nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A computational-geometry-based 3-dimensional guidance law to control impact time and angle
|
Yan, Xinghui |
|
|
98 |
C |
p. |
artikel |
2 |
Active fault-tolerant attitude tracking control with adaptive gain for spacecrafts
|
Hu, Hui |
|
|
98 |
C |
p. |
artikel |
3 |
A globally fixed-time solution of distributed formation control for multiple hypersonic gliding vehicles
|
Zhang, Yao |
|
|
98 |
C |
p. |
artikel |
4 |
A high-order accurate unstructured spectral difference lattice Boltzmann method for computing inviscid and viscous compressible flows
|
Hejranfar, Kazem |
|
|
98 |
C |
p. |
artikel |
5 |
Airfoil gust load alleviation by circulation control
|
Li, Yonghong |
|
|
98 |
C |
p. |
artikel |
6 |
Alternative approaches for UAV dead reckoning based on the immunity paradigm
|
Alnuaimi, Mohanad |
|
|
98 |
C |
p. |
artikel |
7 |
Analysis of flow resistance and combustion characteristics in the combined application of step and strut
|
Shilong, Zhao |
|
|
98 |
C |
p. |
artikel |
8 |
Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement
|
Wang, Youyin |
|
|
98 |
C |
p. |
artikel |
9 |
A new approach of endwall recirculation in axial compressors
|
Khaleghi, Hossein |
|
|
98 |
C |
p. |
artikel |
10 |
Application of modified couple-stress theory to stability and free vibration analysis of single and multi-layered graphene sheets
|
Shafiei, Zahra |
|
|
98 |
C |
p. |
artikel |
11 |
A trajectory design method for coupling aircraft radar cross-section characteristics
|
Xu, Qiangqiang |
|
|
98 |
C |
p. |
artikel |
12 |
Automatic modeling of aircraft external geometries for preliminary design workflows
|
De Marco, Agostino |
|
|
98 |
C |
p. |
artikel |
13 |
Automatic stability control using tip air injection in a multi-stage axial flow compressor
|
Li, Jichao |
|
|
98 |
C |
p. |
artikel |
14 |
Bionic design for the aerodynamic shape of a stratospheric airship
|
Yang, Yueneng |
|
|
98 |
C |
p. |
artikel |
15 |
Breakup criterion for droplets exposed to the unsteady flow generated by an incoming aerodynamic surface
|
Lopez-Gavilan, P. |
|
|
98 |
C |
p. |
artikel |
16 |
Combustion characterization of a CH4/O2 rapid mixed swirl torch igniter for hybrid rocket motors
|
Wu, Yi |
|
|
98 |
C |
p. |
artikel |
17 |
Contact dynamics and relative motion estimation of non-cooperative target with unilateral contact constraint
|
She, Yuchen |
|
|
98 |
C |
p. |
artikel |
18 |
Deformation behaviors and energy absorption of auxetic lattice cylindrical structures under axial crushing load
|
Guo, Yongguang |
|
|
98 |
C |
p. |
artikel |
19 |
Design and aerodynamic performance analysis of a variable-sweep-wing morphing waverider
|
Dai, Pei |
|
|
98 |
C |
p. |
artikel |
20 |
Development of highly electrically conductive composites for aeronautical applications utilizing bi-functional composite interleaves
|
Hu, Dongyuan |
|
|
98 |
C |
p. |
artikel |
21 |
Development of k-R turbulence model for wall-bounded flows
|
Zhang, Yang |
|
|
98 |
C |
p. |
artikel |
22 |
Drag bookkeeping on an aircraft with riblets and NLF control
|
Mele, Benedetto |
|
|
98 |
C |
p. |
artikel |
23 |
Dynamic buckling optimization of laminated aircraft conical shells with hybrid nanocomposite martial
|
Kolahchi, Reza |
|
|
98 |
C |
p. |
artikel |
24 |
Dynamic mode decomposition analysis of flow characteristics of an airfoil with leading edge protuberances
|
Zhao, Ming |
|
|
98 |
C |
p. |
artikel |
25 |
Editorial Board
|
|
|
|
98 |
C |
p. |
artikel |
26 |
Effect of blended blade tip and winglet on aerodynamic and aeroacoustic performances of a diagonal fan
|
Zhang, Chun |
|
|
98 |
C |
p. |
artikel |
27 |
Effect of turbine rotor disc vibration on hot gas ingestion and rotor-stator cavity flow
|
Jia, Xingyun |
|
|
98 |
C |
p. |
artikel |
28 |
Elastostatic assessment of several mixed/displacement-based laminated plate theories, differently accounting for transverse normal deformability
