Publikationsdatum:
2019-08-27
Beschreibung:
An experimental investigation of the local heat transfer coefficient distribution during gas injection into the supersonic-flow portion of a Laval nozzle is discussed. The controlling dimensionless parameters of the investigated process are presented in terms of a generalized relation for the maximum value of the heat transfer coefficient in the nozzle cross section behind the injection hole. Data on the heat transfer coefficient variation along the nozzle length as a function of gas injection rate are also presented, along with the heat transfer coefficient distribution over a cross section of the nozzle.
Schlagwort(e):
FLUID MECHANICS AND HEAT TRANSFER
Materialart:
NASA-TM-77833
,
NAS 1.15:77833
Format:
application/pdf
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