Numerical Investigation of Droplet Properties of a Liquid Jet in Supersonic Crossflow

Table 6

Operational conditions with different nozzle diameters and airflow Ma.

	No.	(mm)	(kg/s)	/
Gas crossflow	1-7	0.3	0.00119	10~70
	8-14	0.5	0.00475	10~70
	15-21	1	0.01900	10~70
	22-28	2	0.07600	10~70
	29-33	3	0.17100	10~50
	No.	Ma	(pa)	/d
Water jet	33-40	2.1	97.43	10~70
	40-47	3	47.74	10~70
	47-54	4	26.85	10~70