|
Icardi, Ugo |
|
|
98 |
C |
p. |
artikel |
29 |
Evaluation of modelling parameters for computing flow-induced noise in a small high-speed centrifugal compressor
|
Sharma, S. |
|
|
98 |
C |
p. |
artikel |
30 |
Experimental study on flame/flow dynamics in a multi-nozzle gas turbine model combustor under thermo-acoustically unstable condition with different swirler configurations
|
Ruan, Can |
|
|
98 |
C |
p. |
artikel |
31 |
Experimental study on the flow field distribution characteristics of an open-end swirl injector under ambient pressure
|
He, Xiujie |
|
|
98 |
C |
p. |
artikel |
32 |
Fuzzy adaptive nonlinear information fusion model predictive attitude control of unmanned rotorcrafts
|
Xu, Qingzheng |
|
|
98 |
C |
p. |
artikel |
33 |
Fuzzy controller design of micro-unmanned helicopter relying on improved genetic optimization algorithm
|
Hu, Yanpeng |
|
|
98 |
C |
p. |
artikel |
34 |
Glide guidance for reusable launch vehicles using analytical dynamics
|
Zhou, Hongyu |
|
|
98 |
C |
p. |
artikel |
35 |
Helicopter wire strike protection and prevention devices: Review, challenges, and recommendations
|
Chandrasekaran, Ruthvik |
|
|
98 |
C |
p. |
artikel |
36 |
Hypersonic boost–glide vehicle strapdown inertial navigation system / global positioning system algorithm in a launch-centered earth-fixed frame
|
Chen, Kai |
|
|
98 |
C |
p. |
artikel |
37 |
Infinite horizon model predictive control tracking application to helicopters
|
Greer, William B. |
|
|
98 |
C |
p. |
artikel |
38 |
Influence of the inlet distortion on fan stall margin at different rotational speeds
|
Zhang, Wenqiang |
|
|
98 |
C |
p. |
artikel |
39 |
Integrated guidance and control system design for laser beam riding missiles with relative position constraints
|
Peng, Qian |
|
|
98 |
C |
p. |
artikel |
40 |
Investigation on effects of shock wave on vortical wake flow in a turbine nozzle cascade
|
Zhao, Ben |
|
|
98 |
C |
p. |
artikel |
41 |
Low speed lateral-directional aerodynamic and static stability analysis of a hypersonic waverider
|
Bykerk, Tamas |
|
|
98 |
C |
p. |
artikel |
42 |
Mechanisms of lobed jet mixing: About circularly alternating-lobe mixers
|
Sheng, Zhi-qiang |
|
|
98 |
C |
p. |
artikel |
43 |
Method for eliminating aerodynamic lift vibration of rigid rotor helicopters based on the novel sine-trim model
|
Lyu, Wei-Liang |
|
|
98 |
C |
p. |
artikel |
44 |
Noise reduction of a Counter Rotating Open Rotor through a locked blade row
|
Smith, D.A. |
|
|
98 |
C |
p. |
artikel |
45 |
Nonlinear resonance of FG multilayer beam-type nanocomposites: Effects of graphene nanoplatelet-reinforcement and geometric imperfection
|
Liu, Hu |
|
|
98 |
C |
p. |
artikel |
46 |
Nonsingular terminal sliding mode control for a quadrotor UAV with a total rotor failure
|
Hou, Zhiwei |
|
|
98 |
C |
p. |
artikel |
47 |
Numerical analysis on combustion instabilities in end-burning-grain solid rocket motors utilizing pressure-coupled response functions
|
Ji, Shixiang |
|
|
98 |
C |
p. |
artikel |
48 |
Numerical analysis on the disintegration of gas-liquid interface in two-phase shear-layer flows
|
Xiang, Gaoming |
|
|
98 |
C |
p. |
artikel |
49 |
Numerical investigation of the effects of plasma actuator on separated laminar flows past an incident plate under ground effect
|
Foshat, Saeed |
|
|
98 |
C |
p. |
artikel |
50 |
Numerical investigation of the error caused by the aero-optical environment around an in-flight wing in optically measuring the wing deformation
|
Liu, Yan |
|
|
98 |
C |
p. |
artikel |
51 |
Numerical simulation of turbulent thermal boundary layer and generation mechanisms of hairpin vortex
|
Li, Heng |
|
|
98 |
C |
p. |
artikel |
52 |
Online trajectory optimization for power system fault of launch vehicles via convex programming
|
Li, Yuan |
|
|
98 |
C |
p. |
artikel |
53 |
