Kumar, Anand and Das, A (1987) Numerical solution of flow fields around delta wings using euler equations method. Technical Report. National Aeronautical Laboratory, Bangalore,India.
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Abstract
Flow over cropped delta wings having a leading edge sweep of 65quot; and aspect ratio of 1.38 are coinputed using the DFVLR Euler code. I3oth sharp and round leading edges are considered. Calculations are pcrforrlied for angles of incidence of 10quot;, 20quot; and 24.' for free-steain Nlach number of 0.95 and for angles of incidence of 2quot;, lo' to 30quot; (5') for free-stream mach number of 04. Influence of grid refinement and surface pressure evaluation on the solution are also studied.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Euler equations;Vortex flow;Delta wing |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 03 Oct 2006 |
| Last Modified: | 24 May 2010 04:21 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2835 |
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