| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Ablation characteristics of aluminum alloy wings with yttria partially–stabilized zirconia coating
|
Kim, Gyeongrok
|
|
|
105 |
C |
p.
|
artikel
|
| 2 |
Adaptive event-triggered control for quadrotor aircraft with output constraints
|
Wang, Jie
|
|
|
105 |
C |
p.
|
artikel
|
| 3 |
Aerodynamic study of paratrooper models used in the C-130 H/J personnel drop operations
|
Bergeron, Keith
|
|
|
105 |
C |
p.
|
artikel
|
| 4 |
Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics
|
Viviani, Antonio
|
|
|
105 |
C |
p.
|
artikel
|
| 5 |
A hybrid onboard adaptive model for aero-engine parameter prediction
|
Pang, Shuwei
|
|
|
105 |
C |
p.
|
artikel
|
| 6 |
Aircraft wing rock oscillations suppression by simple adaptive control
|
Andrievsky, Boris
|
|
|
105 |
C |
p.
|
artikel
|
| 7 |
Analysis of shock-wave unsteadiness in conical supersonic nozzles
|
Zebiri, B.
|
|
|
105 |
C |
p.
|
artikel
|
| 8 |
An improved method for mean flow boundary conditions for computational aeroacoustics
|
Samani, Iman
|
|
|
105 |
C |
p.
|
artikel
|
| 9 |
An investigation of the aerodynamic performance for a propeller-aided lift-enhancing double wing configuration
|
Wang, Hongbo
|
|
|
105 |
C |
p.
|
artikel
|
| 10 |
A novel modular deployable mechanism for the truss antenna: Assembly principle and performance analysis
|
Guo, Jinwei
|
|
|
105 |
C |
p.
|
artikel
|
| 11 |
A novel periodic mono-material strut with geometrical discontinuity for helicopter cabin noise reduction
|
Wang, Fengjiao
|
|
|
105 |
C |
p.
|
artikel
|
| 12 |
A numerical simulation investigation of the influence of rotor wake on sediment particles by computational fluid dynamics coupling discrete element method
|
Hu, Jianping
|
|
|
105 |
C |
p.
|
artikel
|
| 13 |
A reliable data-driven model for Ablative Pulsed Plasma Thruster
|
Hossain, Noman
|
|
|
105 |
C |
p.
|
artikel
|
| 14 |
A robust controller for multi rotor UAVs
|
Jasim, Omar A.
|
|
|
105 |
C |
p.
|
artikel
|
| 15 |
A semi-analytical stochastic buckling quantification of porous functionally graded plates
|
Trinh, Minh-Chien
|
|
|
105 |
C |
p.
|
artikel
|
| 16 |
A simplified computational method for two-body high spinning rate vehicles
|
de Celis, Raúl
|
|
|
105 |
C |
p.
|
artikel
|
| 17 |
A strategy to suppress limit cycle oscillations in helicopter ground resonance including landing gear nonlinearities
|
da Silva, José Augusto Ignacio
|
|
|
105 |
C |
p.
|
artikel
|
| 18 |
Asymptotic adaptive tracking control for hypersonic vehicles with guaranteeing multi-performance requirements
|
Guo, Jianguo
|
|
|
105 |
C |
p.
|
artikel
|
| 19 |
A two-objective design optimisation approach for blending repairs of damaged compressor blisks
|
Berger, Ricarda
|
|
|
105 |
C |
p.
|
artikel
|
| 20 |
Automatic orbital maneuver for mega-constellations maintenance with electrodynamic tethers
|
Liu, Jinyu
|
|
|
105 |
C |
p.
|
artikel
|
| 21 |
Bifurcation of equilibria for general case of gyrostat satellite on a circular orbit
|
Santos, Luis F.M.M.
|
|
|
105 |
C |
p.
|
artikel
|
| 22 |
Classification of supersonic flow over a rigid parachute model with suspension lines
|
Dahal, Nimesh
|
|
|
105 |
C |
p.
|
artikel
|
| 23 |
Compound helicopter multi-rotor dynamic radar cross section response analysis
|
Zhou, Zeyang
|
|
|
105 |
C |
p.
|
artikel
|
| 24 |
Design and real-time implementation of a wireless autopilot using multivariable predictive generalized minimum variance control in the state-space
|
Silveira, Antonio
|
|
|
105 |
C |
p.
