)Residual nodal force
Publication Date：2009-01-01
Online Publishing Date：2026-09-12(First online date of this platform, not the publication date of the document)
Pages：5( 967-971 )