Sundaram, S (1988) Skin friction measurements in a turbulent boundary layer. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Restricted to Archive staff only Download (655Kb) |
Abstract
Skin friction measurements were made in a 'two-dimensional13; turbulent boundary layer under zero pressure gradient by several techniques . The techniques include devices using razor blade ., and sub layer fence . The classical clauser chart method and Bradshaw's scheme were also used in all the tests reported here . The tests were conducted at a unit Reynolds number of 1 .4 million per metre . The applicability of these techniques to a confluent boundary layer was evaluated . 13; A new and simple method of making the sub-layer fence described here was tested for its applicability as a skin friction measuring device . This simple . _device was found to be as good quot;as the regular machined fence generally used for such accurate measurement of wall shear stress .
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Two-dimentional;Turbulent boundary layer;Skin friction;Sub-13; layer fence;Razor technique;Zero-pressure gradient |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Division/Department: | Fluid Dynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 07 Jul 2006 |
| Last Modified: | 24 May 2010 09:45 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2117 |
Actions (login required)
| View Item |
