| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Acoustic measurements of models of military style supersonic nozzle jets
|
Kuo, Ching-Wen
|
|
2014
|
27 |
1 |
p. 23-33
11 p.
|
artikel
|
| 2 |
A salient edges detection algorithm of multi-sensor images and its rapid calculation based on PFCM kernel clustering
|
Xu, Guili
|
|
2014
|
27 |
1 |
p. 102-109
8 p.
|
artikel
|
| 3 |
A spongy icing model for aircraft icing
|
Li, Xin
|
|
2014
|
27 |
1 |
p. 40-51
12 p.
|
artikel
|
| 4 |
A strategic flight conflict avoidance approach based on a memetic algorithm
|
Guan, Xiangmin
|
|
2014
|
27 |
1 |
p. 93-101
9 p.
|
artikel
|
| 5 |
A vision-based navigation approach with multiple radial shape marks for indoor aircraft locating
|
Zhou, Haoyin
|
|
2014
|
27 |
1 |
p. 76-84
9 p.
|
artikel
|
| 6 |
Collision risk-capacity tradeoff analysis of an en-route corridor model
|
Ye, Bojia
|
|
2014
|
27 |
1 |
p. 124-135
12 p.
|
artikel
|
| 7 |
Description of shape characteristics through Fourier and wavelet analysis
|
Yuan, Zhanwei
|
|
2014
|
27 |
1 |
p. 160-168
9 p.
|
artikel
|
| 8 |
Experimental study of partially-cured Z-pins reinforced foam core composites: K-Cor sandwich structures
|
Zheng, Yingying
|
|
2014
|
27 |
1 |
p. 153-159
7 p.
|
artikel
|
| 9 |
Flutter analysis of an airfoil with nonlinear damping using equivalent linearization
|
Chen, Feixin
|
|
2014
|
27 |
1 |
p. 59-64
6 p.
|
artikel
|
| 10 |
Generalized Kutta–Joukowski theorem for multi-vortex and multi-airfoil flow (a lumped vortex model)
|
Bai, Chenyuan
|
|
2014
|
27 |
1 |
p. 34-39
6 p.
|
artikel
|
| 11 |
IFC (Editorial Board)
|
|
|
2014
|
27 |
1 |
p. IFC-
1 p.
|
artikel
|
| 12 |
Multi-objective optimization of aircraft design for emission and cost reductions
|
Wang, Yu
|
|
2014
|
27 |
1 |
p. 52-58
7 p.
|
artikel
|
| 13 |
Precession–nutation correction for star tracker attitude measurement of STECE satellite
|
Lai, Yuwang
|
|
2014
|
27 |
1 |
p. 117-123
7 p.
|
artikel
|
| 14 |
Recent advance in nonlinear aeroelastic analysis and control of the aircraft
|
Xiang, Jinwu
|
|
2014
|
27 |
1 |
p. 12-22
11 p.
|
artikel
|
| 15 |
Robust fault detection and optimization for a network of unmanned vehicles with imperfect communication channels
|
Niu, Erzhuo
|
|
2014
|
27 |
1 |
p. 65-75
11 p.
|
artikel
|
| 16 |
Singular formalism and admissible control of spacecraft with rotating flexible solar array
|
Lu, Dongning
|
|
2014
|
27 |
1 |
p. 136-144
9 p.
|
artikel
|
| 17 |
Sliding mode control based guidance law with impact angle constraint
|
Zhao, Yao
|
|
2014
|
27 |
1 |
p. 145-152
8 p.
|
artikel
|
| 18 |
Survey of orbital dynamics and control of space rendezvous
|
Luo, Yazhong
|
|
2014
|
27 |
1 |
p. 1-11
11 p.
|
artikel
|
| 19 |
Testability integrated evaluation method based on testability virtual test data
|
Liu, Guanjun
|
|
2014
|
27 |
1 |
p. 85-92
8 p.
|
artikel
|
| 20 |
Theoretical study of flow ripple for an aviation axial-piston pump with damping holes in the valve plate
|
Guan, Changbin
|
|
2014
|
27 |
1 |
p. 169-181
13 p.
|
artikel
|
| 21 |
Two-stage open-loop velocity compensating method applied to multi-mass elastic transmission system
|
Zhang, Deli
|
|
2014
|
27 |
1 |
p. 182-188
7 p.
|
artikel
|
| 22 |
Weighted Marginal Fisher Analysis with Spatially Smooth for aircraft recognition
|
Wei, Zhenzhong
|
|
2014
|
27 |
1 |
p. 110-116
7 p.
|
artikel
|
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