dc.contributor.author |
Aeronautical Research Council |
en_US |
dc.date.accessioned |
2014-10-21T15:53:31Z |
|
dc.date.available |
2014-10-21T15:53:31Z |
|
dc.date.issued |
1945 |
en_US |
dc.identifier.other |
ARC/R&M-2368 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3477 |
|
dc.description.abstract |
The lift distribution along a wing of infinite span with a central jet of higher velocity is calculated by standard methods of aerofoil theory for several values of (jet velocity/stream velocity) and of (jet diameter/wing chord). The lift increment and the induced drag are determined and the application of the results to practical cases is discussed. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Calculation of the effect of slipstream on lift and induced drag. Part 1. Wing of infinite span |
en_US |