Ramaswamy, MA and Parikh, PC (1975) Pressure distribution of aerofoils if embedded supersonic region. Technical Report. National Aeronautical Laboratory, Bangalore,India.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
tr_ae_tm_18_75.pdf Restricted to Repository staff only Download (684kB) |
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/other.png) |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Restricted to Repository staff only Download (3kB) |
Abstract
An exploratory attempt at empirically determining the pressure distribution on aerofoils in the embedded supersonic region using the concept of 'Expansion angle sand 'Compression angle ' in the flow development and the concept of connected points, both put forward by Pearcey (l), has been presented Prediction of the pressure distribution over the initial region is based on an universal compression rate curve and that over the region beyond it is based on an empirical correlation for the connected regions.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Airfoil embedded supersonics |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 14 Sep 2006 |
| Last Modified: | 24 May 2010 04:20 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2717 |
Actions (login required)
 |
View Item |
