Heat exchanger integration with an aero-engine bypass duct航空发动机旁路管道中的换热器集成PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERINGIF1.12026-01-011PRE
Cavity Impact on the Base Flow Unsteadiness for a High-Speed Exhaust System腔体对高速排气系统基流脉动性的影响JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASMEIF3.12025-12-010OA
Impact of installation on the performance of a civil turbofan exhaust at wind-milling: A combined experimental and numerical approachAEROSPACE SCIENCE AND TECHNOLOGYIF5.82025-03-010PRE
Design optimisation of non-axisymmetric exhausts for installed civil aero-enginesAEROSPACE SCIENCE AND TECHNOLOGYIF5.82023-11-012OAAI
On the Effects of Optimal Implementation of Variable Rotor Speed and Power Management on Hybrid-Electric RotorcraftJOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASMEIF2.12023-02-231OA
Aerodynamic optimisation of civil aero-engine nacelles by dimensionality reduction and multi-fidelity techniquesINTERNATIONAL JOURNAL OF NUMERICAL METHODS FOR HEAT & FLUID FLOWIF5.12022-09-3016OA
Assessment of hydrogen fuel for rotorcraft applicationsINTERNATIONAL JOURNAL OF HYDROGEN ENERGYIF8.32022-09-018OAAI
Impact of installation on a civil large turbofan exhaust system at idle descent conditionsAEROSPACE SCIENCE AND TECHNOLOGYIF5.82021-12-015OAAI
Preliminary Design of Hybrid-Electric Propulsion Systems for Emerging Urban Air Mobility Rotorcraft ArchitecturesJOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASMEIF2.12021-10-0414OA
Impact of optimized variable rotor speed and active blade twist control on helicopter blade-vortex interaction noise and environmental impactJOURNAL OF FLUIDS AND STRUCTURESIF3.52021-07-018OAAI
Civil turbofan propulsion aerodynamics: Thrust-drag accounting and impact of engine installation positionAEROSPACE SCIENCE AND TECHNOLOGYIF5.82021-04-0134OAAI
Multi-disciplinary optimization of variable rotor speed and active blade twist rotorcraft: Trade-off between noise and emissionsAEROSPACE SCIENCE AND TECHNOLOGYIF5.82020-12-0114OAAI
Design and analysis of non-axisymmetric installed aero-engine exhaust systemsAEROSPACE SCIENCE AND TECHNOLOGYIF5.82020-11-0112OAAI
Parametric design of non-axisymmetric separate-jet aero-engine exhaust systemsAEROSPACE SCIENCE AND TECHNOLOGYIF5.82019-10-0112OAAI
Civil turbofan engine exhaust aerodynamics: Impact of fan exit flow characteristicsAEROSPACE SCIENCE AND TECHNOLOGYIF5.82019-10-0112OAAI
Surrogate models for the prediction of the aerodynamic performance of exhaust systems用于预测排气系统空气动力学性能的替代模型AEROSPACE SCIENCE AND TECHNOLOGYIF5.82019-09-0120OAAI
Integrated methodology for the prediction of helicopter rotor noise at mission levelAEROSPACE SCIENCE AND TECHNOLOGYIF5.82019-06-0134OAAI
Variable rotor speed and active blade twist for civil rotorcraft: Optimum scheduling, mission analysis, and environmental impactAEROSPACE SCIENCE AND TECHNOLOGYIF5.82019-05-0125OAAI
Civil turbofan engine exhaust aerodynamics: Impact of bypass nozzle after-body designAEROSPACE SCIENCE AND TECHNOLOGYIF5.82018-02-0134OAAI
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