航空工程进展
航空工程進展
항공공정진전
ADVANCES IN AERONAUTICAL SCIENCE AND ENGINEERING
2014年
3期
296-301
,共6页
陈燕君%吴榕%梁峰%宋歌
陳燕君%吳榕%樑峰%宋歌
진연군%오용%량봉%송가
地效翼船%水橇%水动力特性%升阻比%FLUENT软件
地效翼船%水橇%水動力特性%升阻比%FLUENT軟件
지효익선%수취%수동력특성%승조비%FLUENT연건
wing-in-ground effect vehicle%hydro-ski%hydrodynamic characteristics%lift-drag ratio%FLUENT sof tw are
地效翼船的发展过程中,必须解决一大技术性难题:起飞过程中升阻比较小,使得船身无法快速抬离水面。基于以上问题,根据船身理论、机翼设计理论和冯·卡门入水冲击理论等,设计一种应用于地效翼船的水橇,利用CATIA对水橇进行三维建模,并使用FLUENT 软件对该水橇进行水动力特性的数值模拟。结果表明:水橇的升力系数和阻力系数随着攻角的增大而增大,其升阻比呈抛物线趋势,在攻角为5°左右到达最大值;相对其他来流速度,水橇在来流速度2m/s时的升力系数、阻力系数和升阻比更大。
地效翼船的髮展過程中,必鬚解決一大技術性難題:起飛過程中升阻比較小,使得船身無法快速抬離水麵。基于以上問題,根據船身理論、機翼設計理論和馮·卡門入水遲擊理論等,設計一種應用于地效翼船的水橇,利用CATIA對水橇進行三維建模,併使用FLUENT 軟件對該水橇進行水動力特性的數值模擬。結果錶明:水橇的升力繫數和阻力繫數隨著攻角的增大而增大,其升阻比呈拋物線趨勢,在攻角為5°左右到達最大值;相對其他來流速度,水橇在來流速度2m/s時的升力繫數、阻力繫數和升阻比更大。
지효익선적발전과정중,필수해결일대기술성난제:기비과정중승조비교소,사득선신무법쾌속태리수면。기우이상문제,근거선신이론、궤익설계이론화풍·잡문입수충격이론등,설계일충응용우지효익선적수취,이용CATIA대수취진행삼유건모,병사용FLUENT 연건대해수취진행수동력특성적수치모의。결과표명:수취적승력계수화조력계수수착공각적증대이증대,기승조비정포물선추세,재공각위5°좌우도체최대치;상대기타래류속도,수취재래류속도2m/s시적승력계수、조력계수화승조비경대。
In the development course of wing-in-ground effect vehicle ,there remains one major technical issue ,i .e .in the process of taking off the lift-drag ratio is too small to lift the aircraft body out from the water rapidly .To solve this difficult problem ,according to the hull theory ,wing design theory and the Theodore Von Karman wa-ter impact theory ,a new hydro-ski applied in wing-in-ground effect vehicle is designed ,and the software CATIA is used to draw 3D model of the hydro-ski ,and the FLUENT is used to figure out the vehicle’s hydrodynamic characteristics .Results show that lift coefficient and drag coefficient of the hydro-ski increases as the angle of attack increases .In addition ,the lift-drag ratio curve is shown as a parabola ,peaking at 5° .In the meantime , when the incoming flow velocity is 2 m/s ,the lift coefficient ,drag coefficient and CL/CD is larger than that of the others .