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Modal Analysis of Turbofan Engine Mount Systems

2021 2nd International Conference on Artificial Intelligence and Information Systems, 2021
Zhenxing Zhang   +5 more
openaire   +1 more source

Gross thrust coefficient - Turbofan engines

Journal of Aircraft, 1969
QL = CS(h ± X6 (2) The plenum pneumatic capacitances are based on isentropic compressibility. The pressure rates associated with the inner circular skirt plenums and the inskirt plenum, which lies between the inner circular skirts and the outer peripheral skirt, vary with vehicle motion in pitch and heave where dP/dt = (kP/V)[2Q + A(dZ/dt ± xd8/dt)] (3)
openaire   +1 more source

Numerical modeling on installed performance of turbofan engine with inlet ejector

Aerospace Science and Technology, 2021
Haoying Chen, Changpeng Cai
exaly  

Turbofan engine components

Aircraft Engineering and Aerospace Technology, 1998
openaire   +1 more source

Simulation and technical-economic-environmental optimization of the General Electric GE90 hydrogen turbofan engine

International Journal of Hydrogen Energy, 2021
Abolfazl Ahmadi, Reza Dashti
exaly  

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