CHINESE JOURNAL OF AERONAUTICS
- Review and propositions for the sliding/impact wear behavior in a contact interface
- Multi-faults diagnosis of rolling bearings via adaptive customization of flexible analytical wavelet bases
- Semi-supervised gear fault diagnosis using raw vibration signal based on deep learning
- Rotating machinery fault diagnosis based on convolutional neural network and infrared thermal imaging
- A new bearing fault diagnosis method based on modified convolutional neural networks
- Improving EGT sensing data anomaly detection of aircraft auxiliary power unit
- Reynolds number eあect on compressible cylindrical cavity flow
- Mach reflection in steady supersonic flow considering wedge boundary-layer correction
- Aerodynamic/aeroacoustic variable-fidelity optimization of helicopter rotor based on hierarchical Kriging model
- Delaying stall of morphing wing by periodic trailing-edge deflection
- Optimization and verification of free flight separation similarity law in high-speed wind tunnel
- Non-intrusive reduced-order model for predicting transonic flow with varying geometries
- Consideration on aircraft tire spray when running on wet runways
- Aeroelastic simulation of the first 1.5-stage aeroengine fan at rotating stall
- Experimental study on NOx emission correlation of fuel staged combustion in a LPP combustor at high pressure based on NO-chemiluminescence
- Research on nonlinear model predictive control for turboshaft engines based on double engines torques matching
- Assessment of converting approach to eきcient design of micro-turboprop engines
- Experimental investigations of the spray structure and interactions between sectors of a double-swirl low-emission combustor
- Fatigue life research and experimental verification of superalloy thin-walled structures subjected to thermal-acoustic loads
- Simulator of pyroshock environment and eあect rules of its adjustable parameters
- Multiscale topology optimization using feature-driven method
- An innovative approach for integrated airline network and aircraft family optimization
- Finite-time composite guidance law with input constraint and dynamics compensation
- Switching control of morphing aircraft based on Q-learning
- Direct position determination using single moving rotating linear array: Noncoherent and coherent processing
- Cooperative formation control of multiple aerial vehicles based on guidance route in a complex task environment
- Finite element modelling and experimental investigation of the impact of filling diあerent materials in copper tubes during 3D free bending process
- Five-axis flank milling tool path generation with curvature continuity and smooth cutting force for pockets
- Dynamics modeling and pressure control of composites tape winding system based on LQSMC