| dc.creator |
Young, A. D. |
|
| dc.creator |
Kirkby, S. |
|
| dc.date |
2012-05-08T18:35:59Z |
|
| dc.date |
2012-05-08T18:35:59Z |
|
| dc.date |
1947-09 |
|
| dc.date.accessioned |
2022-05-09T10:17:16Z |
|
| dc.date.available |
2022-05-09T10:17:16Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7127 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4693 |
|
| dc.description |
The linearised theory is developed in some detail in order to clarify the differences between two-dimensional and axi-symmetric flow. In agreement with other authors it is concluded that the perturbation velocity on a thin body of revolution in compressible flow is 1/β2 times the perturbation velocity in incompressible flow on a thinner body at reduced incidence obtained by reducing the lateral dimensions of the original body in the ratio (3:1).
This result is applied to a representative family of streamline bodies of revolution at zero incidence. Continues… |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Report |
|
| dc.relation |
11 |
|
| dc.title |
Application of the linear perturbation theory to compressible flow about bodies of revolution |
|
| dc.type |
Report |
|