| dc.creator |
Boyd, E. A. |
|
| dc.date |
2014-11-25T17:38:53Z |
|
| dc.date |
2014-11-25T17:38:53Z |
|
| dc.date |
1960-11 |
|
| dc.date.accessioned |
2022-05-09T10:17:27Z |
|
| dc.date.available |
2022-05-09T10:17:27Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/8815 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4815 |
|
| dc.description |
The two-dimensional hypersonic sail is examined using the Newton-
Busemann pressure law. The results are compared with those of Daskin
and Feldman (1958) who used the empirical modified Newtonian pressure
law. It is found that for a given chord length of sail a corrected sail
will give a specified lift for a smaller tension in the sail.
At a flight Mach number of 10 at 100,000 ft. the tension in one
particular sail considered could be supported with a working stress
of about 20 tons/in[squared]. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics |
|
| dc.relation |
College of Aeronautics Reports |
|
| dc.relation |
140 |
|
| dc.relation |
COA/140 |
|
| dc.title |
Busemann correction to the characteristics of the two-dimensional hypersonic sail |
|
| dc.type |
Report |
|