| dc.creator |
Lilley, G. M. |
|
| dc.creator |
Westley, R. |
|
| dc.creator |
Yates, A. H. |
|
| dc.creator |
Busing, J. R. |
|
| dc.date |
2012-09-12T13:25:04Z |
|
| dc.date |
2012-09-12T13:25:04Z |
|
| dc.date |
1953-02 |
|
| 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/1826/7569 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4749 |
|
| dc.description |
The noise problem associated with an aircraft flying at supersonic speeds is shown to depend primarily on the shock wave pattern formed by the aircraft. The noise intensity received by a ground observer from a supersonic aircraft flying at high as well as low altitudes, is shown to be high although it is of a transient nature. Continues… |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Reports |
|
| dc.relation |
71 |
|
| dc.title |
On some aspects of the noise propagation from supersonic aircraft |
|
| dc.type |
Report |
|