helicopter single hydraullic actuator capability
For example in typical helicopter Nz-V envelop for 3T weightclass if dual hydraulic system is designed for 2.5g aerodynamic loads at 240kmph, what could be the single actuator capability (is it 50% or 75% of dualactuator capability) at design stage. The design for aerodynamic loads shouldbe upto 2.5g for dual system what should be the ‘g’ level aerodynamic loads for a single system.
Is there any references / literature available that helps toknow “in a dual hydraulic system, if one hydraulic system fails what should bethe ‘g’ which could sustain and safely land of a helicopter”.
awaiting answers please
regards
TEJAS