中国航空学报(英文版)
中國航空學報(英文版)
중국항공학보(영문판)
CHINESE JOURNAL OF AERONAUTICS
2003年
2期
108-116
,共9页
宋遒志%戴全辉%陈立平%钟毅芳
宋遒誌%戴全輝%陳立平%鐘毅芳
송주지%대전휘%진립평%종의방
过渡曲面%切触线%重新参数化局部基曲面%线性组合%约束%优化
過渡麯麵%切觸線%重新參數化跼部基麯麵%線性組閤%約束%優化
과도곡면%절촉선%중신삼수화국부기곡면%선성조합%약속%우화
blending surface%reparameterized local base surface%contact curve%linear combination%constraints%optimization
在Erich Hartmann提出的由两基曲面线性组合构造Gn连续过渡曲面方法的基础上,针对该方法存在很难找到合适的参数变换的问题,提出了一种基于基曲面局部区域重新参数化构造Gn连续过渡曲面的方法.通过对基曲面上切触线附近区域部分曲面重新参数化,再由重新参数化局部基曲面线性组合构造Gn连续过渡曲面.这样将两基曲面间构造过渡曲面的问题转化为在重新参数化局部基曲面间构造过渡曲面.以构造G2连续的翼身融合面为例,讨论了满足约束要求条件时G2连续过渡面的构造方法.即先对基曲面上过渡切触线附近的局部区域进行重新参数化,后通过优化求解来确定比例因子和偏移量、平衡因子和调配因子,使过渡曲面满足前后边条线约束,最后利用线性组合来构造G2连续的过渡面.约束过渡曲面的形状可通过改变重新参数化基曲面的大小来调整.
在Erich Hartmann提齣的由兩基麯麵線性組閤構造Gn連續過渡麯麵方法的基礎上,針對該方法存在很難找到閤適的參數變換的問題,提齣瞭一種基于基麯麵跼部區域重新參數化構造Gn連續過渡麯麵的方法.通過對基麯麵上切觸線附近區域部分麯麵重新參數化,再由重新參數化跼部基麯麵線性組閤構造Gn連續過渡麯麵.這樣將兩基麯麵間構造過渡麯麵的問題轉化為在重新參數化跼部基麯麵間構造過渡麯麵.以構造G2連續的翼身融閤麵為例,討論瞭滿足約束要求條件時G2連續過渡麵的構造方法.即先對基麯麵上過渡切觸線附近的跼部區域進行重新參數化,後通過優化求解來確定比例因子和偏移量、平衡因子和調配因子,使過渡麯麵滿足前後邊條線約束,最後利用線性組閤來構造G2連續的過渡麵.約束過渡麯麵的形狀可通過改變重新參數化基麯麵的大小來調整.
재Erich Hartmann제출적유량기곡면선성조합구조Gn련속과도곡면방법적기출상,침대해방법존재흔난조도합괄적삼수변환적문제,제출료일충기우기곡면국부구역중신삼수화구조Gn련속과도곡면적방법.통과대기곡면상절촉선부근구역부분곡면중신삼수화,재유중신삼수화국부기곡면선성조합구조Gn련속과도곡면.저양장량기곡면간구조과도곡면적문제전화위재중신삼수화국부기곡면간구조과도곡면.이구조G2련속적익신융합면위례,토론료만족약속요구조건시G2련속과도면적구조방법.즉선대기곡면상과도절촉선부근적국부구역진행중신삼수화,후통과우화구해래학정비례인자화편이량、평형인자화조배인자,사과도곡면만족전후변조선약속,최후이용선성조합래구조G2련속적과도면.약속과도곡면적형상가통과개변중신삼수화기곡면적대소래조정.
This paper presents a method of generating a parametric Gn blending surface based on reparameterizing the partial surface patches in the base surfaces on the basis of Erich Hartmann method.This method is expressed as follows: Firstly, the partial region near contact curves in both base surfaces is reparameterized.The contact curves are used as the boundaries of the reparameterized partial region respectively.The reparameterized partial region in two base surfaces is called the reparameterized local base surfaces.Then the parametric Gn blending surface is generated by a linear combination of the reparameterized local base surface patches depending on one of the common parameters.Therefore, generating a Parametric Gn Blending Surface between two base surfaces is translated into generating a Parametric Gn Blending Surface between the two reparameterized local base surfaces.This paper illustrates the method to generate the Gn blending surface with some constraints by generating a G2 blending surface between the aerofoil and the body of a missile with the constraints of the forward and rear fringe curves.When the Gn blending surface with some constraints is generated, the partial region near contact curves in both base surfaces is reparameterized, and the scale factors, offset, balance factor and thumb weight are defined by meeting the constraints through using an optimization method.Then the parametric Gn blending surface is generated by the linear combination of the reparameterized local base surface patches.The shape of the blending surface can be adjusted by changing the size of the reparameterized local base surface patches.