Quantitative investigation of the evaporation and resistance characteristics of inlet jet precooling
Author:
Affiliation:
1. School of Harbin Engineering University , Harbin , 150001 , P. R. China
2. China Gas Turbine Establishment , Chengdu , 610500 , P. R. China
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2021-0035/pdf
Reference29 articles.
1. Wanng, Z, Wang, Y, Zhang, J, Zhang, B. Overview of the key technologies of combined cycle engine precooling systems and the advanced applications of micro-channel heat transfer. Aero Sci Technol 2014;39:31–9. https://doi.org/10.1016/j.ast.2014.08.008.
2. Chen, F, Ruan, C, Yu, T, Cai, W, Mao, Y, Liu, X. Effects of fuel variation and inlet air temperature on combustion stability in a gas turbine model combustor. Aero Sci Technol 2019;92:126–38. https://doi.org/10.1016/j.ast.2019.05.052.
3. Mehta, U, Bowles, J, Melton, J, Huynh, L, Hagseth, P. Water injection pre-compressor cooling assist space access. Aeronaut J 2015;119:145–71. https://doi.org/10.1017/s0001924000010319.
4. Wilcox, EC, Trout, AM. Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection. NACA; 1951, Report No. NACA TR-1006.
5. Trout, AM. Theoretical turbojet thrust augmentation by evaporation of water during compression as determined by use of a molly diagram. NACA; 1950, Report No. NACA TN-2104.
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