| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active optimization adjustment for the surface accuracy of spaceborne SAR antennas
|
Yu, Dewen
|
|
|
138 |
C |
p.
|
artikel
|
| 2 |
Adaptive finite-time fault-tolerant control for nano-satellite attitude tracking under actuator constraints
|
M. Sadigh, Sevil
|
|
|
138 |
C |
p.
|
artikel
|
| 3 |
A discrete adjoint full potential formulation for fast aerostructural optimization in preliminary aircraft design
|
Crovato, Adrien
|
|
|
138 |
C |
p.
|
artikel
|
| 4 |
Aerodynamic performance-preserving construction method for a near-net-shape blade cross section
|
Guo, Yiming
|
|
|
138 |
C |
p.
|
artikel
|
| 5 |
A joint guidance and control framework for autonomous obstacle avoidance in quadrotor formations under model uncertainty
|
Ma, Zhenwei
|
|
|
138 |
C |
p.
|
artikel
|
| 6 |
A new aerodynamic identification technology for short-time hypersonic wind tunnels while considering inertial force interference
|
Li, Shichao
|
|
|
138 |
C |
p.
|
artikel
|
| 7 |
A refined spectral element model for wave propagation in multiscale hybrid epoxy/carbon fiber/graphene platelet composite shells
|
Hua, Fenfei
|
|
|
138 |
C |
p.
|
artikel
|
| 8 |
A robust adaptive linear parameter-varying gain-scheduling controller for aeroengines
|
Liu, Zhidan
|
|
|
138 |
C |
p.
|
artikel
|
| 9 |
A trade-off analysis between lateral/directional stability and radar cross section requirements of an air-to-air combat airframe
|
Bacci, David
|
|
|
138 |
C |
p.
|
artikel
|
| 10 |
A variable camber wing concept based on corrugated flexible composite skin
|
Bai, Jiang-Bo
|
|
|
138 |
C |
p.
|
artikel
|
| 11 |
Bending analysis of carbon nanotube coated–fiber multi-scale composite beams using the refined zigzag theory
|
Malekimoghadam, Reza
|
|
|
138 |
C |
p.
|
artikel
|
| 12 |
Calibration and validation of a space electrostatic accelerometer onboard Tianzhou-1 cargo spacecraft using GNSS and attitude data
|
Cai, Lin
|
|
|
138 |
C |
p.
|
artikel
|
| 13 |
Computational investigation of quiet propeller designs for small unmanned aerial vehicles
|
Ghoreyshi, Mehdi
|
|
|
138 |
C |
p.
|
artikel
|
| 14 |
Convex optimization for post-fault ascent trajectory replanning using auxiliary phases
|
Miao, Xinyuan
|
|
|
138 |
C |
p.
|
artikel
|
| 15 |
Design of thrust augmentation control schedule during mode transition for turbo-ramjet engine
|
Xi, Zhihua
|
|
|
138 |
C |
p.
|
artikel
|
| 16 |
Distributed cooperative fencing scheme for UAV swarm based on self-organized behaviors
|
Wen, Liangdong
|
|
|
138 |
C |
p.
|
artikel
|
| 17 |
Editorial Board
|
|
|
|
138 |
C |
p.
|
artikel
|
| 18 |
Effect of pressure on regenerative cooling process of endothermic hydrocarbon fuel at severe pyrolysis conditions
|
Tian, Ke
|
|
|
138 |
C |
p.
|
artikel
|
| 19 |
Effects of inlet total pressure on the formation and propagation characteristics of n-decane two-phase rotating detonation waves
|
Shao, Xiaofeng
|
|
|
138 |
C |
p.
|
artikel
|
| 20 |
Effects of swirling motion on the cavity flow field and combustion performance
|
Zhang, Kai
|
|
|
138 |
C |
p.
|
artikel
|
| 21 |
Equivalent plate dynamic modeling of space periodic truss structures
|
Sun, Jie
|
|
|
138 |
C |
p.
|
artikel
|
| 22 |
Event-triggered distributed cooperative extended Kalman filter based on formation estimation
|
Li, Jiali
|
|
|
138 |
C |
p.
|
artikel
|
| 23 |
Experimental and numerical simulation of shock train characteristics in an isolator with incident shocks
|
Wang, Ziao
|
|
|
138 |
C |
p.
|
artikel
|
| 24 |
Experimental and virtual testing of a composite-aluminium aircraft wingbox under thermal loading
|
Guerrero, José M.
|
|
|
138 |
C |
p.
|
artikel
|
| 25 |
Experimental investigation of the interaction between a curved-surface jet and the mainstream on an airfoil at Mach 8
|
Sun, Zhikun
|
|
|
138 |
C |
p.
