dc.contributor.author |
W. J. G. Pinsker |
en_US |
dc.date.accessioned |
2014-10-21T15:50:51Z |
|
dc.date.available |
2014-10-21T15:50:51Z |
|
dc.date.issued |
1972 |
en_US |
dc.identifier.other |
ARC/R&M-3730 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3007 |
|
dc.description.abstract |
Some of the more important practical implications to pilot's control, flight test analysis, and stability augmentor performance of classical longitudinal stability theory are discussed. The distinction between turns and pull-ups is re-emphasized and the differences quantified. Angular momentum of the engines is shown to make a contribution which can be significant with S.T.O.L. aircraft, being destabilizing in turns in one direction but stabilizing in the opposite direction. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Some observations on manoeuvre stability and longitudinal control |
en_US |