CHINESE JOURNAL OF AERONAUTICS
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CHINESE JOURNAL OF AERONAUTICS
2019年2期
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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 Damköhler 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