振动与冲击
振動與遲擊
진동여충격
JOURNAL OF VIBRATION AND SHOCK
2014年
16期
165-170,193
,共7页
超空泡航行体%空泡外形%机动回转运动%离心力%临界回转角速度
超空泡航行體%空泡外形%機動迴轉運動%離心力%臨界迴轉角速度
초공포항행체%공포외형%궤동회전운동%리심력%림계회전각속도
supercavitating vehicle%cavity shape%maneuvering rotational movement%centrifugal force%critical rotation angular velocity
提出超空泡航行体空泡流型概念,将航行体外形、空泡外形、航行体外形与空泡外形匹配统一用超空泡航行体空泡流型描述,用定量关系表达超空泡航行体流体动力特性;建立机动回转运动超空泡数学模型,推导回转运动超空泡外形表达式;研究超空泡航行体由直航运动过渡到稳态机动回转运动过程,给出该过程中超空泡外形变化规律;分析角速度、离心力对机动回转运动超空泡外形影响,揭示该两因素对超空泡外形变化影响程度;以空泡外形与航行体外形匹配为约束,对机动能力进行初步评估,通过仿真计算获得表征航行体机动能力的临界回转角速度。
提齣超空泡航行體空泡流型概唸,將航行體外形、空泡外形、航行體外形與空泡外形匹配統一用超空泡航行體空泡流型描述,用定量關繫錶達超空泡航行體流體動力特性;建立機動迴轉運動超空泡數學模型,推導迴轉運動超空泡外形錶達式;研究超空泡航行體由直航運動過渡到穩態機動迴轉運動過程,給齣該過程中超空泡外形變化規律;分析角速度、離心力對機動迴轉運動超空泡外形影響,揭示該兩因素對超空泡外形變化影響程度;以空泡外形與航行體外形匹配為約束,對機動能力進行初步評估,通過倣真計算穫得錶徵航行體機動能力的臨界迴轉角速度。
제출초공포항행체공포류형개념,장항행체외형、공포외형、항행체외형여공포외형필배통일용초공포항행체공포류형묘술,용정량관계표체초공포항행체류체동력특성;건립궤동회전운동초공포수학모형,추도회전운동초공포외형표체식;연구초공포항행체유직항운동과도도은태궤동회전운동과정,급출해과정중초공포외형변화규률;분석각속도、리심력대궤동회전운동초공포외형영향,게시해량인소대초공포외형변화영향정도;이공포외형여항행체외형필배위약속,대궤동능력진행초보평고,통과방진계산획득표정항행체궤동능력적림계회전각속도。
The concept of supercavitating vehicle cavity pattern was introduced to describe in a unified way thevehicle shape,cavity shape,and their geometric matching.The hydrodynamic characteristics of supercavitating vehiclewere expressed by quantitative parameters.The mathematical model of supercarity in maneuvering rotational movement wasestablished,and the expression of supercavity shape in maneuvering rotational movement was deduced.The transition fromrectilinear motion to steady maneuvering rotational movement of supercavitating vehicle was analysed and the variation ofsupercavity shape was presented.The influences of angular velocity and centrifugal force on supercavity shape inmaneuvering rotational movement were discussed and the affection extent of these two factors were revealed.Taking thegeometric matching between cavity shape and vehicle shape as a constrant a preliminary assessment of maneuveringcapability was made,and the critical rotation angular velocity characterizing maneuvering capability was provided byunmerical simulation.