Research on Optimal Control Method for Turbofan Engine Acceleration Process with Variable Air Bleed Considering High Pressure Turbine Guide Vane Life

Abstract
No abstract available
Funding Information
  • National Natural Science Foundation of China (51906102, 52176009)
  • National Science and Technology Major Project (2017-V-0004-0054, J2019-II-0009-0053, J2019-I-0020-0019)
  • Innovation Centre for Advanced Aviation Power (HKCX2020-02-022, HKCX2020-02-027)
  • Research on the Basic Problem of Intelligent Aero-engine (2017-JCJQ-ZD-047-21)
  • Fundamental Research Funds for the Central Universities (NZ2020002)
  • Natural Science Foundation of Jiangsu Province University (20KJB470017)

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