| dc.creator |
Bolton Shaw, B. W. |
|
| dc.date |
2012-06-08T10:51:57Z |
|
| dc.date |
2012-06-08T10:51:57Z |
|
| dc.date |
1950-05 |
|
| dc.date.accessioned |
2022-05-09T10:17:18Z |
|
| dc.date.available |
2022-05-09T10:17:18Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7206 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4712 |
|
| dc.description |
Expressions are derived for lξ and a2 of nose ailerons and nose elevators on a delta wing, as depicted in Fig. 1, in supersonic flight. Nose and trailing edge controls on delta wings in supersonic flight are compared. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield. |
|
| dc.relation |
College Report |
|
| dc.relation |
36 |
|
| dc.title |
Nose controls on delta wings at supersonic speeds |
|
| dc.type |
Report |
|