A highly robust thrust estimation method with dissimilar redundancy framework for gas turbine engine - Concepedia

Concepedia

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A highly robust thrust estimation method with dissimilar redundancy framework for gas turbine engine

31

Citations

37

References

2022

Year

Hang Zhao, Zengbu Liao, Jinxin Liu, Ming Li, Wei Liu, Lei Wang, Zhiping Song

EngineeringAerospace EngineeringIn-cylinder FlowSystems EngineeringInverse ProblemsPropulsionGas Turbine EngineDissimilar Redundancy Framework

References

	Year	Citations

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