Viswanath, PR (1985) A project proposal for high angle of attack aerodynamic characteristics of wing-body combinations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
tr_pdae_8518_R85689_txt.pdf Restricted to Repository staff only Download (2MB) |
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/other.png) |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Restricted to Repository staff only Download (2kB) |
Abstract
Aerodynamics of highly swept wing-body configurations are13; 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 1s hoped that the results obtained from this investigation will be useful in the preliminary design of combat aircraft of the future.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | High angle of attack aerodynamics;Delta wings |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | Poornima Narayana |
| Date Deposited: | 03 Aug 2006 |
| Last Modified: | 24 May 2010 04:16 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2256 |
Actions (login required)
 |
View Item |
