dc.contributor.author |
N. Gregory |
en_US |
dc.contributor.author |
W. G. Raymer |
en_US |
dc.contributor.author |
Edna M. Love |
en_US |
dc.date.accessioned |
2014-10-21T15:56:18Z |
|
dc.date.available |
2014-10-21T15:56:18Z |
|
dc.date.issued |
1962 |
en_US |
dc.identifier.other |
ARC/R&M-3388 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3970 |
|
dc.description.abstract |
Five-tube yawmeter traverses immediately up and downstream of the fan reveal the flow maldistributions due to forward speed. These are removed by a deep duct or an inlet cascade, which turn the air into the axial direction. Non-uniformity of the exit static pressure, however, does not affect the flow distribution. Since forward speed reduces the pressure rise required, stalling of the fan blades appears not to be a great danger except at very high forward speeds, or when a deflected exit cascade is fitted. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
The effect of forward speed on the inlet flow distribution and performance of a lifting fan installed in a wing |
en_US |