Abstract Safety factors of the Ansat helicopter main rotor blade are determined in the root section at various flight modes with taking into account the possible damages.
Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
Russian Aeronautics (Iz VUZ) ; 59 , 3 ; 308-315
2016-07-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch