@inproceedings{a5a049b490ab45eb89b0c9fdc8f537a2,
title = "Areo-engine cycle parametric analysis and installed performance calculation based on aircraft flight mission",
abstract = "The aircraft/engine integration design numerical simulation model was established. The engine design performance specifications were obtained by calculating aircraft lift-drag characteristics, mission analysis, constraint analysis. Combining engine cycle parametric analysis with installation loss computing, the engine performance parameters can be found, which meet the aircraft flight envelope performance requirements. Taking double bypass variable cycle engine as an example to check the model, the results show that the variable cycle engine can meet aircraft's thrust and fuel consumption demands under different operating conditions, and achieve cruise thrust adjustment at the same inlet mass flow to reduce installation losses.",
keywords = "Constraint analysis, Installed performance, Mission analysis, Parametric analysis, Variable cycle engine",
author = "Hong Zhou and Wang, {Zhan Xue} and Zhang, {Xiao Bo}",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.482.277",
language = "英语",
isbn = "9783037859858",
series = "Applied Mechanics and Materials",
pages = "277--281",
booktitle = "Structural Engineering, Vibration and Aerospace Engineering",
note = "2013 International Conference on Structural Engineering, Vibration and Aerospace Engineering, SEVAE 2013 ; Conference date: 23-11-2013 Through 24-11-2013",
}