CHINESE JOURNAL OF AERONAUTICS
- A review of chatter vibration research in milling
- Impact of reduced frequency on the time lag in pressure distribution over a supercritical airfoil in a pitch-pause-return motion
- Thermal state calculation of chamber in small thrust liquid rocket engine for steady state pulsed mode
- Sliding mode control design for oblique wing aircraft in wing skewing process
- Adaptive optimization methodology based on Kriging modeling and a trust region method
- Aircraft engine fault detection based on grouped convolutional denoising autoencoders
- Predicting lean blow-off of bluffbody stabilized flames based on Damk?hler number
- Numerical study on flow control of ship airwake and rotor airload during helicopter shipboard landing
- Robust decentralized control design for aircraft engines:A fractional type
- Service life prediction of AP/Al/HTPB solid rocket propellant with consideration of softening aging behavior
- Conceptual design and optimization of a tilt-rotor micro air vehicle
- An efficient analytical homogenization technique for mechanical-hygrothermal responses of unidirectional composites with applications to optimization and multiscale analyses
- A model-based prognostics method for fatigue crack growth in fuselage panels
- A data-driven health indicator extraction method for aircraft air conditioning system health monitoring
- A two-step weighted least-squares method for joint estimation of source and sensor locations:A general framework
- Event-triggered adaptive control for attitude tracking of spacecraft
- Efficiency optimized fuel supply strategy of aircraft engine based on air-fuel ratio control
- Effects of splined shaft bending rigidity on cylinder tilt behaviour for high-speed electrohydrostatic actuator pumps
- Identification of the state-space model and payload mass parameter of a flexible space manipulator using a recursive subspace tracking method
- Special Issue call for papers: Emerging Technologies of Unmanned Aerial Vehicles
- Guide for Authors
- Reliable flight performance assessment of multirotor based on interacting multiple model particle filter and health degree