Vepa, Ranjan (1978) Role of aeroelasticity in helicopter design. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
The author offers a personal perspective on how rotocraft aeroelasticity fits into the design of a modern helicopter rotocraft aeroelasticity can be used with advantage towards the design of a modern helicopter a re reviewed.for extensive software for purposes of simulation is The manner in which recent developments in the need emphasized.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Aeroelasticity;Helicopters;Design |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 03 Nov 2006 |
| Last Modified: | 24 May 2010 04:22 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3186 |
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