张靖周
Professor
Education Level:南京航空学院
Degree:Doctoral Degree in Engineering
School/Department:College of Energy and Power Engineering
Discipline:Aerospace Propulsion Theory and Engineering. Engineering Thermophysics
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Affiliation of Author(s):能源与动力学院
Journal:Hangkong Dongli Xuebao
Abstract:Numerical investigation was performed to study the influence of outlet delta-chevrons on the aerodynamic and infrared characteristics of a spherical convergent two-dimensional nozzle in turbofan engine exhaust system. Results showed that the trust coefficient and total pressure recovery coefficient decreased by the outlet shaped-chevrons in relative to the baseline nozzle, especially for the larger base angle of delta-chevron. By comparison, the inner-recessed-chevron mode had a least influence on the aerodynamic performance of exhaust system. However, it resulted in an obvious enhancement both for the exhaust plume and total infrared radiation at the detective angle in the vicinity of ±15°. The outer-extended-chevron mode had a most influence on the aerodynamic performance of exhaust system. The equal-area-chevron mode with a base angle of 30° seemed to be advantageous, as it had a weak influence on the trust coefficient and total pressure recovery coefficient, and also showed certain infrared radiation suppression in the detective angles of -30°-0° and 0°-30°. © 2017, Editorial Department of Journal of Aerospace Power. All right reserved.
ISSN No.:1000-8055
Translation or Not:no
Date of Publication:2017-06-01
Co-author:Zheng, Jiansheng,Shan Yong,Ji, Jingyuan
Correspondence Author:zjz