Viswanath, PR (1986) Buffet onset measurements on an Aircraft model at transonic mach numbers. 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 (8Mb) |
Abstract
Buffet onset measurements have been performed on a low13; aspect ratio, moderately swept, aircraft model at three13; transonic Mach numbers in the 1.2m tunnel. Instrumentation13; included wing root strain gauges, a wing tip accelerometer13; wing trailing edge pressure taps and standard six component13; internal obtained strain gauge balance. Results of buffet onset by these different techniques are compared. A discussion of the buffet onset results as it relates to the main features of the flow on the wing upper surface is also included.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Buffet onset;Buffet response;Transonic buffet |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 04 Sep 2006 |
| Last Modified: | 24 May 2010 09:50 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2617 |
Actions (login required)
| View Item |