|
artikel
|
| 26 |
Experimental study of rocket plume expansion in the rocket-based combined-cycle engine under the ejector mode
|
Yao, Yizhi
|
|
|
138 |
C |
p.
|
artikel
|
| 27 |
Extended-Kalman-filter-based equilibrium manifold expansion observer for ramjet nonlinear control
|
Lv, Chengkun
|
|
|
138 |
C |
p.
|
artikel
|
| 28 |
Forced response in a multi-stage aeroderivative axial compressor with acoustic excitations: Method validation with field data
|
Pinelli, Lorenzo
|
|
|
138 |
C |
p.
|
artikel
|
| 29 |
Improving aircraft performance using machine learning: A review
|
Le Clainche, Soledad
|
|
|
138 |
C |
p.
|
artikel
|
| 30 |
Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure
|
Rioseco Olave, Diego
|
|
|
138 |
C |
p.
|
artikel
|
| 31 |
Influence mechanism and quantificational evaluation of key factors affecting flutter stability of a transonic fan
|
Duan, Xianbo
|
|
|
138 |
C |
p.
|
artikel
|
| 32 |
Influences of microjet pressure and number of microjets on the control of shock wave/boundary layer interaction
|
Xu, Hao
|
|
|
138 |
C |
p.
|
artikel
|
| 33 |
Modeling and experimental study on orientation dynamics of a Mars rotorcraft with swashplate mechanism
|
Zhu, Kaijie
|
|
|
138 |
C |
p.
|
artikel
|
| 34 |
Multivariate ensembles-based hierarchical linkage strategy for system reliability evaluation of aeroengine cooling blades
|
Li, Xue-Qin
|
|
|
138 |
C |
p.
|
artikel
|
| 35 |
Nonlinear stochastic flutter analysis of a three-degree-of-freedom wing in a two-dimensional flow field under stochastic perturbations
|
Hao, Ying
|
|
|
138 |
C |
p.
|
artikel
|
| 36 |
Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle
|
Zhang, Yuqi
|
|
|
138 |
C |
p.
|
artikel
|
| 37 |
Numerical investigation of the effect of blade distortion laws on the corner flow separation of the axial-flow fan
|
Ding, Yanyan
|
|
|
138 |
C |
p.
|
artikel
|
| 38 |
Numerical study on droplet evaporation and propagation stability in normal-temperature two-phase rotating detonation system
|
Wen, Haocheng
|
|
|
138 |
C |
p.
|
artikel
|
| 39 |
On the starting point in designing Kresling origami
|
Alipour, Seyed Masoud
|
|
|
138 |
C |
p.
|
artikel
|
| 40 |
Opposing jets for heat flux reduction and uncertainty analysis on a V-shaped blunt leading edge
|
Liu, Sijia
|
|
|
138 |
C |
p.
|
artikel
|
| 41 |
Over-wing integration of ultra-high bypass ratio engines: A coupled wing redesign and engine position study
|
Tavares Silva, Vinícius
|
|
|
138 |
C |
p.
|
artikel
|
| 42 |
Prescribed-time extended state observer and prescribed performance control of quadrotor UAVs against actuator faults
|
Gong, Wenquan
|
|
|
138 |
C |
p.
|
artikel
|
| 43 |
Refined flow organization in squealer tip gap and its impact on turbine aerodynamic performance
|
He, Xiaojuan
|
|
|
138 |
C |
p.
|
artikel
|
| 44 |
Robust multidisciplinary analysis and optimization for conceptual design of flexible aircraft under dynamic aeroelastic constraints
|
Saporito, Marco
|
|
|
138 |
C |
p.
|
artikel
|
| 45 |
Shape sensing approach for composite and sandwich beam with generic cross-sections: Application to fiber-reinforced polymer composite airfoil
|
Zhao, Feifei
|
|
|
138 |
C |
p.
|
artikel
|
| 46 |
Source of buzz instability in a supersonic air inlet
|
Sepahi-Younsi, Javad
|
|
|
138 |
C |
p.
|
artikel
|
| 47 |
Temperature- and moisture-dependent aeroelastic stability of graphene platelet reinforced nanocomposite lattice sandwich plates subjected to supersonic flow
|
Zhang, Zhipeng
|
|
|
138 |
C |
p.
|
artikel
|
| 48 |
Unsteady characteristics of pressure and swirl distortion in helicopter intake: A lattice Boltzmann method approach
|
Di-Marco, Alexandre
|
|
|
138 |
C |
p.
|
artikel
|
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