|
artikel
|
| 25 |
Design method for non-axisymmetric generalized internal conical flowfield based on double 3D curved shock waves
|
Zhou, Hang
|
|
|
105 |
C |
p.
|
artikel
|
| 26 |
Design, modification and optimization of an ultra-high-load transonic low-reaction aspirated compressor
|
Sun, Shijun
|
|
|
105 |
C |
p.
|
artikel
|
| 27 |
Development of an improved view registration method with application in optical velocimetry
|
Hu, Boyao
|
|
|
105 |
C |
p.
|
artikel
|
| 28 |
Disturbance observer-based control for small nonlinear UAV systems with transient performance constraint
|
Chen, Jieqing
|
|
|
105 |
C |
p.
|
artikel
|
| 29 |
Dual Kriging assisted efficient global optimization of expensive problems with evaluation failures
|
He, Youwei
|
|
|
105 |
C |
p.
|
artikel
|
| 30 |
Dynamic lift characteristics of nonslender delta wing in large-amplitude-pitching
|
Yi, Yuan
|
|
|
105 |
C |
p.
|
artikel
|
| 31 |
Editorial Board
|
|
|
|
105 |
C |
p.
|
artikel
|
| 32 |
Effect of acceleration and deceleration of a capsule train running at transonic speed on the flow and heat transfer in the tube
|
Jiqiang, Niu
|
|
|
105 |
C |
p.
|
artikel
|
| 33 |
Effect of corrugation on the aerodynamic performance of three-dimensional flapping wings
|
Au, Loan Thi Kim
|
|
|
105 |
C |
p.
|
artikel
|
| 34 |
Effect of inclined block on fuel mixing of multi hydrogen jets in scramjet engine
|
Li, Zhixiong
|
|
|
105 |
C |
p.
|
artikel
|
| 35 |
Effect of inlet radial distortion on aerodynamic stability in a multi-stage axial flow compressor
|
Li, Jichao
|
|
|
105 |
C |
p.
|
artikel
|
| 36 |
Effects of the combustor width on propagation characteristics of rotating detonation waves
|
Wang, Zhicheng
|
|
|
105 |
C |
p.
|
artikel
|
| 37 |
Effects of unsteady interaction on the performance of an ultra-high-pressure-ratio centrifugal compressor
|
Zhang, Yingjie
|
|
|
105 |
C |
p.
|
artikel
|
| 38 |
Experimental and numerical study of combustion characteristics in a liquid fuel CAN micro-combustor
|
SadatAkhavi, SeyedMohammadReza
|
|
|
105 |
C |
p.
|
artikel
|
| 39 |
Experimental investigation of liquid transport in a vane type tank of satellite with microgravity
|
Liu, Jintao
|
|
|
105 |
C |
p.
|
artikel
|
| 40 |
Experimental investigation of self-excited combustion instabilities in a small Earth storable bipropellant rocket combustor
|
Xue, Shuaijie
|
|
|
105 |
C |
p.
|
artikel
|
| 41 |
Extraction and analysis of transient signals of a deployable structure vibration based on the sparse decomposition with mixed norms
|
Liu, Tao
|
|
|
105 |
C |
p.
|
artikel
|
| 42 |
Failure mechanism of casing treatment in improving stability of a highly loaded two-stage axial compressor
|
Wang, Wei
|
|
|
105 |
C |
p.
|
artikel
|
| 43 |
Fast pressure distribution prediction of airfoils using deep learning
|
Hui, Xinyu
|
|
|
105 |
C |
p.
|
artikel
|
| 44 |
Flow characteristics on a 4-stage low-speed research compressor with a cantilevered stator
|
Ju, Zhenzhou
|
|
|
105 |
C |
p.
|
artikel
|
| 45 |
Flowfield induced by a plasma synthetic jet actuator with low exit inclination angle under low ambient pressure
|
Huang, He-xia
|
|
|
105 |
C |
p.
|
artikel
|
| 46 |
Free vibration analysis of functionally graded hybrid matrix/fiber nanocomposite conical shells using multiscale method
|
Rezaiee-Pajand, M.
|
|
|
105 |
C |
p.
|
artikel
|
| 47 |
High-velocity impact behavior of sandwich structures with AL faces and foam cores—Experimental and numerical study
|
Abbasi, Mohammad
|
|
|
105 |
C |
p.
