Anantha, KV and Mathur, NB and Krishnan, V (1989) Design characteristics of the variable supersonic nozzle of the base flow facility. 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 (10Mb) |
Abstract
The Base Flow Facility which is a blowdown type of wino tunnel has been designed and is being constructed for simulating afterbqpy'flows of aerospace vehicles during wind tunnel experiments. The facility has an axisynmetric variable supersonic nozzle to achieve different test Mach numters upto a maximum of 4.O and an enclosed free-jet type test section. The nozzle outerbony movement for obtaining required test Mach numhers and annular areas are computed from the inner 2nd outerbody contours, supplied by AMRD international Corporation, U.S.A. The Counter reading settings, for various test mach numbers are also computed and presented in this report.13; i
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Base flow facility;Nozzle;Outer body;Inner body |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Fluid Dynamics, Fluid Dynamics, Fluid Dynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 14 Aug 2006 |
| Last Modified: | 24 May 2010 09:45 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2098 |
Actions (login required)
| View Item |
