Girigoswami, H (1986) Through flow analysis within axial flow turbomachinery blade rows. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
Using Katsani's Through Flow Code, inviscid flow through13; an axial flow compressor rotor blade as well as flow13; through inlet guide vanes are analysed and the computed13; parameters such as meridional velocity distribution, axial velocity distribution along radial lines and velocity distribution over blade surface are presented here.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Through flow |
| Subjects: | AERONAUTICS > Aircraft Propulsion and Power |
| Division/Department: | Propulsion Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 24 Jul 2006 |
| Last Modified: | 24 May 2010 09:46 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2180 |
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