Venugopal, S and Krishna Murthy, M (1989) A computer code based on experimental database to estimate the fin alone normal force characteristics upto high angles of attack. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
A computer code has been developed to compute the normal force characteristics of thin wings with zero trailing-edge, sweep upto very high angles of attack . The code covers a range of aspect ratios from 0.5 to 3.53 and taper ratios of 0 to 1.0. The Mach number range covered is from 0.8 to 3.0. The method uses linear/quadratic interpolation/extrapolation from a data base constructed using the limited experimental data available in the literature.
| Item Type: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | Wing characteristics;Normal force;High angle of attack |
| Subjects: | AERONAUTICS > Aerodynamics MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 19 Dec 2012 04:37 |
| Last Modified: | 19 Dec 2012 04:37 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11402 |
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