A NUMERICAL METHOD FOR CALCULATING UNSTEADY 2-DIMENSIONAL LAMINAR BOUNDARY LAYERS

被引：12

作者：

HALL, MG

机构：

[1] Aerodynamics Department, Royal Aircraft Establishment, Farnborough, Hampshire

来源：

INGENIEUR ARCHIV | 1969年 / 38卷 / 02期

关键词：

D O I：

10.1007/BF00542573

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

A method for calculating unsteady two dimensional boundary layers in laminar incompressible flow has been developed and tested. No restrictive assumptions are made regarding the time-dependent terms in the boundary-layer equation. The differential equations are solved with an implicit difference scheme similar to that employed for steady two-dimensional boundary layers. At each step, here, known conditions at three stations are used to calculate the conditions at a new (fourth) station. The entire field is covered by a succession of these steps. © 1969 Springer-Verlag.

引用

页码：97 / &

共 8 条

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[3] ON NUMERICAL SOLUTION OF UNSTEADY LAMINAR BOUNDARY LAYERS [J].

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[4] BOUNDARY LAYER OVER AN IMPULSIVELY STARTED FLAT PLATE [J].

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[5]

HALL MG, UNPUBLISHED REPORT

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[7]

Richtmyer R.D., 1994, DIFFERENCE METHODS I

[8]

STUART JT, 1963, LAMINAR BOUNDARY LAY, P349

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