The calculation of the total and skin friction drags of bodies of revolution at zero incidence

dc.contributor.author	A. D. Young
dc.date.accessioned	2014-10-21T12:03:24Z
dc.date.available	2014-10-21T12:03:24Z
dc.date.issued	1939
dc.identifier.other	ARC/R&M-1874	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1433
dc.description.abstract	By a modification of the method used to calculate the profile drag of aerofoils a method has been developed for calculating the drag of smooth bodies of revolution. This method has been applied to three bodies at zero incidence, the calculations covering a wide range of fineness ratio, Reynolds number and transition position. It is hoped that the results of these calculations will be of particular value to those engaged in performance estimation and in research relating to the cleanness efficiency of aeroplanes.	en_US
dc.language.iso	en	en_US
dc.publisher	H. M. Stationery Office	en_US
dc.relation.ispartofseries	Aeronautical Research Committee Reports & Memoranda	en_US
dc.title	The calculation of the total and skin friction drags of bodies of revolution at zero incidence	en_US
dc.type	Technical Report	en_US