A New Method of Two-dimensional Aerodynamic Design

dc.contributor.author	M. J. Lighthill	en_US
dc.date.accessioned	2014-10-21T15:55:47Z
dc.date.available	2014-10-21T15:55:47Z
dc.date.issued	1945	en_US
dc.identifier.other	ARC/R&M-2112	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3876
dc.description.abstract	The main object of this report is to describe and illustrate a fairly simple exact method by which aerofoils and other surfaces may be constructed to have desired velocity distributions. Its subsidiary interest is as a progress report on shapes already constructed, which are described in the Appendices and Figures, but should not be regarded as the best which, after further development, the method may be capable of producing.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	A New Method of Two-dimensional Aerodynamic Design	en_US