Seshadri, SN and Rajendra, G (1974) Appplication of the method of axial source for calculation of subcritical pressure distribution on 'Not'slender axisymmetric bodies at zero lift. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
Application of axial distribution of sources based on13; e11x2014;known linearized theory for the calculation of suberxtlea'pressure distribution on. axisymmetric not-so-slender bodies is described. Closed form expressions have been derived for perturbation velocities by approximating the axial rate of change of area istribution of the given body by a polynomial.Results obtained for a parabolic are body show good agreementn with Sprietex's slender body theory.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Axial source;Axisymmetrics |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | National Trisonic Aerodynamic Facility, National Trisonic Aerodynamic Facility |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 22 Sep 2006 |
| Last Modified: | 24 May 2010 09:50 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2690 |
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