Jayaraman, V and Rudrakumar, S (1996) Experimental Study On Upswept Afterbody Shapes Of Light Transport Aircraft. Technical Report. NAL, Bangalore.
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Abstract
Low Speed Experiments Of Parametric Study On Few Upswept Afterbody Models Were Carriedout In The 0 .9m Diameter. Low Speed Tunnel For Independent Determination Of Profile And Vortex Drag Using 3-D Wake Survey Method, With A Primary Objective Of Providing Preliminary Information About Afterbody Drag Relevant To Light Transport Aircraft . This Study Has Broughtout Particularly The Influences Of Various Afterbody Geometric Parameters On The Vortex Drag.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Wind Tunnel Testing Upswept After Body Shapes-3 D Wake Survey Vortex Drag |
| Subjects: | ASTRONAUTICS > Astronautics (General) |
| Division/Department: | Flight Mechanics , Experimental Aerodynamics Division |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 23 Aug 2012 10:58 |
| Last Modified: | 23 Aug 2012 10:58 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10798 |
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