dc.creator |
Campion, B. S. |
|
dc.date |
2012-09-13T15:34:42Z |
|
dc.date |
2012-09-13T15:34:42Z |
|
dc.date |
1954-01 |
|
dc.date.accessioned |
2022-05-09T10:17:21Z |
|
dc.date.available |
2022-05-09T10:17:21Z |
|
dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7579 |
|
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4752 |
|
dc.description |
The effects if distortion on the longitudinal stability of swept wing aircraft at high speeds (sub-critical Mach numbers) are considered on a quasi-static basis. The method employed is based on the theory of Gates and Lyon but involves some extension of this theory. |
|
dc.language |
en |
|
dc.publisher |
College of Aeronautics, Cranfield |
|
dc.relation |
College Reports |
|
dc.relation |
77 |
|
dc.title |
Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers) |
|
dc.type |
Report |
|