Nilakantan, P (1960) Criteria for selection of compressed air storage system for the trisonic wind tunnel. 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 (789Kb) |
Abstract
A Compressed Air Storage System is an essential13; research tool which finds a variety of applications for13; operating high speed wind tunnels and test rigs required13; for experimental investigations in the fields of high13; aerodynamics and propulsion. In the light of the13; developments taking place in supersonic and hyper-13; aerodynamics, the proper design and layout of such13; em that would meet our research requirements for the13; next fifteen years is a matter requiring careful thought.13; Not only should the system be flexible enough and adaptable for a variety of applications but it should also be13; capable of being integrated easily with larger systems13; that may be needed in future years. A desirable feature for immediate purposes is that the basic system designed to meet the requirements of the trisonic tunnel should also be available for operating a number of other smaller supersonic tunnels in the Wind Tunnel Centre and for pilot experiments in the propulsion laboratory that will be located near the aerodynamics laboratories.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Hyperaerodynamics;Supersonic tunnels;Wind Tunnel |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 16 Jan 2009 |
| Last Modified: | 24 May 2010 09:54 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3771 |
Actions (login required)
| View Item |
