| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A clustering based method to complete frame of discernment
|
YANG, Wenran
|
|
|
36 |
4 |
p. 400-408
|
artikel
|
| 2 |
Aerodynamics of non-slender delta and reverse delta wings: Wing thickness, anhedral angle and cropping ratio
|
KOÇAK, Göktuğ
|
|
|
36 |
4 |
p. 79-91
|
artikel
|
| 3 |
Agent-based effectiveness evaluation method and impact analysis of airborne laser weapon system in cooperation combat
|
SHI, Likuan
|
|
|
36 |
4 |
p. 442-454
|
artikel
|
| 4 |
A partition of unity level set method with moving knot CS-RBFs for optimizing variable stiffness composites
|
LI, Gen
|
|
|
36 |
4 |
p. 565-572
|
artikel
|
| 5 |
A point cloud deep neural network metamodel method for aerodynamic prediction
|
XIONG, Fenfen
|
|
|
36 |
4 |
p. 92-103
|
artikel
|
| 6 |
Bayesian parameter estimation of SST model for shock wave-boundary layer interaction flows with different strengths
|
TANG, Denggao
|
|
|
36 |
4 |
p. 217-236
|
artikel
|
| 7 |
Beam resource scheduling for a VHF-MIMO radar network in low-angle tracking
|
ZHANG, Haowei
|
|
|
36 |
4 |
p. 423-441
|
artikel
|
| 8 |
Behavior pattern mining based on spatiotemporal trajectory multidimensional information fusion
|
JIANG, Qiaowen
|
|
|
36 |
4 |
p. 387-399
|
artikel
|
| 9 |
Collision risk assessment of reduced aircraft separation minima in procedural airspace using advanced communication and navigation
|
CAI, Qing
|
|
|
36 |
4 |
p. 315-337
|
artikel
|
| 10 |
Control-oriented modeling of a high-aspect-ratio flying wing with coupled flight dynamics
|
NIU, Cong
|
|
|
36 |
4 |
p. 409-422
|
artikel
|
| 11 |
Corrosion and aging of organic aviation coatings: A review
|
ZHANG, Tianyu
|
|
|
36 |
4 |
p. 1-35
|
artikel
|
| 12 |
Direct thrust test and asymmetric performance of porous ionic liquid electrospray thruster
|
GUO, Yuntao
|
|
|
36 |
4 |
p. 120-133
|
artikel
|
| 13 |
Editorial Board - Inside Front Cover
|
|
|
|
36 |
4 |
p. IFC
|
artikel
|
| 14 |
Effect of blank quenching on shear spinning forming precision of 2219 aluminum alloy complex thin-walled components
|
LI, Zhixin
|
|
|
36 |
4 |
p. 538-555
|
artikel
|
| 15 |
Effect of mixing section configurations on combustion efficiency of Mg-CO2 Martian ramjet
|
WANG, Xu
|
|
|
36 |
4 |
p. 165-173
|
artikel
|
| 16 |
Experimental investigation of characteristics of instability evolution in a centrifugal compressor
|
ZHANG, Hanzhi
|
|
|
36 |
4 |
p. 174-189
|
artikel
|
| 17 |
High-entropy (La0.2Nd0.2Sm0.2Gd0.2Yb0.2)2(Zr0.75Ce0.25)2O7 thermal barrier coating material with significantly enhanced fracture toughness
|
GUO, Donghui
|
|
|
36 |
4 |
p. 556-564
|
artikel
|
| 18 |
Hot deformation behavior and strain compensation constitutive model of equiaxed fine grain diffusion-welded micro-duplex TC4 titanium alloy
|
LI, Can
|
|
|
36 |
4 |
p. 510-522
|
artikel
|
| 19 |
Identifying and managing risks of AI-driven operations: A case study of automatic speech recognition for improving air traffic safety
|
LIN, Yi
|
|
|
36 |
4 |
p. 366-386
|
artikel
|
| 20 |
Improving profile accuracy and surface quality of blisk by electrochemical machining with a micro inter-electrode gap
|
WANG, Jingtao
|
