Acta Aeronautica et Astronautica Sinica ›› 2026, Vol. 47 ›› Issue (8): 132554.doi: 10.7527/S1000-6893.2025.32554
• Fluid Mechanics and Flight Mechanics •
Shiqi WANG1(
), Bo FAN2, Zhixuan HAN2, Neng WAN1, Liang MA2, Zhigang JIA1, Quan WEN1
Received:2025-07-11
Revised:2025-08-20
Accepted:2025-11-19
Online:2025-12-09
Published:2025-12-08
Contact:
Shiqi WANG
E-mail:wangsq6@126.com
Supported by:CLC Number:
Shiqi WANG, Bo FAN, Zhixuan HAN, Neng WAN, Liang MA, Zhigang JIA, Quan WEN. Comparative analysis on spray characteristics of three pressure nozzles in high-speed crossflow[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(8): 132554.
Table 1
Experimental specimen parameters and experimental conditions
| 实验件 | 孔径/mm | 流量数/(kg·h-1· MPa-0.5) | 来流 风速ua/ (m·s-1) | 燃油 压降/MPa | 燃油流量 m/(kg·h-1) | 燃油喷射 特征速度 uj/(m·s-1) | 液气动 量比q | 横流特征尺寸/mm | 韦伯数 We |
|---|---|---|---|---|---|---|---|---|---|
| 直射式喷嘴 | 0.4 (几何孔径) | 11.4 | 142 | 1.5 | 13.96 | 39.6 | 56 | 0.40 | 314 |
| 2.0 | 16.12 | 45.7 | 82 | ||||||
| 3.0 | 19.75 | 57.4 | 121 | ||||||
| 离心式喷嘴 | 0.4 (流量等效孔径) | 11.3 | 142 | 1.5 | 13.84 | ||||
| 2.0 | 15.98 | ||||||||
| 3.0 | 19.57 | ||||||||
| 自激扫掠喷嘴 | 0.4 (几何等效孔径) | 13.3 | 142 | 1.5 | 16.80 | 32.1 | 40 | 0.56 | 443 |
| 2.0 | 19.04 | 37.1 | 52 | ||||||
| 3.0 | 22.91 | 45.5 | 75 | ||||||
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