Note on the application of Thwaites' numerical method for the design of cambered aerofoils

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