| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Acoustic and radar integrated stealth design for ducted tail rotor based on comprehensive optimization method
|
Zhou, Zeyang
|
|
2019
|
92 |
C |
p. 244-257
|
artikel
|
| 2 |
AC plasma retarded flame spread over thin solid fuels in a simulated microgravity environment
|
Wang, Zihan
|
|
2019
|
92 |
C |
p. 139-147
|
artikel
|
| 3 |
Adaptive constrained backstepping controller with prescribed performance methodology for carrier-based UAV
|
Zhang, Yang
|
|
2019
|
92 |
C |
p. 55-65
|
artikel
|
| 4 |
Adaptive super-twisting sliding mode control of variable sweep morphing aircraft
|
Yan, Binbin
|
|
2019
|
92 |
C |
p. 198-210
|
artikel
|
| 5 |
Aerodynamic optimal design for a glider with the supersonic airfoil based on the hybrid MIGA-SA method
|
Wang, F.P.
|
|
2019
|
92 |
C |
p. 224-231
|
artikel
|
| 6 |
Aerothermodynamic analysis for deformed membrane of inflatable aeroshell in orbital reentry mission
|
Takahashi, Yusuke
|
|
2019
|
92 |
C |
p. 858-868
|
artikel
|
| 7 |
A gradient-based aero-stealth optimization design method for flying wing aircraft
|
Li, Ming
|
|
2019
|
92 |
C |
p. 156-169
|
artikel
|
| 8 |
A method of 3D path planning for solar-powered UAV with fixed target and solar tracking
|
Huang, Yu
|
|
2019
|
92 |
C |
p. 831-838
|
artikel
|
| 9 |
A multivariable adaptive control scheme for automatic carrier landing of UAV
|
Zhen, Ziyang
|
|
2019
|
92 |
C |
p. 714-721
|
artikel
|
| 10 |
Analytical frequency response solution for composite plates embedding viscoelastic layers
|
Alaimo, A.
|
|
2019
|
92 |
C |
p. 429-445
|
artikel
|
| 11 |
An efficient method combining adaptive Kriging and fuzzy simulation for estimating failure credibility
|
Ling, Chunyan
|
|
2019
|
92 |
C |
p. 620-634
|
artikel
|
| 12 |
A nonlinear analytical formula for forced vibration analysis of the hard-coating cylindrical shell based on the strain energy density principle
|
Zhang, Yue
|
|
2019
|
92 |
C |
p. 326-336
|
artikel
|
| 13 |
A novel three-axis attitude stabilization method using in-plane internal mass-shifting
|
He, Liang
|
|
2019
|
92 |
C |
p. 489-500
|
artikel
|
| 14 |
Application of deep learning based multi-fidelity surrogate model to robust aerodynamic design optimization
|
Tao, Jun
|
|
2019
|
92 |
C |
p. 722-737
|
artikel
|
| 15 |
Appointed-time fault-tolerant attitude tracking control of spacecraft with double-level guaranteed performance bounds
|
Liu, Mingmin
|
|
2019
|
92 |
C |
p. 337-346
|
artikel
|
| 16 |
A satellite mission concept for high drag environments
|
McCreary, Lance
|
|
2019
|
92 |
C |
p. 972-989
|
artikel
|
| 17 |
Aspects of the design, evaluation and accuracy of airborne sensor clusters using time-difference of arrival
|
Marcus, Carina
|
|
2019
|
92 |
C |
p. 892-900
|
artikel
|
| 18 |
A velocity-free adaptive RISE-based trajectory tracking approach for quadrotors with desired model compensation
|
Wang, Hongliang
|
|
2019
|
92 |
C |
p. 551-562
|
artikel
|
| 19 |
Axially functionally graded beams and panels in supersonic airflow and their excellent capability for passive flutter suppression
|
Song, Zhiguang
|
|
2019
|
92 |
C |
p. 668-675
|
artikel
|
| 20 |
