PARAMETER ANALYSIS ON CIRCULATION CONTROLLED CIRCULAR CYLINDER FOR NOTARTM TAIL BOOM

摘要

Lift on circulation control(CC)circular cylinder is calculated via numerical simulations based on 2Drealizable k-εepsilon viscous model and compared with experimental data.The simulation result shows an acceptable agreement with tested data.With the proved grid and simulation method,series of simulations are conducted to study the effect of parameters on lift.Single slotted tail booms under different down wash velocities are optimized with the principle of generating maximum total moment around the main rotor shaft with same total power consumption.The results show that larger jet flow velocity,or smaller blow angle,or larger diameter of the cross section can help generating larger lift while enhancing the attachment of both the jet flow and down wash flow.Multiple slotted tail boom is better because it increases lift with same total slot width,and can increase lift by increasing total slot width without causing separation,also it helps generating high steady lift at a big rank of slot attack angles.To mount a guide vane(GV)at the exit of the slot,or shape the upper slot wall like a smooth-GV,or design the slot with an edge fillet is not recommended because it reduces the velocity of both the jet flow and the upstream of the attached downwash flow.Compared with other shapes of the slots,arcs-profiled slot performs better because of larger jet flow velocity and smaller blow angle.In order to generate the largest moment with same total power consumed by the entire NOTARTMsystem,total width of the slots and slot attack angle should be optimized according to velocity of down wash flow.