Publication Date:
2019-06-28
Description:
Experimental data on the characteristics of the spray produced by a gas-turbine engine airblast fuel injector are reported. The data acquired include the mass-flux distribution measured by use of a high-resolution spray patternator; the gas-phase velocity field measured by use of a two-component laser Doppler velocimeter, and the liquid droplet size and velocity distributions measured by use of a single-component phase-Doppler anemometer. The data are intended for use in assessments of two-phase flow computational methods as applied to combustor design procedures.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-CR-180864
,
NAS 1.26:180864
Format:
application/pdf
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