Biomimetic skeleton structure of morphing nose cone for aerospace vehicle inspired by variable geometry mechanism of honeybee abdomen
|
Zhang, Yuling
|
|
2019
|
92 |
C |
p. 405-416
|
artikel
|
| 21 |
Combustion characteristics of a novel design of solid-fuel ramjet motor with swirl flow
|
Musa, Omer
|
|
2019
|
92 |
C |
p. 750-765
|
artikel
|
| 22 |
Computational investigations into heat transfer over a double wedge in hypersonic flows
|
Expósito, Diego
|
|
2019
|
92 |
C |
p. 839-846
|
artikel
|
| 23 |
Data-driven constraint approach to ensure low-speed performance in transonic aerodynamic shape optimization
|
Li, Jichao
|
|
2019
|
92 |
C |
p. 536-550
|
artikel
|
| 24 |
Design and implementation of MPC for turbofan engine control system
|
Montazeri-Gh, Morteza
|
|
2019
|
92 |
C |
p. 99-113
|
artikel
|
| 25 |
Editorial Board
|
|
|
2019
|
92 |
C |
p. ii
|
artikel
|
| 26 |
Effect of disk angle-of-attack on aerodynamic performance of small propellers
|
Serrano, David
|
|
2019
|
92 |
C |
p. 901-914
|
artikel
|
| 27 |
Effect of rear-fuselage design on the aerodynamics of a helicopter at side-slip angle
|
Gingras, Drew
|
|
2019
|
92 |
C |
p. 192-197
|
artikel
|
| 28 |
Effects of fuel variation and inlet air temperature on combustion stability in a gas turbine model combustor
|
Chen, Feier
|
|
2019
|
92 |
C |
p. 126-138
|
artikel
|
| 29 |
Experimental and numerical investigations of trailing edge injection in a transonic turbine cascade
|
Gao, Jie
|
|
2019
|
92 |
C |
p. 258-268
|
artikel
|
| 30 |
Experimental demonstration of an end-burning swirling flow hybrid rocket engine
|
Lestrade, J.-Y.
|
|
2019
|
92 |
C |
p. 1-8
|
artikel
|
| 31 |
Fast task allocation for heterogeneous unmanned aerial vehicles through reinforcement learning
|
Zhao, Xinyi
|
|
2019
|
92 |
C |
p. 588-594
|
artikel
|
| 32 |
Flatness-based finite-time leader–follower formation control of multiple quadrotors with external disturbances
|
Ai, Xiaolin
|
|
2019
|
92 |
C |
p. 20-33
|
artikel
|
| 33 |
Free vibration analysis of variable angle-tow composite wing structures
|
Viglietti, A.
|
|
2019
|
92 |
C |
p. 114-125
|
artikel
|
| 34 |
Frozen orbit design and maintenance with an application to small body exploration
|
Li, Xiangyu
|
|
2019
|
92 |
C |
p. 170-180
|
artikel
|
| 35 |
Fuel injection location studies on pylon-cavity aided jet in supersonic crossflow
|
Oamjee, Aryadutt
|
|
2019
|
92 |
C |
p. 869-880
|
artikel
|
| 36 |
Geometry effect on the airfoil-gust interaction noise in transonic flows
|
Zhong, Siyang
|
|
2019
|
92 |
C |
p. 181-191
|
artikel
|
| 37 |
Global smooth sliding mode controller for flexible air-breathing hypersonic vehicle with actuator faults
|
Ding, Yibo
|
|
2019
|
92 |
C |
p. 563-578
|
artikel
|
| 38 |
High-precision control method for the satellite with large rotating components
|
Wang, Feng
|
|
2019
|
92 |
C |
p. 91-98
|
artikel
|
| 39 |
Implementation and verification of gust modeling in an open-source flow solver
|
Ghoreyshi, Mehdi
|
|
2019
|
92 |
C |
p. 777-789
|
artikel
|
| 40 |
Implicit high-order gas kinetic scheme for turbulence simulation
|
Cao, Guiyu
|
|
2019
|
92 |
C |
p. 958-971
|
artikel
|
| 41 |
Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures
|
Fang, Yishen
|
|
2019
|
92 |
C |
p. 676-684
|
artikel
|
| 42 |
Inverse design methodology on a single expansion ramp nozzle for scramjets
|
Yu, Kaikai
|
|
2019
|
92 |
C |
p. 9-19
|
artikel
|
| 43 |
Investigation for electro-thermo-mechanical vibration of nanocomposite cylindrical shells with an internal fluid flow
|
Ninh, Dinh Gia
|
|
2019
|
92 |
C |
p. 501-519
|
artikel
|
| 44 |
Investigation of pitch damping derivatives for the Standard Dynamic Model at high angles of attack using neural network
|
Tatar, Massoud
|
|
2019
|
92 |
C |
p. 685-695
|
artikel
|
| 45 |
Magnetic sail-based displaced non-Keplerian orbits
|
Bassetto, Marco
|
|
2019
|
92 |
C |
p. 363-372
|
artikel
|
| 46 |
Modeling method of coating thickness random mistuning and its effect on the forced response of coated blisks
|
Yan, Xianfei
|
|
2019
|
92 |
C |
p. 478-488
|
artikel
|
| 47 |
Mode multigrid - A novel convergence acceleration method
|
Liu, Yilang
|
|
2019
|
92 |
C |
p. 605-619
|
artikel
|
| 48 |
Morphing control of a new bionic morphing UAV with deep reinforcement learning
|
Xu, Dan
|
|
2019
|
92 |
C |
p. 232-243
|
artikel
|
| 49 |
Multidisciplinary design optimization of aircraft wing using commercial software integration
|
Benaouali, Abdelkader
|
|
2019
|
92 |
C |
p. 766-776
|
artikel
|
| 50 |
Multidisciplinary design optimization of long-range slender guided rockets considering aeroelasticity and subsidiary loads
|
Wei, Zhao
|
|
2019
|
92 |
C |
p. 790-805
|
artikel
|
| 51 |
Multi-failure probabilistic design for turbine bladed disks using neural network regression with distributed collaborative strategy
|
Song, Lu-Kai
|
|
2019
|
92 |
C |
p. 464-477
|
artikel
|
| 52 |
Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise
|
Cilden-Guler, Demet
|
|
2019
|
92 |
C |
p. 66-76
|
artikel
|
| 53 |
Nonlinear material and geometric analysis of thick functionally graded plates with nonlinear strain hardening using nonlinear finite element method
|
Zafarmand, Hassan
|
|
2019
|
92 |
C |
p. 930-944
|
artikel
|
| 54 |
Nonlinear reentry guidance law guaranteeing convergence before attainment of desired line-of-sight range
|
Jiang, Chunwang
|
|
2019
|
92 |
C |
p. 579-587
|
artikel
|
| 55 |
Non-modal stability analysis of low-Re separated flow around a NACA 4415 airfoil in ground effect
|
He, Wei
|
|
2019
|
92 |
C |
p. 269-279
|
artikel
|
| 56 |
Non-uniform stator loss reduction design strategy in a transonic axial-flow compressor stage under inflow distortion
|
Lu, Hanan
|
|
2019
|
92 |
C |
p. 347-362
|
artikel
|
| 57 |
Numerical and experimental investigation on hybrid rocket motor with two-hole segmented rotation grain
|
Tian, Hui
|
|
2019
|
92 |
C |
p. 820-830
|
artikel
|
| 58 |
Numerical investigation on detonation initiation using toroidal shock wave focusing
|
Chen, Xiang
|
|
2019
|
92 |
C |
p. 300-313
|
artikel
|
| 59 |
Numerical investigation on flow control effects of dynamic hump for turbine cascade at different Reynolds number and hump oscillating frequency
|
Yang, Rongfei
|
|
2019
|
92 |
C |
p. 280-288
|
artikel
|
| 60 |
Numerical predictions of low Reynolds number compressible aerodynamics
|
Désert, T.
