| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active aeroelastic output feedback control with partial measurements by the method of receptances
|
Singh, Kumar Vikram
|
|
2019
|
86 |
C |
p. 47-63
|
artikel
|
| 2 |
Adaptive fractional order sliding mode control for a quadrotor with a varying load
|
Vahdanipour, Mohsen
|
|
2019
|
86 |
C |
p. 737-747
|
artikel
|
| 3 |
Aerodisk effects on drag reduction for hypersonic blunt body with an ellipsoid nose
|
Zhong, Kang
|
|
2019
|
86 |
C |
p. 599-612
|
artikel
|
| 4 |
Aerodynamic characteristics of flexible wings with leading-edge veins in pitch motions
|
Ryu, YeongGyun
|
|
2019
|
86 |
C |
p. 558-571
|
artikel
|
| 5 |
Aerodynamic shape optimization using a novel optimizer based on machine learning techniques
|
Yan, Xinghui
|
|
2019
|
86 |
C |
p. 826-835
|
artikel
|
| 6 |
Aero-servo-elastic design of a morphing wing trailing edge system for enhanced cruise performance
|
Arena, Maurizio
|
|
2019
|
86 |
C |
p. 215-235
|
artikel
|
| 7 |
A fast finite-time convergent guidance law with nonlinear disturbance observer for unmanned aerial vehicles collision avoidance
|
Zhang, Ning
|
|
2019
|
86 |
C |
p. 204-214
|
artikel
|
| 8 |
A flutter prediction method with low cost and low risk from test data
|
Zhang, Weiwei
|
|
2019
|
86 |
C |
p. 542-557
|
artikel
|
| 9 |
A grid strategy for predicting the space plane's hypersonic aerodynamic heating loads
|
Qu, Feng
|
|
2019
|
86 |
C |
p. 659-670
|
artikel
|
| 10 |
An iterative dimension-by-dimension method for structural interval response prediction with multidimensional uncertain variables
|
Xiong, Chuang
|
|
2019
|
86 |
C |
p. 572-581
|
artikel
|
| 11 |
An iterative strategy for task assignment and path planning of distributed multiple unmanned aerial vehicles
|
Yao, Weiran
|
|
2019
|
86 |
C |
p. 455-464
|
artikel
|
| 12 |
A probabilistic approach to measure aircraft conflict severity considering wind forecast uncertainty
|
Hernández-Romero, Eulalia
|
|
2019
|
86 |
C |
p. 401-414
|
artikel
|
| 13 |
Autonomous reduced-gravity enabling quadrotor test-bed: Design, modelling and flight test analysis
|
Siddhardha, Kedarisetty
|
|
2019
|
86 |
C |
p. 64-77
|
artikel
|
| 14 |
Autonomous temperature-based orbit estimation
|
Nasihati Gourabi, Forough
|
|
2019
|
86 |
C |
p. 671-682
|
artikel
|
| 15 |
Buckling and post-buckling analysis of cracked stiffened panels via an X-Ritz method
|
Gulizzi, V.
|
|
2019
|
86 |
C |
p. 268-282
|
artikel
|
| 16 |
Combustion flow in different advanced vortex combustors with/without vortex generator
|
Zeng, Zhuoxiong
|
|
2019
|
86 |
C |
p. 640-649
|
artikel
|
| 17 |
Comparison of wind speed models within a Pitot-free airspeed estimation algorithm using light aviation data
|
Rhudy, Matthew B.
|
|
2019
|
86 |
C |
p. 21-29
|
artikel
|
| 18 |
Computational study of axisymmetric divergent bypass dual throat nozzle
|
Wang, Yangsheng
|
|
2019
|
86 |
C |
p. 177-190
|
artikel
|
| 19 |
Control of compressor tip leakage flow using plasma actuation
|
Zhang, Haideng
|
|
2019
|
86 |
C |
p. 244-255
|
artikel
|
| 20 |
Damage development and lifetime prediction of fiber-reinforced ceramic-matrix composites subjected to cyclic loading at 1300°C in vacuum, inert and oxidative atmospheres
|
Li, Longbiao
|
|
2019
|
86 |
C |
p. 613-629
|
artikel
|
| 21 |
Design methodology using characteristic parameters control for low Reynolds number airfoils
|
Zhang, Sen
|
|
2019
|
86 |
C |
p. 143-152
|
artikel
|
| 22 |
Development of a computational fluid dynamics compatible mathematical model for boundary layer transitional flows in low-disturbance environment
|
Xu, Jiakuan
|
|
2019
|
86 |
C |
p. 487-496
|
artikel
|
| 23 |
Discharge voltage characteristic in ablative pulsed plasma thrusters
|
Sun, Guorui
|
|
2019
|
86 |
C |
p. 153-159
|
artikel
|
| 24 |
Editorial Board
|
|
|
2019
|
86 |
C |
p. ii
|
artikel
|
| 25 |
Effect of acicular vortex generators on the aerodynamic features of a slender delta wing
|
Nematollahi, Omid
|
|
2019
|
86 |
C |
p. 327-340
|
artikel
|
| 26 |
Effect of von Karman length scale in scale adaptive simulation approach on the prediction of supersonic turbulent flow
|
Xu, Chang-Yue
|
|
2019
|
86 |
C |
p. 630-639
|
artikel
|
| 27 |
Evaluation of the relationship between the aerothermodynamic process and operational parameters in the high-pressure turbine of an aircraft engine
|
Nguyen, Trung Hieu
|
|
2019
|
86 |
C |
p. 93-105
|
artikel
|
| 28 |
Experimental investigation on hover performance of a single-rotor system for Mars helicopter
|
Zhao, Pengyue
|
|
2019
|
86 |
C |
p. 582-591
|
artikel
|
| 29 |
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor
|
Zhong, Fengquan
|
|
2019
|
86 |
C |
p. 775-781
|
artikel
|
| 30 |
Flexible aircraft gust encounter simulation using subspace projection model reduction
|
Bekemeyer, P.
