Srinathkumar, S and Parameswaran, V and Girija, G (1986) Estimation of teh longitudinal stability characteristics of MiG-21BIS aircraft from flight data. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
This report presents the parameter estimation results derived from flight test data of a MIG-21BIS aircraft. The flight test program was executed by Aircraft & Systems Testing Establishment (ASTE) and the flight data analysis was carried out at NAL. The aircraft was tested in four configurations to evaluate the effect of i) a vortex plate attached to the leading edge of the wing to improve the drag characteristics and ii) a larger saddle tank to improve the range.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Flight test, Parameter estimation, Stability derivatives |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Systems Engineering Division, Systems Engineering Division, Systems Engineering Division |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 10 May 2012 11:43 |
| Last Modified: | 10 May 2012 11:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10447 |
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