|
|
2019
|
92 |
C |
p. 211-223
|
artikel
|
| 61 |
Observer-based fault tolerant control and experimental verification for rigid spacecraft
|
Hu, Qinglei
|
|
2019
|
92 |
C |
p. 373-386
|
artikel
|
| 62 |
Observer-based linear parameter varying control design with unmeasurable varying parameters under sensor faults for quad-tilt rotor unmanned aerial vehicle
|
Liu, Zhong
|
|
2019
|
92 |
C |
p. 696-713
|
artikel
|
| 63 |
Performance analysis of dual-duct rotating detonation aero-turbine engine
|
Ji, Zifei
|
|
2019
|
92 |
C |
p. 806-819
|
artikel
|
| 64 |
Preliminary design of multirotor UAVs with tilted-rotors for improved disturbance rejection capability
|
Chen, Z.J.
|
|
2019
|
92 |
C |
p. 635-643
|
artikel
|
| 65 |
Quasi-3D isogeometric buckling analysis method for advanced composite plates in thermal environments
|
Do, Vuong Nguyen Van
|
|
2019
|
92 |
C |
p. 34-54
|
artikel
|
| 66 |
Rapid design approach for U-bend of a turbine serpentine cooling passage
|
Kim, Changhee
|
|
2019
|
92 |
C |
p. 417-428
|
artikel
|
| 67 |
Rarefied airfoil aerodynamics based on the generalized hydrodynamic model
|
Xiao, H.
|
|
2019
|
92 |
C |
p. 148-155
|
artikel
|
| 68 |
Real-time simulation model for helicopter flight task analysis in turbulent atmospheric environment
|
Ji, Honglei
|
|
2019
|
92 |
C |
p. 289-299
|
artikel
|
| 69 |
Resistojet thruster with supercapacitor power source – design and experimental research
|
Kindracki, Jan
|
|
2019
|
92 |
C |
p. 847-857
|
artikel
|
| 70 |
RISE based active vibration control for the flexible refueling hose
|
Su, Zikang
|
|
2019
|
92 |
C |
p. 387-404
|
artikel
|
| 71 |
Robust optimization for a wing at drag divergence Mach number based on an improved PSO algorithm
|
Tao, Jun
|
|
2019
|
92 |
C |
p. 653-667
|
artikel
|
| 72 |
Robust output-feedback cascaded tracking controller for spatial motion of anisotropically-actuated vehicles
|
Michałek, Maciej Marcin
|
|
2019
|
92 |
C |
p. 915-929
|
artikel
|
| 73 |
Robust trajectory optimization using polynomial chaos and convex optimization
|
Wang, Fenggang
|
|
2019
|
92 |
C |
p. 314-325
|
artikel
|
| 74 |
Stability and ground experiments of a spinning triangular tethered satellite formation on a low earth orbit
|
Yu, B.S.
|
|
2019
|
92 |
C |
p. 595-604
|
artikel
|
| 75 |
Station-keeping performance analysis for high altitude balloon with altitude control system
|
Du, Huafei
|
|
2019
|
92 |
C |
p. 644-652
|
artikel
|
| 76 |
Structural health monitoring for long-term aircraft storage tanks under cryogenic temperature
|
Gao, Dongyue
|
|
2019
|
92 |
C |
p. 881-891
|
artikel
|
| 77 |
Surrogate models for the prediction of the aerodynamic performance of exhaust systems
|
Giangaspero, Giorgio
|
|
2019
|
92 |
C |
p. 77-90
|
artikel
|
| 78 |
Turbulent and transitional flow around the AVT-183 diamond wing
|
Buzica, Andrei
|
|
2019
|
92 |
C |
p. 520-535
|
artikel
|
| 79 |
Unknown-but-bounded uncertainty propagation in spacecraft structural system: Interval reduced basis method and its integrated framework
|
Lyu, Zheng
|
|
2019
|
92 |
C |
p. 945-957
|
artikel
|
| 80 |
Unscented Kalman filter state estimation for manipulating unmanned aerial vehicles
|
Bonyan Khamseh, H.
|
|
2019
|
92 |
C |
p. 446-463
|
artikel
|
| 81 |
Use of Blended Blade and End Wall method in compressor cascades: Definition and mechanism comparisons
|
Li, Jiabin
|
|
2019
|
92 |
C |
p. 738-749
|
artikel
|
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