CHINESE JOURNAL OF AERONAUTICS
- Determining effects of impact loading on residual strength of fiber-metal laminates with grid-characteristic numerical method
- Morphing wing flaps for large civil aircraft:Evolution of a smart technology across the Clean Sky program
- A hybrid multidimensional Riemann solver to couple self-similar method with MULTV method for complex flows
- Reduction of vibration by periodically stitched sandwich panel
- Aeroelastic prediction and analysis for a transonic fan rotor with the ‘‘hot” blade shape
- Parameter studies and evaluation principles of delamination damage in laminated composites
- Prediction of combined cycle fatigue life of TC11 alloy based on modified nonlinear cumulative damage model
- A review of recent studies on rotating internal cooling for gas turbine blades
- Integrated batteries layout and structural topology optimization for a solar-powered drone
- Polynomial networks based adaptive attitude tracking control for NSVs with input constraints and stochastic noises
- A physics-based framework for online surface roughness assessment for high-pressure turbines
- A novel sparse feature extraction method based on sparse signal via dual-channel self-adaptive TQWT
- Review on bio-inspired flight systems and bionic aerodynamics
- SARISTU:Adaptive Trailing Edge Device(ATED)design process review
- Experimental investigations of a full model with adaptive elasto-flexible membrane wings
- Continuous morphing trailing-edge wing concept based on multi-stable nanomaterial
- A study of morphing aircraft on morphing rules along trajectory
- Performance of wavecatcher intakes at angles of attack and sideslip
- Highly reliable relative navigation for multi-UAV formation flight in urban environments
- Comparative study of two lay-up sequence dispositions for flexible skin design of morphing leading edge