On the low-velocity impact responses of auxetic double arrowed honeycomb
|
Gao, Qiang |
|
|
98 |
C |
p. |
artikel |
54 |
On the mode transition of a double bypass variable cycle compression system
|
Liu, Baojie |
|
|
98 |
C |
p. |
artikel |
55 |
Optimal control of turbulent premixed combustion instability with annular micropore air jets
|
Zhou, Hao |
|
|
98 |
C |
p. |
artikel |
56 |
Over-expanded separation transitions of single expansion ramp nozzle in the accelerating and decelerating processes
|
Yu, Yang |
|
|
98 |
C |
p. |
artikel |
57 |
Performance analysis of rotatable energy system of high-altitude airships in real wind field
|
Zhu, Weiyu |
|
|
98 |
C |
p. |
artikel |
58 |
Performance comparison of representative model-based fault reconstruction algorithms for aircraft sensor fault detection and diagnosis
|
He, Qizhi |
|
|
98 |
C |
p. |
artikel |
59 |
Practical finite time adaptive robust flight control system for quad-copter UAVs
|
Eliker, Karam |
|
|
98 |
C |
p. |
artikel |
60 |
Probabilistic stability analysis of functionally graded graphene reinforced porous beams
|
Gao, Kang |
|
|
98 |
C |
p. |
artikel |
61 |
Quaternion based linear time-varying model predictive attitude control for satellites with two reaction wheels
|
Golzari, Ali |
|
|
98 |
C |
p. |
artikel |
62 |
Reinforcement learning based two-level control framework of UAV swarm for cooperative persistent surveillance in an unknown urban area
|
Liu, Yuxuan |
|
|
98 |
C |
p. |
artikel |
63 |
Reinforcement learning in dual-arm trajectory planning for a free-floating space robot
|
Wu, Yun-Hua |
|
|
98 |
C |
p. |
artikel |
64 |
Robust inertial navigation system/ultra wide band integrated indoor quadrotor localization employing adaptive interacting multiple model-unbiased finite impulse response/Kalman filter estimator
|
Xu, Yuan |
|
|
98 |
C |
p. |
artikel |
65 |
Scaling laws and similarity models for the preliminary design of multirotor drones
|
Budinger, M. |
|
|
98 |
C |
p. |
artikel |
66 |
Sensitivity of ice accretion and aerodynamic performance degradation to critical physical and modeling parameters affecting airfoil icing
|
Prince Raj, L. |
|
|
98 |
C |
p. |
artikel |
67 |
Simulations of airborne collisions between drones and an aircraft windshield
|
Lu, Xiaohua |
|
|
98 |
C |
p. |
artikel |
68 |
Structural design and experimental verification of a novel split aileron wing
|
Zhao, Anmin |
|
|
98 |
C |
p. |
artikel |
69 |
Study on the combined effect of various injection conditions on the drag reduction by a counter-flow jet in supersonic flow
|
Kim, Yongchan |
|
|
98 |
C |
p. |
artikel |
70 |
The influence of the wedge shock generator on the vortex structure within the trapezoidal cavity at supersonic flow
|
Li, Zhixiong |
|
|
98 |
C |
p. |
artikel |
71 |
Theoretical study on energy performance of a stratospheric solar aircraft with optimum Λ-shaped rotatable wing
|
Wu, Mingjian |
|
|
98 |
C |
p. |
artikel |
72 |
Thermal protection of a hypersonic vehicle by modulating stagnation-point heat flux
|
Han, Quan |
|
|
98 |
C |
p. |
artikel |
73 |
Tip leakage flow and aeroacoustics analysis of a low-speed axial fan
|
Luo, Bo |
|
|
98 |
C |
p. |
artikel |
74 |
Trajectory optimization for parafoil delivery system considering complicated dynamic constraints in high-order model
|
Sun, Hao |
|
|
98 |
C |
p. |
artikel |
75 |
Transient analysis of upstream wake inside turbine blade passage with purge flow
|
Sushanlal, Babu |
|
|
98 |
C |
p. |
artikel |
76 |
Transitional boundary layer study over an airfoil in combined pitch-plunge motions
|
Akhlaghi, Hassan |
|
|
98 |
C |
p. |
artikel |
77 |
Vibration characteristics of rotating pretwisted composite tapered blade with graphene coating layers
|
Zhang, W. |
|
|
98 |
C |
p. |
artikel |
78 |
Wind estimation using quadcopter motion: A machine learning approach
|
Allison, Sam |
|
|
98 |
C |
p. |
artikel |