dc.contributor.author |
G. Z. Harris |
en_US |
dc.date.accessioned |
2014-10-21T15:56:31Z |
|
dc.date.available |
2014-10-21T15:56:31Z |
|
dc.date.issued |
1965 |
en_US |
dc.identifier.other |
ARC/R&M-3453 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4034 |
|
dc.description.abstract |
A numerical method of solving the integral equation connecting the lift and downwash on a wing oscillating harmonically in a supersonic flow of any Mach number is described. The integral equation is replaced by a matrix equation connecting the values of the lift and downwash at sets of points on the wing, and the generalised aerodynamic forces acting on the wing are found simply as a matrix product. Comparisons are made between aerodynamic derivatives calculated by this method, and theoretical and experimental derivatives from other sources. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory |
en_US |