The average effective pitch damping increases with increasing Angleofoscillation amplitude and decreases with increasing Mach number.
角振幅增大会使返回舱的平均俯仰阻尼增加,马赫数增大使俯仰阻尼降低。
2
While impulse forces not acting on the centroid, the influence of accessional attack Angleoscillation amplitude, impulse force scale and function time interval on range correction was discussed.
In order to study dynamic stall phenomena of an aircraft in portrait at a high Angleof attack, designing a measuring device of heave oscillation for a low speed wind tunnel.