nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Active vibration isolation of ultra-stable optical reference cavity of space optical clock
|
He, Keda |
|
|
112 |
C |
p. |
artikel |
2 |
Adaptive control for linear parameter-varying systems with application to a VTOL aircraft
|
Snyder, Steven |
|
|
112 |
C |
p. |
artikel |
3 |
Adaptive super-twisting non-singular terminal sliding mode control for tracking of quadrotor with bounded disturbances
|
Ghadiri, Hamid |
|
|
112 |
C |
p. |
artikel |
4 |
Aerodynamic and aeroacoustic investigations of multi-copter rotors with leading edge serrations during forward flight
|
Hu, Haitao |
|
|
112 |
C |
p. |
artikel |
5 |
Aerodynamic behavior of a transonic axial flow compressor stage with self-recirculating casing treatment
|
Kumar, S Satish |
|
|
112 |
C |
p. |
artikel |
6 |
Air curtain application for leakage reduction in gas turbine shroud sealing
|
Wasilczuk, Filip |
|
|
112 |
C |
p. |
artikel |
7 |
A multi-body control approach for flapping wing micro aerial vehicles
|
Khosravi, Mahdi |
|
|
112 |
C |
p. |
artikel |
8 |
A nacelle inlet design approach with more three-dimensional geometric consideration
|
Wang, Shuyue |
|
|
112 |
C |
p. |
artikel |
9 |
An adaptive sampling strategy for construction of surrogate aerodynamic model
|
Wang, Xiaojun |
|
|
112 |
C |
p. |
artikel |
10 |
Analysis of acoustic, entropy and vorticity waves in a non-uniform annular combustor
|
Yang, Lijun |
|
|
112 |
C |
p. |
artikel |
11 |
An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles
|
Aprovitola, Andrea |
|
|
112 |
C |
p. |
artikel |
12 |
A numerical investigation on heterogeneous combustion of aluminum nanoparticle clouds
|
Zou, Xiangrui |
|
|
112 |
C |
p. |
artikel |
13 |
Application of three-dimensional diagnostics on the direct-current electric-field assisted combustion
|
Liu, Hecong |
|
|
112 |
C |
p. |
artikel |
14 |
Assessment of dynamic pairwise wake vortex separations for approach and landing at Vienna airport
|
Holzäpfel, Frank |
|
|
112 |
C |
p. |
artikel |
15 |
Cavitation suppression in the nozzle-flapper valves of the aircraft hydraulic system using triangular nozzle exits
|
Yang, He |
|
|
112 |
C |
p. |
artikel |
16 |
Data-based approach for wing shape design optimization
|
Li, Jichao |
|
|
112 |
C |
p. |
artikel |
17 |
Design, aerodynamic analysis and test flight of a bat-inspired tailless flapping wing unmanned aerial vehicle
|
Bie, Dawei |
|
|
112 |
C |
p. |
artikel |
18 |
Eddy current de-tumbling large geostationary debris based on feedback linearization model predictive control
|
Liu, Xiyao |
|
|
112 |
C |
p. |
artikel |
19 |
Editorial Board
|
|
|
|
112 |
C |
p. |
artikel |
20 |
Effect of the reaction mechanism on the numerical prediction of the performance of a scramjet combustor at cruise flight 8 Mach number
|
Rabadan Santana, Edder |
|
|
112 |
C |
p. |
artikel |
21 |
Experimental characterization of a novel nose landing gear shimmy damper using a small-scale test rig
|
Mustashin, Mir Sakib |
|
|
112 |
C |
p. |
artikel |
22 |
Experimental cross-flow control in a 3D boundary layer by multi-discharge plasma actuators
|
Baranov, Sergey A. |
|
|
112 |
C |
p. |
artikel |
23 |
Experimental investigation on axial compressor stall phenomena using aeroacoustics measurements via empirical mode and proper orthogonal decomposition methods
|
Guan, Di |
|
|
112 |
C |
p. |
artikel |
24 |
Experimental investigations of equivalence ratio effect on nonlinear dynamics features in premixed swirl-stabilized combustor
