CHINESE JOURNAL OF AERONAUTICS
- Application of a PCA-DBN-based surrogate model to robust aerodynamic design optimization
- Numerical exploration on the thermal invasion characteristics of two typical gap-cavity structures subjected to hypersonic airflow
- Experimental study on plasma jet deflection and energy extraction with MHD control
- Numerical simulation of compression corner flows at Mach number 9
- Application of improved active disturbance rejection control algorithm in tilt quad rotor
- Investigation on nonlinear lateral-torsional coupled vibration of a rotor system with substantialunbalance
- An adaptive sequential experiment design method for model validation
- A new structural reliability analysis method in presence of mixed uncertainty variables
- NOx emissions of turbofan powered unmanned aerial vehicle for complete flight cycle
- Fluid structure interaction simulation of supersonic parachute inflation by an interface tracking method
- Model-free adaptive optimal design for trajectory tracking control of rocket-powered vehicle
- Hybrid integration method for highly maneuvering radar target detection based on a Markov motion model
- A novel variable structure multi-model approach based on error-ambiguity decomposition
- Multi-block SSD based on small object detection for UAV railway scene surveillance
- A new online modelling method for aircraft engine state space model
- Inverted decoupling and LMI-based controller design for a turboprop engine with actuator dynamics
- Cross-sectional deformation of H96 brass double-ridged rectangular tube in rotary draw bending process with diあerent yield criteria
- Cross-sectional deformation behavior of double-ridged rectangular tube with fillers in diあerent stages of H-typed bending
- Evaluation of thermal eあects on temperaturesensitive operating force of flow servo valve for fuel metering unit
- Corrosion mechanism investigation of TiN/Ti coating and TC4 alloy for aircraft compressor application