航空工程进展
航空工程進展
항공공정진전
ADVANCES IN AERONAUTICAL SCIENCE AND ENGINEERING
2011年
3期
260-266
,共7页
秦浩%李华星%孟宣市%罗时钧%刘锋
秦浩%李華星%孟宣市%囉時鈞%劉鋒
진호%리화성%맹선시%라시균%류봉
圆锥体%等离子体诱导流场%主动流动控制%脉冲循环%粒子图像激光测速仪
圓錐體%等離子體誘導流場%主動流動控製%脈遲循環%粒子圖像激光測速儀
원추체%등리자체유도류장%주동류동공제%맥충순배%입자도상격광측속의
conical cone%flow field induced by plasma%active flow control%periodic-pulsed%particle image velocimetry
对等离子体诱导流场特性进行研究,有利于解决双稳态非对称分离涡带来的连续比例控制困难的问题。在封闭光学玻璃箱体内,应用介质阻挡放电等离子体对20°顶角圆锥附近静止大气进行了定常和脉冲循环控制,对等离子体诱导的圆锥截面绕流速度场进行了二维PIV测量,对定常控制和脉冲循环控制下最大绕流速度及最大轴向涡量进行了比较分析。实验结果表明:相对于定常控制模式,脉冲循环控制下沿垂直于圆锥截面对称面径线分布的时间平均切向速度和轴向涡量范围较广;在脉冲循环控制下,动量传递的主要表现在离散涡的形成而不是气流的加速。
對等離子體誘導流場特性進行研究,有利于解決雙穩態非對稱分離渦帶來的連續比例控製睏難的問題。在封閉光學玻璃箱體內,應用介質阻擋放電等離子體對20°頂角圓錐附近靜止大氣進行瞭定常和脈遲循環控製,對等離子體誘導的圓錐截麵繞流速度場進行瞭二維PIV測量,對定常控製和脈遲循環控製下最大繞流速度及最大軸嚮渦量進行瞭比較分析。實驗結果錶明:相對于定常控製模式,脈遲循環控製下沿垂直于圓錐截麵對稱麵徑線分佈的時間平均切嚮速度和軸嚮渦量範圍較廣;在脈遲循環控製下,動量傳遞的主要錶現在離散渦的形成而不是氣流的加速。
대등리자체유도류장특성진행연구,유리우해결쌍은태비대칭분리와대래적련속비례공제곤난적문제。재봉폐광학파리상체내,응용개질조당방전등리자체대20°정각원추부근정지대기진행료정상화맥충순배공제,대등리자체유도적원추절면요류속도장진행료이유PIV측량,대정상공제화맥충순배공제하최대요류속도급최대축향와량진행료비교분석。실험결과표명:상대우정상공제모식,맥충순배공제하연수직우원추절면대칭면경선분포적시간평균절향속도화축향와량범위교엄;재맥충순배공제하,동량전체적주요표현재리산와적형성이불시기류적가속。
Research of flow characteristics induced by periodic-pulsed plasma can solve the problem of control continuous difficulties brought by two steady state asymmetric separation vortexes.A pair of plasma actuators is added behind the original plasma actuator pair over a 20° conical forebody to extend the angle of attack range for lateral control.Flow induced by the additional actuator in a still air chamber with one atmospheric pressure is investigated using a two-dimensional particle image velocimetry.The effects of pulse duty ratio and pulse frequency on the induced maximum crossflow velocity and maximum axial vorticity are compared with those of steady discharge.The tests indicate that the ensemble-averaged tangential velocity profile along a radial line perpendicular to the body symmetry plane induced by periodic-pulsed discharge is thicker than that of steady actuation.This is caused by formation of stronger discrete vortices that leave the cone surface in the unsteady actuation case.The main mechanism of momentum transfer under periodic-pulsed actuation is the formation of discrete vortices,rather than the gas acceleration.