|
artikel
|
| 48 |
Hybrid robust and optimal control for pointing a staring-mode spacecraft
|
Geng, Yuanzhuo
|
|
|
105 |
C |
p.
|
artikel
|
| 49 |
Incremental model based online heuristic dynamic programming for nonlinear adaptive tracking control with partial observability
|
Zhou, Ye
|
|
|
105 |
C |
p.
|
artikel
|
| 50 |
Investigation of the casing groove location effect for a large tip clearance in a counter-rotating axial flow compressor
|
Mao, Xiaochen
|
|
|
105 |
C |
p.
|
artikel
|
| 51 |
Jet impingement using an adjustable spreading-angle sweeping jet
|
Wen, Xin
|
|
|
105 |
C |
p.
|
artikel
|
| 52 |
Large eddy simulation of a turbulent non-premixed flame based on the flamelet-generated manifolds approach and a reduced mechanism verification
|
Xing, Yunfei
|
|
|
105 |
C |
p.
|
artikel
|
| 53 |
Model-based path prediction for fixed-wing unmanned aircraft using pose estimates
|
Kang, Changkoo
|
|
|
105 |
C |
p.
|
artikel
|
| 54 |
Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows
|
Ju, Shengjun
|
|
|
105 |
C |
p.
|
artikel
|
| 55 |
Near and far field laminar flow structures in an axisymmetric zero-net-mass-flux jet
|
Le Clainche, Soledad
|
|
|
105 |
C |
p.
|
artikel
|
| 56 |
Neural observer-based quantized output feedback control for MEMS gyroscopes with guaranteed transient performance
|
Shi, Yi
|
|
|
105 |
C |
p.
|
artikel
|
| 57 |
Nonlinear guaranteed cost attitude control via dynamic gain design
|
Wang, Hui
|
|
|
105 |
C |
p.
|
artikel
|
| 58 |
Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection
|
Zhang, Zijian
|
|
|
105 |
C |
p.
|
artikel
|
| 59 |
Numerical investigation of compressibility effect on dynamic stall
|
Kim, Taesoon
|
|
|
105 |
C |
p.
|
artikel
|
| 60 |
Numerical investigation of pitch motion induced unsteady effects on transverse jet interaction
|
Lai, Jiang
|
|
|
105 |
C |
p.
|
artikel
|
| 61 |
Numerical investigation of second throat exhaust diffuser performance with thrust optimized parabolic nozzles
|
Fouladi, N.
|
|
|
105 |
C |
p.
|
artikel
|
| 62 |
Numerical investigation on convective heat transfer of supercritical aviation kerosene in a horizontal tube under hyper gravity conditions
|
Lv, Lulu
|
|
|
105 |
C |
p.
|
artikel
|
| 63 |
Numerical simulations of flutter mechanism for high-speed wide-chord transonic fan
|
Dong, Xu
|
|
|
105 |
C |
p.
|
artikel
|
| 64 |
Numerical study of aerodynamic and aeroacoustic characteristics of flow over porous coated cylinders: Effects of porous properties
|
Li, Zhiyong
|
|
|
105 |
C |
p.
|
artikel
|
| 65 |
Optimization and analysis of inverse design method of maximum thrust scramjet nozzles
|
Yu, Kaikai
|
|
|
105 |
C |
p.
|
artikel
|
| 66 |
Orbit determination for fuel station in multiple SSO spacecraft refueling considering the J2 perturbation
|
Zhu, Xiaoyu
|
|
|
105 |
C |
p.
|
artikel
|
| 67 |
Overall flow dynamics characteristics of slit-vent cylinders
|
Zhu, Rui
|
|
|
105 |
C |
p.
|
artikel
|
| 68 |
Performance characteristics of a solid oxide fuel cell hybrid jet engine under different operating modes
|
Ji, Zhixing
|
|
|
105 |
C |
p.
|
artikel
|
| 69 |
Performance of a novel mixed-flow trapped vortex combustor for turboshaft engine
|
Jiang, Ping
|
|
|
105 |
C |
p.
|
artikel
|
| 70 |
POD analysis of the unsteady behavior of blade wake under the influence of laminar separation vortex shedding in a compressor cascade
|
Shi, Lei
|
|
|
105 |
C |
p.
|
artikel
|
| 71 |
Prediction and evaluation of the stage-separation compatibility of an internally carried air-launch vehicle
|
Song, Wei
|
|
|
105 |
C |
p.
