Experience with a steady-state heat-transfer technique in a large wind-tunnel

dc.contributor.author	K. G. Winter	en_US
dc.contributor.author	L. Gaudet	en_US
dc.contributor.author	T. G. Gell	en_US
dc.date.accessioned	2014-10-21T15:51:27Z
dc.date.available	2014-10-21T15:51:27Z
dc.date.issued	1975	en_US
dc.identifier.other	ARC/R&M-3797	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3076
dc.description.abstract	The Report covers the design and development of a plant for pumping a liquid through a model so as to control its temperature, the design and manufacture of the model, and the development of the heat-flow meters used in the model and the means of calibrating them. Sample measurements of heat transfer on the model, a rhombic cone of unit aspect ratio at a Mach number of 2.45, are shown and compared with calculated values.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Experience with a steady-state heat-transfer technique in a large wind-tunnel	en_US