dc.contributor.author |
D. W. Holder |
en_US |
dc.contributor.author |
R. J. North |
en_US |
dc.date.accessioned |
2014-10-21T15:52:49Z |
|
dc.date.available |
2014-10-21T15:52:49Z |
|
dc.date.issued |
1949 |
en_US |
dc.identifier.other |
ARC/R&M-2781 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3332 |
|
dc.description.abstract |
A 9 X 3 in. high-speed wind tunnel driven by a compressed-air injector has been built in the Aerodynamics Division of the National Physical Laboratory. The tunnel operates at roughly atmospheric stagnation pressure and has so far been used to give Mach numbers up to 1.8. The general arrangement of the tunnel and the preliminary calibration, which is generally satisfactory, are described. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
The 9 x 3 in. induced-flow high-speed wind tunnel at the national physical laboratory |
en_US |