dc.contributor.author |
E. Priestley |
en_US |
dc.date.accessioned |
2014-10-21T15:52:34Z |
|
dc.date.available |
2014-10-21T15:52:34Z |
|
dc.date.issued |
1944 |
en_US |
dc.identifier.other |
ARC/R&M-2732 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3280 |
|
dc.description.abstract |
A general method of treatment of stick-fixed static longitudinal stability with propellers is given, distortion and compressibility effects being neglected. Model full-throttle data on some single-engined fighters are analysed for the flaps-up condition to establish a basis of estimation of effect of propeller on stability for this type of design. The general effect of propellers on manceuvre point, more particularly the effect on Hm - Kn, is considered in an appendix. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
A general treatment of static longitudinal stability with propellers, with application to single-engined aircraft |
en_US |