Viswanath , PR (1985) Aerodynamics of delta wing-body Combinations at high angles of attack - A project proposal. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
Aerodynamics of highly swept wing-body configurations are dominated by vortex flows at high angles of attack . This research is proposed with a view to improving our general understanding on the nature of the vortical interactions on delta wing-body combinations and to provide information on static aerodynamic characteristics at high angles of attack. Experiments are proposed on two delta wing-body configurations at subsonic speeds. It is hoped that the results obtained from this investigation will be useful in the preliminary design of combat aircraft of the future.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | High angle of attack aerodynamics;Delta wings |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 26 Sep 2012 14:09 |
| Last Modified: | 26 Sep 2012 14:09 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11024 |
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