Some Tests on the Spread of Velocity in a Cold Jet Discharging with Excess Pressure from a Sonic Exit into Still Air

dc.contributor.author	J. Seddon	en_US
dc.contributor.author	L. Haverty	en_US
dc.date.accessioned	2014-10-20T11:01:05Z
dc.date.available	2014-10-20T11:01:05Z
dc.date.issued	1956	en_US
dc.identifier.other	ARC/CP-246	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/259
dc.description.abstract	The spread of the half-velocity circle in a jet discharging with excess pressure from a length of parallel pipe into still air has been examined over the range 40 to 200 diameters from the exit. Jet pressure ratios (outside static pressure + jet total pressure) were from 0.479 to 0.042, corresponding to isentropic Mach numbers from 1.08 to 2.72.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Some Tests on the Spread of Velocity in a Cold Jet Discharging with Excess Pressure from a Sonic Exit into Still Air	en_US