COMPUTATION OF STEADY AND UNSTEADY VISCOUS FLOWS USING A SIMULTANEOUSLY COUPLED INVISCID-VISCOUS INTERACTION TECHNIQUE

被引:7
作者
CIZMAS, PGA
HALL, KC
机构
[1] Department of Mechanical Engineering and Materials Science, Duke University, Durham
关键词
D O I
10.1006/jfls.1995.1035
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
An interacting viscous-inviscid method for efficiently computing steady and unsteady low Mach number viscous flows with separation is presented. The inviscid region is modeled using a finite element discretization of the full potential equation. The viscous region is modeled using a finite difference boundary layer technique. The two regions are-simultaneously coupled through the requirement that the edge velocities of the two regions be equal, and through an injection velocity arising from the displacement thickness. For unsteady flows, the fluid how is assumed to be composed of two parts: a mean or steady flow plus a harmonically varying small unsteady disturbance. This assumption results in a nonlinear description for the mean flow, and a linear description for the small disturbance unsteady flow. For the solution of the mean how the nonlinear governing equations are reduced to a series of linear matrix equations using Newton iteration. The resulting mean how solution is then used to form the variable coefficients of the linearized unsteady equations, which are solved directly. The present method is able to compute flows with separation, and in the case of unsteady flows, flows with moving separation and reattachment points. (C) 1995 Academic Press Limited
引用
收藏
页码:639 / 657
页数:19
相关论文
共 39 条
[1]   UNSTEADY LAMINAR BOUNDARY-LAYER ON A SEMI-INFINITE FLAT PLATE DUE TO SMALL FLUCTUATIONS IN MAGNITUDE OF FREE-STREAM VELOCITY [J].
ACKERBERG, RC ;
PHILLIPS, JH .
JOURNAL OF FLUID MECHANICS, 1972, 51 (JAN11) :137-+
[2]   ANALYSIS OF HIGH REYNOLDS-NUMBER INVISCID VISCID INTERACTIONS IN CASCADES [J].
BARNETT, M ;
VERDON, JM ;
AYER, TC .
AIAA JOURNAL, 1993, 31 (11) :1969-1976
[3]   INVISCID-VISCOUS INTERACTION ANALYSIS OF COMPRESSOR CASCADE PERFORMANCE [J].
BARNETT, M ;
HOBBS, DE ;
EDWARDS, DE .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1991, 113 (04) :538-552
[4]   Irrotational motion of a compressible inviscid fluid [J].
Bateman, H .
PROCEEDINGS OF THE NATIONAL ACADEMY OF SCIENCES OF THE UNITED STATES OF AMERICA, 1930, 16 :816-825
[5]  
BRUNE GW, 1974, AIAA74601 PAP
[6]  
CARTER JE, 1979, AIAA791490 PAP
[7]   INTEGRATION OF 2-DIMENSIONAL LAMINAR BOUNDARY-LAYER EQUATIONS PAST POINT OF VANISHING SKIN FRICTION [J].
CATHERALL, D ;
MANGLER, KW .
JOURNAL OF FLUID MECHANICS, 1966, 26 :163-+
[8]   AN INVISCID-VISCOUS INTERACTION APPROACH TO THE CALCULATION OF DYNAMIC STALL INITIATION ON AIRFOILS [J].
CEBECI, T ;
PLATZER, MF ;
JANG, HM ;
CHEN, HH .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1993, 115 (04) :714-723
[9]   CALCULATION OF UNSTEADY 2-DIMENSIONAL LAMINAR AND TURBULENT BOUNDARY-LAYERS WITH FLUCTUATIONS IN EXTERNAL VELOCITY [J].
CEBECI, T .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 1977, 355 (1681) :225-238
[10]  
Cebeci T., 1974, ANAL TURBULENT BOUND