| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Adaptive decoupling synchronous control of dissimilar redundant actuation system for large civil aircraft
|
Shi, Cun
|
|
2015
|
47 |
C |
p. 114-124
11 p.
|
artikel
|
| 2 |
A full engine cycle analysis of a turbofan engine for optimum scheduling of variable guide vanes
|
Kim, Sangjo
|
|
2015
|
47 |
C |
p. 21-30
10 p.
|
artikel
|
| 3 |
An airplane jig shape design method based on high fidelity aeroelastic simulation
|
Yang, Wei
|
|
2015
|
47 |
C |
p. 314-323
10 p.
|
artikel
|
| 4 |
An improved micro-vortex generator in supersonic flows
|
Zhang, Binbin
|
|
2015
|
47 |
C |
p. 210-215
6 p.
|
artikel
|
| 5 |
A nonaxisymmetric endwall design approach and its computational assessment in the NGV of an HP turbine stage
|
Turgut, Özhan H.
|
|
2015
|
47 |
C |
p. 456-466
11 p.
|
artikel
|
| 6 |
Automatic mode tracking for flight dynamic analysis using a spanning algorithm
|
Beaverstock, C.S.
|
|
2015
|
47 |
C |
p. 54-67
14 p.
|
artikel
|
| 7 |
Cooperative simultaneous attack of multi-missiles under unreliable and noisy communication network: A consensus scheme of impact time
|
Song, Lei
|
|
2015
|
47 |
C |
p. 31-41
11 p.
|
artikel
|
| 8 |
Corrosion fatigue performance of TC4 plates with holes in aviation kerosene
|
Liu, Jun
|
|
2015
|
47 |
C |
p. 420-424
5 p.
|
artikel
|
| 9 |
Design, implementation and flight testing of advanced RNP to SBAS LPV approaches in Germany
|
Dautermann, Thomas
|
|
2015
|
47 |
C |
p. 280-290
11 p.
|
artikel
|
| 10 |
Design of a hybrid carbon fibre/carbon nanotube composite for enhanced lightning strike resistance
|
Ma, Xiang
|
|
2015
|
47 |
C |
p. 367-377
11 p.
|
artikel
|
| 11 |
Design of the H ∞ robust control for the piezoelectric actuator based on chaos optimization algorithm
|
E, Jiaqiang
|
|
2015
|
47 |
C |
p. 238-246
9 p.
|
artikel
|
| 12 |
Determination of fracture toughness and fatigue crack growth rate using circumferentially cracked round bar specimens of Al2014T651
|
Neelakantha, V.L.
|
|
2015
|
47 |
C |
p. 92-97
6 p.
|
artikel
|
| 13 |
Direction and surface sampling in ray tracing for spacecraft radiative heat transfer
|
Jacques, Lionel
|
|
2015
|
47 |
C |
p. 146-153
8 p.
|
artikel
|
| 14 |
Dynamics analysis of flexible space robot with joint friction
|
Liu, Xiaofeng
|
|
2015
|
47 |
C |
p. 164-176
13 p.
|
artikel
|
| 15 |
Editorial Board
|
|
|
2015
|
47 |
C |
p. IFC-
1 p.
|
artikel
|
| 16 |
Effect of semi-open impeller side clearance on the centrifugal pump performance using CFD
|
Ayad, A. Farid
|
|
2015
|
47 |
C |
p. 247-255
9 p.
|
artikel
|
| 17 |
False alarm rate of the GLRT-LQ detector in non-Gaussian and heterogeneous clutter
|
Zhang, Zi-Jing
|
|
2015
|
47 |
C |
p. 191-194
4 p.
|
artikel
|
| 18 |
Fault detection and isolation for a small CMG-based satellite: A fuzzy Q-learning approach
|
Choi, Young-Cheol
|
|
2015
|
47 |
C |
p. 340-355
16 p.
|
artikel
|
| 19 |
Hardware-in-the-loop environment for verification of a small satellite's on-board software
|
Fritz, Michael
|
|
2015
|
47 |
C |
p. 388-395
8 p.
|
artikel
|
| 20 |
Heat balance evaluation of double-base solid propellant combustion using thermography and laser heating on a burning surface
|
Kakami, Akira
|
|
2015
|
47 |
C |
p. 86-91
6 p.
|
artikel
|
| 21 |
Helicopter drag reduction by vortex generators
|
Gibertini, G.
|
|
2015
|
47 |
C |
p. 324-339
16 p.
|
artikel
|
| 22 |
Indirect adaptive control for attitude tracking of spacecraft with unknown reaction wheel friction
|
Cao, Xibin
|
|
2015
|
47 |
C |
p. 493-500
8 p.
|
artikel
|
| 23 |
Leader-following formation control of quadcopters with heading synchronization
|
Mahmood, Arshad
|
|
2015
|
47 |
C |
p. 68-74
7 p.
|
artikel
|
| 24 |
Low velocity impact and quasi-static in-plane loading on a graded honeycomb structure; experimental, analytical and numerical study
|
Galehdari, S.A.
|
|
2015
|
47 |
C |
p. 425-433
9 p.
