Numerical Simulation of Vector Aerodynamic Three with Three Swing Arm Spoiler
In order to adapt to the development trend that the nozzle of intelligent controllable ammunition engine is getting smaller and smaller,the aerodynamic numerical simulation was carried out for the vector control form of three swing arm spoiler.The results show that the thrust decreases with the increase of the main thrust angle.The maximum thrust loss is only related to the main thrust an-gle.When the main thrust angle is greater than 36°,the aerodynamic interference between the spoilers increases.The lateral force in-creases with the increase of lateral angle and inlet pressure.As the three spoilers are all located in the engine wake,the interference of the lateral force adjustment in the front rear direction and the left and right direction is small,and the influence of the lateral force ad-justment on the thrust is small.
solid rocket motorspoilernumerical simulationthrust vector control
万方数据
维普
