Poornima, L and Seshadri, K (1991) Instrumentation for ASE Experiments in the Dynamic Wind Tunnel. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
The instrumentation package developed for use with the13; flexible wing models to be tested in the dynamic wind tunnel for aero-servo-elastic studies is detailed.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Strain gauge amplifiers;Servo drive;Aero-servo-elasticity |
| Subjects: | AERONAUTICS > Avionics & Aircraft Instrumentation |
| Division/Department: | Other, Flight Mechanics and Control Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 23 Jun 2006 |
| Last Modified: | 24 May 2010 09:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1791 |
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