Tests on a working model ram jet in a supersonic wind tunnel

dc.contributor.author	J. R. Singham	en_US
dc.contributor.author	F. W. Pruden	en_US
dc.contributor.author	R. C. Tomlinson	en_US
dc.date.accessioned	2014-10-21T15:50:00Z
dc.date.available	2014-10-21T15:50:00Z
dc.date.issued	1947	en_US
dc.identifier.other	ARC/R&M-2568	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2855
dc.description.abstract	The report describes experiments with a small scale model of a ram jet burning hydrogen in the 1-ft diameter Circular High-speed Tunnel of the National Physical Laboratory adapted to run at a (nominal) Mach number of 1.4. The purpose of the tests was twofold. First, to examine how far it was practicable to test such a small scale model in a wind tunnel. Secondly, to determine to what extent the external drag of a model duct tested hot would differ from that of the same model tested cold. The design, development and construction of a suitable model was carried out by R. P. Probert and the staff of Power Jets (Research and Development) Ltd., (now National Gas Turbine Establishment) whilst the testing was done jointly with the staff of the National Physical Laboratory.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Tests on a working model ram jet in a supersonic wind tunnel	en_US