Kangovi, S and Krishnan, V (1982) Measurements related to afterbody studies on thrust-minus-drag rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Restricted to Archive staff only Download (22Mb) |
Abstract
The need for proper afterbody design is on account of its13; significant influence on the net thrust and total drag of an air-craft. Achievements of such a design has become significantly difficult with ,the advent of multimission aircraft requiring variable geometry nozzle(s) operating over a broad range of conditions. In view of the complexity of flow field in the afterbody region and also due to the limitations of available semi-empirical and analytical methods,; the wind tunnel, tests are essential to get accurate quantitative results.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Wind tunnel;Reynolds number;Boat-tail pressure distribution |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 28 Aug 2006 |
| Last Modified: | 24 May 2010 09:48 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2500 |
Actions (login required)
| View Item |
