Viswanathan, S (1970) Programs to analyze supersonic flow past right circular cones with a view to make use of uncalibrated cones for determination of flow angles and mach numbers in wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
Two programs are developed for SIRIUS Digital computer to13; analyse the supersonic flow around right circular cones at zero angle of attack and at small angle of attack. These programs can be used 1;0 generate tables similar to NASA SP-3004 (Ref.1) and NASA SP-3007( Ref.2). Certain modif1cations are incorporated in the programs to make use of13; the same to calibrate any wind tunnel in supersonic range for local flow inclination and free stream Mach number using an uncalibrated conical pressure probe,
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | SIRIUS digital computer;Trisonic wind tunnel |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 10 Nov 2006 |
| Last Modified: | 24 May 2010 09:53 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3343 |
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