Jain, Ashok K (1982) Performance Evaluation of Two-dimensional External Compression Inlet Configuration at Supersonic Speeds13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
tr_pd_ae_tm_3_82_txt.pdf Restricted to Repository staff only Download (23MB) |
![[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 (12kB) |
Abstract
A computing method for the estimation of the various performance parameters like critical mass flow ratio, spillage, additive drag coefficient, shock stand-off distance, entry Mach number, total pressure recovery and static pressure rise, of two dimensional, external compression, supersonic single ramp inlet configurations13; operating at critical an.d subcritical conditions is presented here, Using. the Ferri criterion, the stability margin for the subcritical mode of operation of the inlet has been worked out.For better performance characteristics, the present method suggests that the inlet should be designed to have some spillage at13; design Mach number.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Inlet configeration;Mass flow ratio |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | Poornima Narayana |
| Date Deposited: | 31 Aug 2006 |
| Last Modified: | 24 May 2010 04:19 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2526 |
Actions (login required)
 |
View Item |