|
Rao, Zhuming |
|
|
112 |
C |
p. |
artikel |
25 |
Flight quality characteristics and observer-based anti-windup finite-time terminal sliding mode attitude control of aileron-free full-wing configuration UAV
|
Sun, Ruijie |
|
|
112 |
C |
p. |
artikel |
26 |
Flight testing full conversion of a 40-kg-class tilt-duct unmanned aerial vehicle
|
Chang, Sungho |
|
|
112 |
C |
p. |
artikel |
27 |
Free vibration analysis of cracked FG CNTRC plates using phase field theory
|
Duc, Nguyen Dinh |
|
|
112 |
C |
p. |
artikel |
28 |
Game theoretic self-organization in multi-satellite distributed task allocation
|
Sun, Changhao |
|
|
112 |
C |
p. |
artikel |
29 |
Geometrically nonlinear flexural analysis of multilayered composite plate using polynomial and non-polynomial shear deformation theories
|
Verma, Surendra |
|
|
112 |
C |
p. |
artikel |
30 |
Gradient based empirical cumulative distribution function approximation for robust aerodynamic design
|
Morales, Elisa |
|
|
112 |
C |
p. |
artikel |
31 |
HNN-based generalized predictive control for turbofan engine direct performance optimization
|
Zhou, Xin |
|
|
112 |
C |
p. |
artikel |
32 |
Hybrid path planning using positioning risk and artificial potential fields
|
Shin, Yujin |
|
|
112 |
C |
p. |
artikel |
33 |
Improvement of the low-frequency sound insulation of the poroelastic aerospace constructions considering Pasternak elastic foundation
|
Zarastvand, M.R. |
|
|
112 |
C |
p. |
artikel |
34 |
Kalman-filter-based robust control for hypersonic flight vehicle with measurement noises
|
Liang, Shuai |
|
|
112 |
C |
p. |
artikel |
35 |
Lambda shock behaviors of elliptic supersonic jets; a numerical analysis with modification of RANS turbulence model
|
Mirjalily, Seyed Ali Agha |
|
|
112 |
C |
p. |
artikel |
36 |
Large eddy simulation of film cooling effectiveness on a turbine vane pressure side with a saw-tooth plasma actuator
|
Li, Guozhan |
|
|
112 |
C |
p. |
artikel |
37 |
Luminescent intensity enhancement of pressure-sensitive paint by optimization of mole fraction of oxygen
|
Kurihara, Daiki |
|
|
112 |
C |
p. |
artikel |
38 |
Modal decomposition of the unsteady non-reactive flow field in a swirl-stabilized combustor operated by a Lean Premixed injection system
|
Salvador, F.J. |
|
|
112 |
C |
p. |
artikel |
39 |
Modeling and stability of balloon-borne gondolas with coupled pendulum-torsion dynamics
|
Kassarian, E. |
|
|
112 |
C |
p. |
artikel |
40 |
Modeling multi-loop intelligent pilot control behavior for aircraft-pilot couplings analysis
|
Xu, Shuting |
|
|
112 |
C |
p. |
artikel |
41 |
Nonlinear optimal attitude control of spacecraft using novel state-dependent coefficient parameterizations
|
Yao, Junyu |
|
|
112 |
C |
p. |
artikel |
42 |
Novel method to calculate satellite visibility for an arbitrary sensor field
|
Han, Chao |
|
|
112 |
C |
p. |
artikel |
43 |
Numerical investigation on spray self-pulsation characteristics of a liquid-centered swirl coaxial injector
|
Ren, Yongjie |
|
|
112 |
C |
p. |
artikel |
44 |
Numerical modeling on installed performance of turbofan engine with inlet ejector
|
Chen, Haoying |
|
|
112 |
C |
p. |
artikel |
45 |
Numerical simulation of hypersonic reaction flows with nonlinear coupled constitutive relations
|
Yuan, Zhenyu |
|
|
112 |
C |
p. |
artikel |
46 |
On deep-learning-based geometric filtering in aerodynamic shape optimization
|
Li, Jichao |
|
|
112 |
C |
p. |
artikel |
47 |
Optimal detumbling trajectory generation and coordinated control after space manipulator capturing tumbling targets
