Areo-Engine Cycle Parametric Analysis and Installed Performance Calculation Based on Aircraft Flight Mission

Hong Zhou; Zhan Xue Wang; Xiao Bo Zhang

doi:10.4028/www.scientific.net/AMM.482.277

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 482Areo-Engine Cycle Parametric Analysis and...

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 aircrafts thrust and fuel consumption demands under different operating conditions, and achieve cruise thrust adjustment at the same inlet mass flow to reduce installation losses.

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Periodical:

Applied Mechanics and Materials (Volume 482)

Pages:

277-281

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.482.277

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Online since:

December 2013

Authors:

Hong Zhou, Zhan Xue Wang*, Xiao Bo Zhang

Keywords:

Constraint Analysis, Installed Performance, Mission Analysis, Parametric Analysis, Variable Cycle Engine

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* - Corresponding Author

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