火箭绕流问题与解析函数边值问题  

The Problems of Flow Around Rocket and Boundary Value Problems of Analytic Functions

作　　者：仇淑芬 

机构地区：[1]首都师范大学数学系

出　　处：《首都师范大学学报（自然科学版）》1996年第3期63-67,共5页Journal of Capital Normal University：Natural Science Edition

摘　　要：用解析函数边值问题，解决火箭尾翼剖面绕流的复势，复速度，升为及力矩等问题．In thin paper, ths traditional problems of Complex potential, complex Velocity, elevating force and force moment in the flow around rocket tail profile have been studied by usingthe theory of boundory value problem of analytic functions.

关 键 词：保形变换 解析函数 边值问题 火箭 绕流 

分 类 号：V421[航空宇航科学与技术—飞行器设计] O174.55[理学—数学]