目录
- Special Column:NDT and SHM in Aerospace
- Hypervelocity impact induced shock acoustic emission waves for quantitative damage evaluation using in situ miniaturized piezoelectric sensor network
- Multiphysics simulation method of Lamb wave propagation with piezoelectric transducers under load condition
- A Lamb wave signal reconstruction method for high-resolution damage imaging
- Online condition diagnosis for a two-stage gearbox machinery of an aerospace utilization system using an ensemble multi-fault features indexing approach
- Effect of surface blowing on aerodynamic characteristics of tubercled straight wing
- Effects of blade aspect ratio and taper ratio on hovering performance of cycloidal rotor with large blade pitching amplitude
- Experimental investigation on boiling heat transfer characteristics of Al2O3-water nanofluids in swirl microchannels subjected to an acceleration force
- Development of an efficient contact-friction model for high-fidelity cargo airdrop simulation
- Fault diagnosis based on measurement reconstruction of HPT exit pressure for turbofan engine
- A combined application of micro-vortex generator and boundary layer suction in a high-load compressor cascade
- Measurement of mass diffusion coefficients of O2 in aviation fuel through digital holographic interferometry
- Leading-edge flow separation control over an airfoil using a symmetrical dielectric barrier discharge plasma actuator
- Two freedom linear parameter varying μ synthesis control for flight environment testbed
- Experimental investigation on aero-heating of rudder shaft within laminar/turbulent hypersonic boundary layers
- Analysis of direct operating cost of wide-body passenger aircraft:A parametric study based on Hong Kong
- Multi-disciplinary design optimization with variable complexity modeling for a stratosphere airship
- Exploring mission planning method for a team of carrier aircraft launching
- Fixed-time adaptive model reference sliding mode control for an air-to-ground missile
- Data-driven model-free adaptive attitude control of partially constrained combined spacecraft with external disturbances and input saturation
- Three-dimensional finite-time cooperative guidance for multiple missiles without radial velocity measurements
- Crystal orientation and morphology of α lamellae in wrought titanium alloys:On the role of microstructure evolution in β processing
- Role of the inter-pass cooling rate in recrystallization behaviors of Ni-based superalloy during interrupted hot compression
- Thermoelastohydrodynamic analysis of misaligned bearings with texture on journal surface under high-speed and heavy-load conditions
- Effect of W addition on phase transformation and microstructure of powder metallurgic Ti-22Al-25Nb alloys during quenching and furnace cooling
- Guide for Authors