Srikantan, KV (1975) Transonic mach number sweep system for the NAL 4'x4' trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
This note describes the design of Transonic Mach Number Sweep system meant to vaxy the Mach number during a b1owdown in the Transonic range (M = 0.8 to 1.40). Mach number steps are achieved by preset controlled operation of Transonic Control13; Flaps. The stepwise increase in Mach number is obtained through divergence of the flaps and vice versa.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Transonic mach number |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 30 Aug 2006 |
| Last Modified: | 24 May 2010 09:50 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2606 |
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