Prathapanayaka, R and Shembharkar, TR (2005) CFD ANALYSIS OF A CONTROLLED DIFFUSION AEROFOIL. Technical Report. NAL, Bangalore.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF - Published Version Restricted to Registered users only Download (281Kb) | Request a copy |
Abstract
As a part of the validation exercise for the Dawes code ‘un_b3d_ke’, the code has been used to compute the flow over a controlled diffusion aerofoil (CDNAL) for which extensive cascade test data is available in-house for comparison. Computations have been carried out for full blade span (3-D) and thin slice (Quasi 3-D) for a given inlet condition. The computed surface Mach number distribution and wake profiles have been discussed and compared with the TCT (NAL) cascade test results.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Subjects: | AERONAUTICS > Aircraft Propulsion and Power |
| Division/Department: | Propulsion Division, Propulsion Division |
| Depositing User: | Mr R Prathapanayaka |
| Date Deposited: | 23 Jul 2010 16:30 |
| Last Modified: | 23 Jul 2010 16:30 |
| URI: | http://nal-ir.nal.res.in/id/eprint/8669 |
Actions (login required)
| View Item |