|
|
2019
|
86 |
C |
p. 805-817
|
artikel
|
| 31 |
Flight performance simulation and station-keeping endurance analysis for stratospheric super-pressure balloon in real wind field
|
Du, Huafei
|
|
2019
|
86 |
C |
p. 1-10
|
artikel
|
| 32 |
Flow characteristics of monopropellant micro-scale planar nozzles
|
Banuti, Daniel T.
|
|
2019
|
86 |
C |
p. 341-350
|
artikel
|
| 33 |
Forecasting-based data-driven model-free adaptive sliding mode attitude control of combined spacecraft
|
Gao, Han
|
|
2019
|
86 |
C |
p. 364-374
|
artikel
|
| 34 |
Full-length visualisation of liquid oxygen disintegration in a single injector sub-scale rocket combustor
|
Suslov, Dmitry I.
|
|
2019
|
86 |
C |
p. 444-454
|
artikel
|
| 35 |
Fusing wind-tunnel measurements and CFD data using constrained gappy proper orthogonal decomposition
|
Mifsud, Michael
|
|
2019
|
86 |
C |
p. 312-326
|
artikel
|
| 36 |
Fuzzy-reconstruction-based robust tracking control of an air-breathing hypersonic vehicle
|
Cheng, Xianlei
|
|
2019
|
86 |
C |
p. 694-703
|
artikel
|
| 37 |
Generalized boundary equations for conservative Navier–Stokes equations
|
Du, Yongle
|
|
2019
|
86 |
C |
p. 836-849
|
artikel
|
| 38 |
Gust load alleviation in a flexible smart idealized wing
|
Versiani, Thiago de Souza Siqueira
|
|
2019
|
86 |
C |
p. 762-774
|
artikel
|
| 39 |
High-power mode control for triaxial gas turbines with variable power turbine guide vanes
|
Wang, Tao
|
|
2019
|
86 |
C |
p. 132-142
|
artikel
|
| 40 |
Impact time and angle control guidance independent of time-to-go prediction
|
Zhu, Jianwen
|
|
2019
|
86 |
C |
p. 818-825
|
artikel
|
| 41 |
Improved artificial potential field based lateral entry guidance for waypoints passage and no-fly zones avoidance
|
Li, Zhenhua
|
|
2019
|
86 |
C |
p. 119-131
|
artikel
|
| 42 |
Improvements of performance and stability of a single-stage transonic axial compressor using a combined flow control approach
|
Hu, Jiaguo
|
|
2019
|
86 |
C |
p. 283-295
|
artikel
|
| 43 |
Influence of spanwise transversal surface wave on coherent structures in turbulent boundary layers
|
Roggenkamp, Dorothee
|
|
2019
|
86 |
C |
p. 387-400
|
artikel
|
| 44 |
Infrared signature of serpentine nozzle with engine swirl
|
Cheng, Wen
|
|
2019
|
86 |
C |
p. 794-804
|
artikel
|
| 45 |
Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraft
|
Bravo-Mosquera, Pedro David
|
|
2019
|
86 |
C |
p. 497-519
|
artikel
|
| 46 |
Investigating the effect of engine speed and flight altitude on the performance of throttle body injection (TBI) system of a two-stroke air-powered engine
|
Hassantabar, Ali
|
|
2019
|
86 |
C |
p. 375-386
|
artikel
|
| 47 |
Investigation of winglet on the transonic flutter characteristics for a wind tunnel test model CHNT-1
|
Lv, Binbin
|
|
2019
|
86 |
C |
p. 430-437
|
artikel
|
| 48 |
Lagrangian analysis of mass transport and its influence on the lift enhancement in a flow over the airfoil with a synthetic jet
|
Cao, Shengli
|
|
2019
|
86 |
C |
p. 11-20
|
artikel
|
| 49 |
Large eddy simulation of supersonic, compressible, turbulent mixing layers
|
Arora, Konark
|
|
2019
|
86 |
C |
p. 592-598
|
artikel
|
| 50 |
Modified near-wakes of axisymmetric cylinders with slanted base
|
Bulathsinghala, D.S.