|
|
36 |
4 |
p. 523-537
|
artikel
|
| 21 |
Integrated passage design based on extended free-form deformation and adjoint optimization
|
LI, Xin
|
|
|
36 |
4 |
p. 148-164
|
artikel
|
| 22 |
Interaction tonal noise generated by contra-rotating open rotors
|
SHU, Wangjian
|
|
|
36 |
4 |
p. 134-147
|
artikel
|
| 23 |
Layout design of thin-walled structures with lattices and stiffeners using multi-material topology optimization
|
LI, Yang
|
|
|
36 |
4 |
p. 496-509
|
artikel
|
| 24 |
Load distribution strategy for multi-lift system with helicopters based on power consumption and robust adaptive game control
|
DUAN, Dengyan
|
|
|
36 |
4 |
p. 268-285
|
artikel
|
| 25 |
Locally generalised multi-agent reinforcement learning for demand and capacity balancing with customised neural networks
|
CHEN, Yutong
|
|
|
36 |
4 |
p. 338-353
|
artikel
|
| 26 |
Minimizing airfoil drag at low angles of attack with DBD-based turbulent drag reduction methods
|
SU, Zhi
|
|
|
36 |
4 |
p. 104-119
|
artikel
|
| 27 |
Multi-objective optimization of different dome reinforcement methods for composite cases
|
ZU, Lei
|
|
|
36 |
4 |
p. 299-314
|
artikel
|
| 28 |
Multi–physical-field characteristics modeling and structure optimization for kW-level ultra-high-speed PM motors with integrated support system
|
GAO, Qixing
|
|
|
36 |
4 |
p. 455-467
|
artikel
|
| 29 |
Nonlinear adaptive flight control system: Performance enhancement and validation
|
FENG, Yue
|
|
|
36 |
4 |
p. 354-365
|
artikel
|
| 30 |
Novel attitude determination method by integration of electronic level meter, INS, and low-cost turntable for level attitude evaluation and calibration of INS
|
YANG, Anlan
|
|
|
36 |
4 |
p. 486-495
|
artikel
|
| 31 |
Pneumatic pressure control based on improved NMPC and its application to aeroengine surge simulation
|
ZHANG, Xinglong
|
|
|
36 |
4 |
p. 468-485
|
artikel
|
| 32 |
Quantification of parametric uncertainty in γ-Reθ model for typical flat plate and airfoil transitional flows
|
SONG, Ziming
|
|
|
36 |
4 |
p. 237-251
|
artikel
|
| 33 |
Recent advances and trends in roll bonding process and bonding model: A review
|
LI, Zixuan
|
|
|
36 |
4 |
p. 36-74
|
artikel
|
| 34 |
Source free unsupervised domain adaptation for electro-mechanical actuator fault diagnosis
|
WANG, Jianyu
|
|
|
36 |
4 |
p. 252-267
|
artikel
|
| 35 |
Substructure evolution in two phases based constitutive model for hot deformation of TC18 in α + β phase region
|
LI, Lian
|
|
|
36 |
4 |
p. 573-588
|
artikel
|
| 36 |
Symmetric Mach reflection configuration with asymmetric unsteady solution
|
BAI, Chenyuan
|
|
|
36 |
4 |
p. 75-78
|
artikel
|
| 37 |
Table of Content
|
|
|
|
36 |
4 |
p. i-ii
|
artikel
|
| 38 |
Time-resolved visualization of coherent structures during supersonic boundary layer transition
|
HE, Lin
|
|
|
36 |
4 |
p. 190-200
|
artikel
|
| 39 |
Unmanned aerial vehicle strike on a flat plate: Tests and numerical simulations
|
LIU, Jun
|
|
|
36 |
4 |
p. 286-298
|
artikel
|
| 40 |
Wind tunnel test of gust load alleviation for a large-scale full aircraft model
|
ZHAO, Dongqiang
|
|
|
36 |
4 |
p. 201-216
|
artikel
|
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