Aircraft Engineering And Aerospace Technology

Aircraft Engineering And Aerospace Technology

飞机工程与航空航天技术

  • 4区 中科院分区
  • Q3 JCR分区

高引用文章

文章名称 引用次数
Thermoelastic flexural analysis of FG-CNT doubly curved shell panel 14
Effect of hydrogen addition on exergetic performance of gas turbine engine 10
Aircraft positioning using PPP method in GLONASS system 7
Bending and vibration analysis of skew sandwich plate 7
Simulation-based dynamic model and speed controller design of a small-scale turbojet engine 6
Analysis and optimization of morphing wing aerodynamics 6
Utilization PPP method in aircraft positioning in post-processing mode 6
Flight test of fault-tolerant flight control system using simple adaptive control with PID controller 6
Optimization of machining parameters for abrasive water jet drilling of carbon fiber-reinforced polymer composite material using Taguchi method 6
Evaluation of load-carrying capabilities of friction stir welded, TIG welded and riveted joints of AA2014-T6 aluminium alloy 5
FDM 3D printing method utility assessment in small RC aircraft design 5
LCA of the maintenance of a piston-prop engine 4
Design of parallel adaptive extended Kalman filter for online estimation of noise covariance 4
Overview of thermal arcjet thruster development 4
Comparison of flutter calculation methods based on ground vibration test result 3
New hail impact simulation models on composite laminated wing leading edge 3
Development taxonomy of human risk factors for corporate sustainability in aviation sector 3
Qualitative research on AZ31 magnesium alloy aircraft brackets with a triangular rib produced by a new forging method 3
Neural network based redesign of morphing UAV for simultaneous improvement of roll stability and maximum lift/drag ratio 3
Jet engine degradation prognostic using artificial neural networks 3
Uncertain evaluation of crashworthiness of thin-walled composite structures 3
Proof-of-concept analysis of a supplemental solar power system for aircraft 3
Aircraft neural modeling and parameter estimation using neural partial differentiation 3
An automatic system for a helicopter autopilot performance evaluation 3
Fast high fidelity CFD/CSM fluid structure interaction using RBF mesh morphing and modal superposition method 3
Comparative analysis of numerical methods for the determination of contact pattern of spiral bevel gears 3
Coatings characterization of Ni-based alloy applied by HVOF 3
Aircraft runway excursion features: a multiple correspondence analysis 3
Conflict-resolution algorithms for RPAS in non-segregated airspace 3
Simulation of dynamic stall using direct-forcing immersed boundary method at low Reynolds number 3
UAV application for precision agriculture 3
Developing the pilots' load measuring system 2
A novel improvement of Kriging surrogate model 2
Knock combustion investigation on a two-stroke spark ignition UAV engine burning RP-3 kerosene fuel 2
4D-trajectory time windows: definition and uncertainty management 2
Review of augmented reality in aerospace industry 2
Digital holography interferometry for measuring the mass diffusion coefficients of N-2 in RP-3 and RP-5 jet fuels 2
Unsteady aerodynamic characteristics of a morphing wing 2
Guidance law to control impact time constraining the seeker's field of view? 2
Prioritisation of factors contributing to human error for airworthiness management strategy with ANP 2
Simless GSM positioning for navigation in GPS-denied environments 2
Combustion characteristics of a two-stroke spark ignition UAV engine fuelled with gasoline and kerosene (RP-3) 2
Evaluation of ozone risk under different air-supply mode in aircraft cabins 2
An assessment of flight efficiency based on the point merge system at metroplex airports 2
On-orbit frequency identification of spacecraft based on attitude maneuver data 2
Neural-sliding mode approach-based adaptive estimation, isolation and tolerance of aircraft sensor fault 2
RBF-based mesh morphing approach to perform icing simulations in the aviation sector 2
Multidisciplinary wing design of a light long endurance UAV 2
Rapid trajectory optimization for hypersonic entry using convex optimization and pseudospectral method 2
Properties of direct-quenched aircraft forged component made of ultrahigh-strength steel 300M 2