CHINESE JOURNAL OF AERONAUTICS
- Efficient multi-response adaptive sampling algorithm for construction of variable- fidelity aerodynamic tables
- Numerical and experimental investigation into hypersonic boundary layer transition induced by roughness elements
- Aerodynamic characteristics of rigid coaxial rotor by wind tunnel test and numerical calculation
- An innovative study on low surface energy micronano coatings with multilevel structures for laminar flow design
- Non-affine parameter dependent LPV model and LMI based adaptive control for turbofan engines
- Vee-tail conceptual design criteria for commercial transport aeroplanes
- Deformation behavior of non-rigid airships in wind tunnel tests
- Remaining useful life prediction for engineering systems under dynamic operational conditions:A semi-Markov decision process-based approach
- Dynamics and de-spin control of massive target by single tethered space tug
- A new dynamic pushback control method for reducing fuel-burn costs:Using predicted taxi-out time
- Adaptive fault-tolerant attitude tracking control for spacecraft with time-varying inertia uncertainties
- Adaptive control for attitude coordination of leader-following rigid spacecraft systems with inertia parameter uncertainties
- Effect of selective laser treatment on initiation of fatigue crack in the main part of an undercarriage drag strut
- Joints of continuous carbon fi ber reinforced lithium aluminosilicate glass ceramics matrix composites to Ti60 alloy brazed using Ti-Zr-Ni-Cu active alloy
- Haptic based teleoperation with master-slave motion mapping and haptic rendering for space exploration
- Design of a tunable mass damper for mitigating vibrations in milling of cylindrical parts
- An improved analytical model of cutting temperature in orthogonal cutting of Ti6Al4V