Numerical Analysis and Verification of the Gas Jet from Aircraft Engines Impacting a Jet Blast Deflector

Author:

Gao Fu-DongORCID,Wang De-Xin,Wang Hai-Dong,Jia Ming-Ming

Funder

National Natural Science Foundation of China

Natural Science Foundation of Shandong Province

Publisher

Springer Science and Business Media LLC

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering

Reference26 articles.

1. L P Zhao. Numerical simulation for high temperature and high pressure flow field of aircraft engine jet impingement. Ship Science and Technology, 2016, 38(1): 145–149.

2. K Z Yue, L L Cheng, H Liu, et al. Analysis of jet blast impact of embarked aircraft on deck takeoff zone. Aerospace Science & Technology, 2015, 45(5): 60–66.

3. N A Buchmann, C Atkinson, J Soria. Ultra-high-speed tomographic digital holographic velocimetry in supersonic particle-laden jet flows. Measurement Science & Technology, 2012, 24(2): 827–837.

4. D R Brooks, T Ecker, K T Lowe, et al. Experimental Reynolds stress spectra in hot supersonic round jets. 52nd Aerospace Sciences Meeting, Maryland, USA, January 13–17, 2014: 1227–1245.

5. S Huang, C Wang, J Hu. Research on velocity field of carrier-based aircraft engine’s jet flow. Journal of Harbin Engineering University, 2009, 30(4): 353–356. (in Chinese)

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