dc.contributor.author |
W. G. A. Port |
en_US |
dc.contributor.author |
J. C. Morrall |
en_US |
dc.date.accessioned |
2014-10-20T11:05:38Z |
|
dc.date.available |
2014-10-20T11:05:38Z |
|
dc.date.issued |
1967 |
en_US |
dc.identifier.other |
ARC/CP-1105 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1118 |
|
dc.description.abstract |
Flight tests have been made to measure the static and dynamic longitudinal stability, the effect of ground on stability, and the elevator power of the Avro 7078 which has a delta wing sweptback 44.5 degress. A comparison of the results with those of tunnel tests is made. There is a loss of static stability, stick fixed and free, above a lift coefficient of 0.5. Stick force/g at low speed is small particularly at the aft og position, although no great difficulties were encountered due to this or the lack of static stability during the approach and landing. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Current Papers |
en_US |
dc.title |
Low speed flight tests on a tailless delta wing aircraft (Avro 707B) Part 2. longitudinal stability and control |
en_US |