|
artikel
|
| 72 |
Probabilistic multi-aircraft conflict detection and resolution considering wind forecast uncertainty
|
Hernández-Romero, Eulalia
|
|
|
105 |
C |
p.
|
artikel
|
| 73 |
Proper orthogonal decomposition assisted inverse design optimisation method for the compressor cascade airfoil
|
Zhu, Yujie
|
|
|
105 |
C |
p.
|
artikel
|
| 74 |
Quaternion-based nonlinear attitude control of quadrotor formations carrying a slung load
|
Ariyibi, Segun O.
|
|
|
105 |
C |
p.
|
artikel
|
| 75 |
Rigid spacecraft robust optimal attitude stabilization under actuator misalignments
|
Wang, Zhong
|
|
|
105 |
C |
p.
|
artikel
|
| 76 |
Simultaneous simulation of transition and massive separation by RANS-LES-Tr model
|
Wang, Guangxing
|
|
|
105 |
C |
p.
|
artikel
|
| 77 |
Spiral flow induced destabilizing force analysis and its reduction with a novel helix-comb gas seal
|
Zhang, Mingjie
|
|
|
105 |
C |
p.
|
artikel
|
| 78 |
Stall inception in a contra-rotating fan under radially distorted inflows
|
Manas, M.P.
|
|
|
105 |
C |
p.
|
artikel
|
| 79 |
Stochastic meshless method for nonlinear vibration analysis of composite plate reinforced with carbon fibers
|
Wang, J.F.
|
|
|
105 |
C |
p.
|
artikel
|
| 80 |
Study on decay characteristics of vertical four-vortex system for increasing airport capacity
|
Cho, Junho
|
|
|
105 |
C |
p.
|
artikel
|
| 81 |
Study on inner characteristics of plasma synthetic jet actuator and geometric effects
|
Zhang, Weilin
|
|
|
105 |
C |
p.
|
artikel
|
| 82 |
The design and validation of over/under turbine-based combined cycle inlet
|
Yuan, Huacheng
|
|
|
105 |
C |
p.
|
artikel
|
| 83 |
The joint empirical mode decomposition-local mean decomposition method and its application to time series of compressor stall process
|
Yue, Shaoyuan
|
|
|
105 |
C |
p.
|
artikel
|
| 84 |
The role of shaft-speed oscillation on the instability behavior of transonic radial compressor
|
Zeng, Hanxuan
|
|
|
105 |
C |
p.
|
artikel
|
| 85 |
Three-dimensional (3D) Monte-Carlo modeling for UAS collision risk management in restricted airport airspace
|
Wang, C.H. John
|
|
|
105 |
C |
p.
|
artikel
|
| 86 |
Three-dimensional impact angle control guidance with field-of-view constraint
|
Liu, Bojun
|
|
|
105 |
C |
p.
|
artikel
|
| 87 |
Towards a PDE-based large-scale decentralized solution for path planning of UAVs in shared airspace
|
Radmanesh, Reza
|
|
|
105 |
C |
p.
|
artikel
|
| 88 |
Transient 3D conjugate heat transfer simulation of a rectangular GOX–GCH4 rocket combustion chamber and validation
|
Hötte, Felix
|
|
|
105 |
C |
p.
|
artikel
|
| 89 |
Two-layer adaptive augmentation for incremental backstepping flight control of transport aircraft in uncertain conditions
|
Ignatyev, Dmitry I.
|
|
|
105 |
C |
p.
|
artikel
|
| 90 |
Two-stage fuel injection performance of RBCC under scramjet mode
|
Li, Jiang
|
|
|
105 |
C |
p.
|
artikel
|
| 91 |
Upper trust bound feasibility criterion for mixed constrained Bayesian optimization with application to aircraft design
|
Priem, R.
|
|
|
105 |
C |
p.
|
artikel
|
| 92 |
Variable-fidelity multipoint aerodynamic shape optimization with output-based adapted meshes
|
Chen, Guodong
|
|
|
105 |
C |
p.
|
artikel
|
| 93 |
Vibro-acoustics response of an isotropic plate under non-uniform edge loading: An analytical investigation
|
Gunasekaran, Vijay
|
|
|
105 |
C |
p.
|
artikel
|
| 94 |
Vortex trajectory prediction and mode analysis of compressor stall with strong non-uniformity
|
Fu, Li
|
|
|
105 |
C |
p.
|
artikel
|
Tijdschrift beschrijving