Some investigations into the design of wind tunnels with gas turbine jet engine drives

dc.contributor.author	H.J. Higgs	en_US
dc.date.accessioned	2014-10-20T11:00:10Z
dc.date.available	2014-10-20T11:00:10Z
dc.date.issued	1950	en_US
dc.identifier.other	ARC/CP-107	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/120
dc.description.abstract	The basic design of wind tunnels suitable for jet engine drives has been investigated by matching the predicted mass flows and total pressure losses of typical tunnel configurations with the estimated mass flow and total pressure rise characteristics of possible pumping systems. There are three possibilities of jet engine pumping (i) induction pumping (ii) suction pumping and (iii) parallel suction and induction pumping, of which induction pumping is shown to be the most favourable.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Some investigations into the design of wind tunnels with gas turbine jet engine drives	en_US