Srinathkumar, S and Parameswaran, V and Girija, G (1986) Estimation of the longitudinal stability characterisiticvs 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: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Systems Engineering Division |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 12 Oct 2012 14:01 |
| Last Modified: | 12 Oct 2012 14:01 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11087 |
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