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- [1] CONTROL OF THE AERO-ENGINE NACELLE INTAKE FLOW SEPARATION CAUSED BY CROSSWIND CONDITION USING PLASMA ACTUATION PROCEEDINGS OF THE ASME TURBO EXPO 2020: TURBOMACHINERY TECHNICAL CONFERENCE AND EXHIBITION, VOL 2D, 2020,
- [2] Numerical investigation of nozzle flow separation control using plasma actuation Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2021, 42 (07):
- [5] Flow and separation characteristics of pressurized centrifugal separator for aero-engine Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2024, 45 (02):
- [8] Study on Plasma Flow Control of Nacelle Flow Separation Under Crosswind Conditions Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2021, 42 (01): : 64 - 72
- [10] The three-dimensional measurement research of aero-engine blade based on structured light INTERNATIONAL SYMPOSIUM ON PHOTOELECTRONIC DETECTION AND IMAGING 2011: ADVANCES IN IMAGING DETECTORS AND APPLICATIONS, 2011, 8194