|
|
2019
|
86 |
C |
p. 351-363
|
artikel
|
| 51 |
Multi-point powered descent guidance based on optimal sensitivity
|
Ma, Lin
|
|
2019
|
86 |
C |
p. 465-477
|
artikel
|
| 52 |
Nonlinear dynamic analysis near resonance of a beam-ring structure for modeling circular truss antenna under time-dependent thermal excitation
|
Zhang, W.
|
|
2019
|
86 |
C |
p. 296-311
|
artikel
|
| 53 |
Nonlinear mapping based impact angle control guidance with seeker's field-of-view constraint
|
Liu, Bojun
|
|
2019
|
86 |
C |
p. 724-736
|
artikel
|
| 54 |
Numerical evaluation of aerodome and cooling jet for aeroheating reduction
|
Qin, Qihao
|
|
2019
|
86 |
C |
p. 520-533
|
artikel
|
| 55 |
Numerical investigation into the underlying mechanism connecting the vortex breakdown to the flow unsteadiness in a transonic compressor rotor
|
Wu, Yanhui
|
|
2019
|
86 |
C |
p. 106-118
|
artikel
|
| 56 |
Numerical investigation of aeroacoustics damping performance of a Helmholtz resonator: Effects of geometry, grazing and bias flow
|
Wu, Gang
|
|
2019
|
86 |
C |
p. 191-203
|
artikel
|
| 57 |
Output feedback continuous terminal sliding mode guidance law for missile-target interception with autopilot dynamics
|
Zhao, Zhenhua
|
|
2019
|
86 |
C |
p. 256-267
|
artikel
|
| 58 |
Path dependence characteristic of shock train in a 2D hypersonic inlet with variable background waves
|
Shi, Wen
|
|
2019
|
86 |
C |
p. 650-658
|
artikel
|
| 59 |
Planform-customized waverider design integrating with vortex effect
|
Liu, Chuanzhen
|
|
2019
|
86 |
C |
p. 438-443
|
artikel
|
| 60 |
Positioning control for stratospheric satellites subject to dynamics uncertainty and input constraints
|
Yang, Yueneng
|
|
2019
|
86 |
C |
p. 534-541
|
artikel
|
| 61 |
Robust multi-target tracking under mismatches in both dynamic and measurement models
|
Zhang, Wanying
|
|
2019
|
86 |
C |
p. 748-761
|
artikel
|
| 62 |
Solid fuel ramjet fuel optimization for maximum impulse-density with respect to air to fuel ratio and relative fuel regression rates derived from thermogravimetric analysis
|
McDonald, Brian
|
|
2019
|
86 |
C |
p. 478-486
|
artikel
|
| 63 |
Sound transmission loss behavior of sandwich panel with different truss cores under external mean airflow
|
Fu, Tao
|
|
2019
|
86 |
C |
p. 714-723
|
artikel
|
| 64 |
Static performance modeling and simulation of the staged combustion cycle LPREs
|
Naderi, Mahyar
|
|
2019
|
86 |
C |
p. 30-46
|
artikel
|
| 65 |
Suggestions on investigations of lobed jet mixing
|
Sheng, Zhi-qiang
|
|
2019
|
86 |
C |
p. 415-429
|
artikel
|
| 66 |
Supersonic inlet buzz detection using pressure measurement on wind tunnel wall
|
Farahani, Mohammad
|
|
2019
|
86 |
C |
p. 782-793
|
artikel
|
| 67 |
The effect of mismatching between combustor and HP vanes on the aerodynamics and heat load in a 1-1/2 stages turbine
|
Li, Yifei
|
|
2019
|
86 |
C |
p. 78-92
|
artikel
|
| 68 |
Three-dimensional terminal angle constrained robust guidance law with autopilot lag consideration
|
Ji, Yi
|
|
2019
|
86 |
C |
p. 160-176
|
artikel
|
| 69 |
Three-dimensional unsteady simulation of a multistage axial compressor with labyrinth seals and its effects on overall performance and flow characteristics
|
Kim, Sangjo
|
|
2019
|
86 |
C |
p. 683-693
|
artikel
|
| 70 |
Treatment and optimization of casing and blade tip for aerodynamic control of tip leakage flow in a turbine cascade
|
Jiang, Shuai
|
|
2019
|
86 |
C |
p. 704-713
|
artikel
|
| 71 |
Velocity behavior downstream of perforated plates with large blockage ratio for unstable and stable detonations
|
Zhang, Bo
|
|
2019
|
86 |
C |
p. 236-243
|
artikel
|
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