Boundary-layer flow along a ridge: alternatives to the Falkner-Skan solutions

被引:13
作者
Duck, PW
Stow, SR
Dhanak, MR
机构
[1] Univ Manchester, Dept Math, Manchester M13 9PL, Lancs, England
[2] Florida Atlantic Univ, Dept Ocean Engn, Boca Raton, FL 33431 USA
来源
PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES | 2000年 / 358卷 / 1777期
关键词
three-dimensional boundary layers; flows along a ridge; Falkner-Skan; non-uniqueness; similarity solutions;
D O I
10.1098/rsta.2000.0697
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
We consider the laminar boundary-layer flow past a semi-infinite plate with a streamwise ridge. We seek similarity solutions to the problem, when the freestream velocity takes the form x*n, where x* denotes the distance from the leading edge of the plate; such solutions may exist if the transverse and lateral scales of the ridge develop in the streamwise direction at the same rate as the boundary-layer thickness grows. In deriving the necessary far-field boundary conditions for these calculations, we are led to a consideration of a class of flows of the Falkner-Skan type, but which may possess a cross-flow component of velocity (which grows linearly in the cross-flow direction). This new class of how is a three-dimensional alternative to the Falkner-Skan family. Wall transpiration effects are also addressed and portions of the solution curves correspond to separated flows. Solutions for the flow along a ridge for both the aforementioned classes of far-field behaviour are presented. A study of the effects of relaxing the similarity constraint on both the classical solution and new families of solution is also made. It is found that the problem is (frequently) complicated by the existence of spatially developing eigensolutions (originating from the leading edge), which have the effect of rendering standard parabolic marching procedures ill posed.
引用
收藏
页码:3075 / 3090
页数:16
相关论文
共 17 条
[1]   NON-UNIQUENESS OF HYPERSONIC BOUNDARY-LAYER [J].
BROWN, SN ;
STEWARTSON, K .
QUARTERLY JOURNAL OF MECHANICS AND APPLIED MATHEMATICS, 1975, 28 (FEB) :75-90
[2]  
CHAPMAN DR, 1950, 958 NACA
[3]   BOUNDARY LAYERS WITH SMALL DEPARTURES FROM FALKNER-SKAN PROFILE [J].
CHEN, KK ;
LIBBY, PA .
JOURNAL OF FLUID MECHANICS, 1968, 33 :273-&
[4]   REVERSE FLOW SOLUTIONS OF FALKNER-SKAN EQUATION FOR LAMBDA GREATER THAN OR EQUAL TO 1 [J].
CRAVEN, AH ;
PELETIER, LA .
MATHEMATIKA, 1972, 19 (37) :135-&
[5]   3-DIMENSIONAL FLOW NEAR A 2-DIMENSIONAL STAGNATION POINT [J].
DAVEY, A ;
SCHOFIELD, D .
JOURNAL OF FLUID MECHANICS, 1967, 28 :149-+
[6]   The effects of freestream pressure gradient on a corner boundary layer [J].
Dhanak, MR ;
Duck, PW .
PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 1997, 453 (1964) :1793-1815
[7]   Non-similarity solutions to the corner boundary-layer equations (and the effects of wall transpiration) [J].
Duck, PW ;
Stow, SR ;
Dhanak, MR .
JOURNAL OF FLUID MECHANICS, 1999, 400 :125-162
[8]  
Hartree DR, 1937, P CAMB PHILOS SOC, V33, P223
[9]   SOME PERTURBATION SOLUTIONS IN LAMINAR BOUNDARY-LAYER THEORY .1. THE MOMENTUM EQUATION [J].
LIBBY, PA ;
FOX, H .
JOURNAL OF FLUID MECHANICS, 1963, 17 (03) :433-449
[10]   THEORY OF VISCOUS HYPERSONIC FLOW [J].
MIKHAILOV, VV ;
NEILAND, VY ;
SYCHEV, VV .
ANNUAL REVIEW OF FLUID MECHANICS, 1971, 3 :371-+