dc.contributor.author |
A. R. Curtis |
en_US |
dc.date.accessioned |
2014-10-21T15:52:14Z |
|
dc.date.available |
2014-10-21T15:52:14Z |
|
dc.date.issued |
1949 |
en_US |
dc.identifier.other |
ARC/R&M-2665 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3206 |
|
dc.description.abstract |
Some minor developments ill the technique of Thwaites' Numerical Method of Aerofoil Design I are described. In particular, the process of obtaining the camber-line ordinates from the Goldstein Approximation I velocity distribution is discussed in detail; the relevant tables of constants are given. An opportunity is taken to include a complete set of 20-point tables of Conjugation Factors needed in any actual application of the Numerical Methods. The theory underlying these tables is given by Watson in R. & M. 2716. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Note on the application of Thwaites' numerical method for the design of cambered aerofoils |
en_US |