Author:
QIU Xianghai,XIN Bo,WU Long,MENG Yang,JING Xiaodong
Funder
National Natural Science Foundation of China
Subject
Mechanical Engineering,Aerospace Engineering
Reference38 articles.
1. Optimization of acoustic impedance, geometric structure and operating condition of liners mounted in engine duct;Lu;Chin J Aeronaut,1996
2. Watson WR. A method for determining acoustic-liner admit-tance in ducts with sheared flow in two-cross-sectional direc-tions. Washington, D.C.: NASA; 1985. Report No.: NASA-TP- 601 2518.
3. Watson WR. A new method for determining acoustic-liner admittance in a rectangular duct with grazing flow from experimental data. Washington, D.C.: NASA; 1984. Report No.: NASA-TP-2310.
4. Watson WR, Jones MG. Impedance eduction in ducts with higher-order modes and flow. Reston(VA): AIAA; 2009. Report No.: AIAA-2009-3236.
5. Watson WR, Jones MG. Validation of a new procedure for impedance eduction in flow. Reston(VA): AIAA; 2010. Report No.: AIAA-2010-3764.
Cited by
20 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献