| dc.creator |
Barna, P. S. |
|
| dc.date |
2017-02-28T13:11:31Z |
|
| dc.date |
2017-02-28T13:11:31Z |
|
| dc.date |
1957-05 |
|
| dc.date.accessioned |
2022-05-09T10:07:05Z |
|
| dc.date.available |
2022-05-09T10:07:05Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/11511 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4426 |
|
| dc.description |
Experimental investigations have been made of the
now characteristics on wings of moderate sweepback.
This note presents the results of the experimental investigation
into the pressure distribution over a swept back
wing, having an aspect ratio 4. 5 and sweep back angle 40°
at quarter chord. A half model technique has been used.
The wing section was R. A. E. 101 (symmetrical) with 6%
maximum thickness and zero camber. Measurements of
chordwise pressure distributions at a number of spanwise
sections were made in the incidence range 2 - 32°. The
experiments were performed at Reynolds numbers of 0. 9 x 10(6)
and 2 x 10(6) (based on geometric mean chord). From these
measurements, lift, drag and pitching moment characteristics
of the wing were calculated. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics |
|
| dc.relation |
CoA/N-65 |
|
| dc.relation |
65 |
|
| dc.title |
A preliminary report on the aerodynamic characteristics of a 40 degrees swept back wing of aspect ratio 4.5 |
|
| dc.type |
Report |
|