How the Raleigh Flow Transits to Blasius NumericallySource: Journal of Applied Mechanics:;1998:;volume( 065 ):;issue: 002::page 445Author:G. N. Sarma
DOI: 10.1115/1.2789074Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper answers the question numerically how a two-dimensional incompressible Rayleigh boundary layer started impulsively past a semi-infinite flat plate with uniform velocity in the mainstream transits to steady Blasius flow. It is shown that the transition is a convective transition and smooth with no discontinuities. It is effected by the parameters called the convective and angular parameters. The velocity field gets disintegrated into discrete dissimilar diffusive layers of different convective orders. This is an example based on modified boundary layer theory of Sarma. Polynomial solutions are found using the theory of definite thickness boundary layers and the method of weighted residuals. This modifies the numerical works of Hall and Dennis, which are based on Stewartson’s theory of propagation of disturbances.
keyword(s): Flow (Dynamics) , Boundary layers , Flat plates , Polynomials AND Thickness ,
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| contributor author | G. N. Sarma | |
| date accessioned | 2017-05-08T23:55:43Z | |
| date available | 2017-05-08T23:55:43Z | |
| date copyright | June, 1998 | |
| date issued | 1998 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26443#445_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/119943 | |
| description abstract | This paper answers the question numerically how a two-dimensional incompressible Rayleigh boundary layer started impulsively past a semi-infinite flat plate with uniform velocity in the mainstream transits to steady Blasius flow. It is shown that the transition is a convective transition and smooth with no discontinuities. It is effected by the parameters called the convective and angular parameters. The velocity field gets disintegrated into discrete dissimilar diffusive layers of different convective orders. This is an example based on modified boundary layer theory of Sarma. Polynomial solutions are found using the theory of definite thickness boundary layers and the method of weighted residuals. This modifies the numerical works of Hall and Dennis, which are based on Stewartson’s theory of propagation of disturbances. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | How the Raleigh Flow Transits to Blasius Numerically | |
| type | Journal Paper | |
| journal volume | 65 | |
| journal issue | 2 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.2789074 | |
| journal fristpage | 445 | |
| journal lastpage | 453 | |
| identifier eissn | 1528-9036 | |
| keywords | Flow (Dynamics) | |
| keywords | Boundary layers | |
| keywords | Flat plates | |
| keywords | Polynomials AND Thickness | |
| tree | Journal of Applied Mechanics:;1998:;volume( 065 ):;issue: 002 | |
| contenttype | Fulltext |