1.
					
							The Humidity Effect on the Discharge Coefficient of Sonic Nozzles
						
					
					
						
						
					
					
						湿度对音速喷嘴流出系数影响的研究
					2.
					
							Study on Gas Separation Performance of Vortex Tube with Supersonic Inlet Nozzles
						
					
					
						
						
					
					
						超音速喷嘴涡流管气体分离性能研究
					3.
					
							Structural Design and Assist Gas Flow Analysis of Two-Laser Cutting Supersonic Nozzles
						
					
					
						
						
					
					
						两种激光切割超音速喷嘴结构设计与辅助气体流场分析
					4.
					
							Computer aided design of supersonic jet nozzle for jet mill
						
					
					
						
						
					
					
						超音速气流粉碎机喷嘴计算机辅助设计
					5.
					
							Numerical Simulations of Flows in the Hartmann Resonance Tube and Ultra-Sonic Gas Atomization Nozzle;
						
						
						Hartmann共振管及超音速气体雾化喷嘴流场数值模拟
					6.
					
							The research of supersonic multi-nozzle ejector reverse circulation bit
						
					
					
						
						
					
					
						超音速多喷嘴引射器式反循环钻头研究
					7.
					
							AN EXPERIMENTAL STUDY OF HELIUM INJECTION WITH AN AERODYNAMIC RAMP INJECTOR IN SUPERSONIC FLOW
						
						
						超音速空气流中气动斜坡喷嘴喷射氦的实验研究
					8.
					
							The Laval Nozzle Design and Numerical Simulation of Flow Field for A Supersonic Arc-spraying Gun
						
						
						超音速电弧喷枪的拉瓦尔喷嘴设计及流场的数值模拟
					9.
					
							sonic nozzle flow prover
						
					
					
						
						
					
					
						声速喷嘴流量检定装置
					10.
					
							outlet triangle
						
					
					
						
						
					
					
						喷嘴出口速度三角图
					11.
					
							Research about Nozzle Discharge Speed Distribution for Meltblown Model
						
					
					
						
						
					
					
						熔喷模头喷嘴孔流场速度分布的研究
					12.
					
							ISA 1932 nozzle
						
					
					
						
						
					
					
						ISA 1932喷嘴
					13.
					
							single subsonic jet
						
					
					
						
						
					
					
						单亚音速喷气发动机
					14.
					
							supersonic oxygen-fuel oil burner
						
					
					
						
						
					
					
						超音速氧-燃料油喷燃器
					15.
					
							"supersonic ""rocket"" burner"
						
					
					
						
						
					
					
						"超音速""火箭式""喷燃器"
					16.
					
							At higher speeds, a larger amount of fuel tends to be discharged from the main nozzle.
						
					
					
						
						
					
					
						在较高转速时。主喷嘴会喷出大量的燃油。
					17.
					
							Effect of velocity ratio on combustion process gas-gas injector
						
					
					
						
						
					
					
						速度比对气-气喷嘴燃烧性能的影响
					18.
					
							Fully accelerating abrasive particle velocity to near water-jet velocity is main aid of nozzle design.
						
						
						喷嘴设计的主要任务就是要使从喷嘴喷出的磨料粒子得到充分加速,以便接近水射流的速度.