|
Zong, Lijun |
|
|
112 |
C |
p. |
artikel |
48 |
Optimization configuration of gas path sensors using a hybrid method based on tabu search artificial bee colony and improved genetic algorithm in turbofan engine
|
Hu, Yu |
|
|
112 |
C |
p. |
artikel |
49 |
Optimization of low-thrust Earth-orbit transfers using the vectorial orbital elements
|
Wang, Yu |
|
|
112 |
C |
p. |
artikel |
50 |
Performance estimation for Kalman filter based multi-agent cooperative navigation by employing graph theory
|
Wang, Shizhuang |
|
|
112 |
C |
p. |
artikel |
51 |
Potential hop reachable domain over surfaces of small bodies
|
Zeng, Xiangyuan |
|
|
112 |
C |
p. |
artikel |
52 |
Pretension modeling and form-finding for cable-network antennas with varying topologies and parameters
|
Yuan, Pengfei |
|
|
112 |
C |
p. |
artikel |
53 |
Range-based collaborative relative navigation for multiple unmanned aerial vehicles using consensus extended Kalman filter
|
Gong, Baichun |
|
|
112 |
C |
p. |
artikel |
54 |
Rapid design generation and multifidelity analysis of aircraft structures
|
Gandhi, Viraj |
|
|
112 |
C |
p. |
artikel |
55 |
Reciprocal guidance approach for suspicious collision point identification in a multi-agent unmanned aerial vehicle scenario
|
Shalumov, Vitaly |
|
|
112 |
C |
p. |
artikel |
56 |
Robust neural-network-based quasi-sliding-mode control for spacecraft-attitude maneuvering with prescribed performance
|
Fu, Jingbo |
|
|
112 |
C |
p. |
artikel |
57 |
Robust spacecraft rendezvous using a variable speed control moment gyro and thruster
|
Biggs, James D. |
|
|
112 |
C |
p. |
artikel |
58 |
Simultaneous trajectory tracking and aerial manipulation using a multi-stage model predictive control
|
Emami, Seyyed Ali |
|
|
112 |
C |
p. |
artikel |
59 |
Spatial coherence of low-frequency unsteadiness associated with a normal shock wave
|
Ligrani, P.M. |
|
|
112 |
C |
p. |
artikel |
60 |
Static and dynamic testing of a full-composite VLA by using digital image correlation and output-only ground vibration testing
|
Pagani, A. |
|
|
112 |
C |
p. |
artikel |
61 |
Statistical residual-based time series methods for multicopter fault detection and identification
|
Dutta, Airin |
|
|
112 |
C |
p. |
artikel |
62 |
Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner
|
Wang, Kuanliang |
|
|
112 |
C |
p. |
artikel |
63 |
Study on the mixing characteristics of circular transverse jet in crossflow
|
Li, Ziwan |
|
|
112 |
C |
p. |
artikel |
64 |
The application of support vector regression and mesh deformation technique in the optimization of transonic compressor design
|
Hu, Handuo |
|
|
112 |
C |
p. |
artikel |
65 |
The dynamic vortical flow behaviour on a coplanar canard configuration during large-amplitude-pitching
|
Chen, Qingmin |
|
|
112 |
C |
p. |
artikel |
66 |
Three-dimensional pore-scale study of the directional heat transfer in a high thermal conductivity carbon/carbon composite protection system
|
Wang, Hui |
|
|
112 |
C |
p. |
artikel |
67 |
Topological optimization design on constrained layer damping treatment for vibration suppression of aircraft panel via improved Evolutionary Structural Optimization
|
Zhang, Jingqi |
|
|
112 |
C |
p. |
artikel |
68 |
Using a CFD analysis of the flow capacity in a twin-entry turbine to develop a simplified physics-based model
|
Galindo, José |
|
|
112 |
C |
p. |
artikel |
69 |
Visualization of over-expanded supersonic wall-jet
|
S, Vaisakh |
|
|
112 |
C |
p. |
artikel |