|
artikel
|
| 25 |
Mathematical modeling and control of a tilt-rotor aircraft
|
Wang, Xinhua
|
|
2015
|
47 |
C |
p. 473-492
20 p.
|
artikel
|
| 26 |
Nonlinear aerodynamic reduced order modeling by discrete time recurrent neural networks
|
Mannarino, Andrea
|
|
2015
|
47 |
C |
p. 406-419
14 p.
|
artikel
|
| 27 |
Non-linear transient and damping analysis of a long cylindrical sandwich panel with embedded SMA wires
|
Khanjani, M.
|
|
2015
|
47 |
C |
p. 98-113
16 p.
|
artikel
|
| 28 |
Nonlinear vibration of FGM doubly curved panels resting on elastic foundations in thermal environments
|
Shen, Hui-Shen
|
|
2015
|
47 |
C |
p. 434-446
13 p.
|
artikel
|
| 29 |
Numerical investigation of flow structures around a cylindrical afterbody under supersonic condition
|
Das, Pratik
|
|
2015
|
47 |
C |
p. 195-209
15 p.
|
artikel
|
| 30 |
Numerical investigation of three-dimensional effects during dynamic stall
|
Costes, M.
|
|
2015
|
47 |
C |
p. 216-237
22 p.
|
artikel
|
| 31 |
OARPER-MAFO algorithm for anti-ship missile path planning
|
Liu, Gang
|
|
2015
|
47 |
C |
p. 135-145
11 p.
|
artikel
|
| 32 |
On dynamic stiffness of spacecraft flexible appendages in deployment phase
|
Bagheri Ghaleh, P.
|
|
2015
|
47 |
C |
p. 1-9
9 p.
|
artikel
|
| 33 |
On vibrational behavior of pulse detonation engine tubes
|
Mirzaei, M.
|
|
2015
|
47 |
C |
p. 177-190
14 p.
|
artikel
|
| 34 |
Optimal redundant sensor configuration for accuracy increasing in space inertial navigation system
|
Jafari, Mehdi
|
|
2015
|
47 |
C |
p. 467-472
6 p.
|
artikel
|
| 35 |
Optimal scheduling of multiple geosynchronous satellites refueling based on a hybrid particle swarm optimizer
|
Zhou, Yang
|
|
2015
|
47 |
C |
p. 125-134
10 p.
|
artikel
|
| 36 |
Performance and lifetime testing of a pulsed plasma thruster for Cubesat applications
|
Ciaralli, S.
|
|
2015
|
47 |
C |
p. 291-298
8 p.
|
artikel
|
| 37 |
Preliminary analysis of scramjet engines based on engineering models
|
Rolim, Tiago C.
|
|
2015
|
47 |
C |
p. 256-268
13 p.
|
artikel
|
| 38 |
Real-time path planning of unmanned aerial vehicle for target tracking and obstacle avoidance in complex dynamic environment
|
Yao, Peng
|
|
2015
|
47 |
C |
p. 269-279
11 p.
|
artikel
|
| 39 |
Robust hazard matching approach for visual navigation application in planetary landing
|
Yu, Meng
|
|
2015
|
47 |
C |
p. 378-387
10 p.
|
artikel
|
| 40 |
Sensitivity of trajectory stability estimated by Lyapunov characteristic exponents
|
Masarati, Pierangelo
|
|
2015
|
47 |
C |
p. 501-510
10 p.
|
artikel
|
| 41 |
Solving the maximum-crossrange problem via successive second-order cone programming with a line search
|
Liu, Xinfu
|
|
2015
|
47 |
C |
p. 10-20
11 p.
|
artikel
|
| 42 |
Stability of thin FGM microplate subjected to mechanical and thermal loading based on the modified couple stress theory and spline finite strip method
|
Mirsalehi, Maryam
|
|
2015
|
47 |
C |
p. 356-366
11 p.
|
artikel
|
| 43 |
Supersonic flutter of laminated composite panel in coupled multi-fields
|
Zhao, Hai
|
|
2015
|
47 |
C |
p. 75-85
11 p.
|
artikel
|
| 44 |
Thermal buckling of temperature dependent FG-CNT reinforced composite conical shells
|
Mirzaei, M.
|
|
2015
|
47 |
C |
p. 42-53
12 p.
|
artikel
|
| 45 |
The self-excited rolling oscillations induced by fore-body vortices
|
Ma, Bao-Feng
|
|
2015
|
47 |
C |
p. 299-313
15 p.
|
artikel
|
| 46 |
Unsteady pressure distributions at the wind tunnel model of a pitching Lambda wing with development of vortical flow
|
Wiggen, Stefan
|
|
2015
|
47 |
C |
p. 396-405
10 p.
|
artikel
|
| 47 |
Vector Fourier transform analysis of stacked rectangular microstrip patches on isotropic and anisotropic substrates
|
Bouraiou, A.
|
|
2015
|
47 |
C |
p. 447-455
9 p.
|
artikel
|
| 48 |
Visualization studies of the spray from swirl injectors under elevated ambient pressure
|
Fu, Qing-fei
|
|
2015
|
47 |
C |
p. 154-163
10 p.
|
artikel
|
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