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.
![]() |
PDF
tr_ae_tm_14_74.pdf Restricted to Repository staff only Download (834kB) |
![]() |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Restricted to Repository staff only Download (3kB) |
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: | Monograph (Technical Report) |
---|---|
Uncontrolled Keywords: | Axial source;Axisymmetrics |
Subjects: | AERONAUTICS > Aerodynamics |
Depositing User: | M/S ICAST NAL |
Date Deposited: | 22 Sep 2006 |
Last Modified: | 24 May 2010 04:20 |
URI: | http://nal-ir.nal.res.in/id/eprint/2690 |
Actions (login required)
![]() |
View Item |