A new design approach of compact high performance airbreathing engine combustors

T. L. Jiang, H. H. Chiu

研究成果: Paper同行評審

2 引文 斯高帕斯(Scopus)

摘要

A design criterion for a high temperature rise, compact burner with minimum length and at fixed fuel, air flowrate6 is established based on the concept of Optimum Size Droplet (OSD) spray. To aid in the design of the optimum spray, the required optimum Sauter Mean Diameter (SMD), the droplet number density are given explicitly In terms of the flowrates and the properties of the sprays at the equivalent injection plan of a combustor. The performance chart representing the relationship between combustion efficiency or temperature rise, the burner length are given as function of the inlet group combustion number of spray. The chart also gives the minimum length and the optimum spray. Based on the simulation of the spray combustion of n—octane, one concludes that approximately 15 to 20% reduction in burner length can be achieved when the ratio of the optimum group combustion number to the non-optimized group combustion number is of the order of 10 or larger, or of the order of 0.1 or smaller. The present approach can be extended to account for the swirling combustor with staging, or in dual annual ∆T combustor of the future generation.

原文English
出版狀態Published - 1987
事件AIAA/ASME/SAE/ASEE 23rd Joint Propulsion Conference, 1987 - San Diego, United States
持續時間: 1987 六月 291987 七月 2

Other

OtherAIAA/ASME/SAE/ASEE 23rd Joint Propulsion Conference, 1987
國家/地區United States
城市San Diego
期間87-06-2987-07-02

All Science Journal Classification (ASJC) codes

  • 機械工業
  • 航空工程
  • 能源工程與電力技術
  • 控制與系統工程
  • 電氣與電子工程

指紋

深入研究「A new design approach of compact high performance airbreathing engine combustors」主題。共同形成了獨特的指紋。

引用此