Vimala, CS and Nath, G (1975) Mass transfer effectiveness on three-dimensional laminar compressible boundary layer flows. Journal of Fluids Engineering, 97 . pp. 382-384.Full text not available from this repository.
The effects of mass transfer on laminar boundary-layer flow with or without slip on an axisymmetric surface of variable cross section in the case of compressible swirling flow are investigated together with the same effects on the laminar compressible boundary-layer flow over a yawed infinite wing in the case of hypersonic flow. The similarity equations governing these two flows are solved by a quasi-linearization technique. Numerical values of the skin-friction and heat-transfer parameters for the axisymmetric surface and yawed infinite wing are tabulated for different values of the mass-transfer and slip parameters.
|Item Type:||Journal Article|
|Uncontrolled Keywords:||Compressible boundary layer;Hypersonic flow;Infinite span wings;Laminar boundary layer;Mass Transfer;Three dimensional boundary layer;Flow equations;Laminar heat transfer; Linearization;Similarity theorem;Skin friction;Swirling|
|Subjects:||ENGINEERING > Fluid Mechanics and Thermodynamics|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||12 Jan 2007|
|Last Modified:||24 May 2010 09:54|
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