| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active monitoring and vibration control of smart structure aircraft based on FBG sensors and PZT actuators
|
Gao, Zhiyuan
|
|
2017
|
63 |
C |
p. 101-109
|
artikel
|
| 2 |
Additive manufacturing in unmanned aerial vehicles (UAVs): Challenges and potential
|
Goh, G.D.
|
|
2017
|
63 |
C |
p. 140-151
|
artikel
|
| 3 |
Aerodynamic design of an ultra-low rotating speed geared fan
|
Zhang, Jinhuan
|
|
2017
|
63 |
C |
p. 73-81
|
artikel
|
| 4 |
A fast multi-objective optimization design method for emergency libration point orbits transfer between the Sun–Earth and the Earth–Moon systems
|
Wang, Wei
|
|
2017
|
63 |
C |
p. 152-166
|
artikel
|
| 5 |
An investigation on supersonic bevelled nozzle jets
|
Wu, Jie
|
|
2017
|
63 |
C |
p. 278-293
|
artikel
|
| 6 |
Automated thermal and stress preliminary analyses applied to a turbine rotor
|
Moret, Maxime
|
|
2017
|
63 |
C |
p. 123-131
|
artikel
|
| 7 |
Behaviour of trailing wing(s) in echelon formation due to wing twist and aspect ratio
|
M., Gunasekaran
|
|
2017
|
63 |
C |
p. 294-303
|
artikel
|
| 8 |
Design optimization of a three-dimensional diffusing S-duct using a modified SST turbulent model
|
Gan, Wenbiao
|
|
2017
|
63 |
C |
p. 63-72
|
artikel
|
| 9 |
Distributed real-time non-linear receding horizon control methodology for multi-agent consensus problems
|
Sun, Fei
|
|
2017
|
63 |
C |
p. 82-90
|
artikel
|
| 10 |
Dynamic optimal output feedback control of satellite formation reconfiguration based on an LMI approach
|
Wei, Changzhu
|
|
2017
|
63 |
C |
p. 214-231
|
artikel
|
| 11 |
Editorial Board
|
|
|
2017
|
63 |
C |
p. IFC
|
artikel
|
| 12 |
Evaluation of forming forces in ultrasonic incremental sheet metal forming
|
Li, Pengyang
|
|
2017
|
63 |
C |
p. 132-139
|
artikel
|
| 13 |
Expected drag minimization for aerodynamic design optimization based on aircraft operational data
|
Liem, Rhea P.
|
|
2017
|
63 |
C |
p. 344-362
|
artikel
|
| 14 |
Experimental and 3D CFD analysis on optimization of geometrical parameters of parallel vortex tube cyclone separator
|
Rafiee, Seyed Ehsan
|
|
2017
|
63 |
C |
p. 110-122
|
artikel
|
| 15 |
Formation of near-Chapman–Jouguet oblique detonation wave over a dual-angle ramp
|
Bhattrai, Sudip
|
|
2017
|
63 |
C |
p. 1-8
|
artikel
|
| 16 |
Form-finding design of cable-mesh reflector antennas with minimal length configuration
|
Yang, Guigeng
|
|
2017
|
63 |
C |
p. 9-17
|
artikel
|
| 17 |
Free vibration analysis of a hard-coating cantilever cylindrical shell with elastic constraints
|
Sun, Wei
|
|
2017
|
63 |
C |
p. 232-244
|
artikel
|
| 18 |
Hygrothermal analysis of laminated composite plates in terms of an improved C0-type global–local model
|
Jin, Qilin
|
|
2017
|
63 |
C |
p. 328-343
|
artikel
|
| 19 |
Individual stress determination in irregularly perforated unsymmetrically-loaded structures from temperature data
|
Samad, W.A.
|
|
2017
|
63 |
C |
p. 91-99
|
artikel
|
| 20 |
Influence of the presence of defects on the adhesive layer for the single-lap bonded joint—Part II: Probabilistic assessment of the critical state
|
Elhannani, M.
|
|
2017
|
63 |
C |
p. 372-386
|
artikel
|
| 21 |
Iterative update correction and multi-frame state extraction based probability hypothesis density filter
|
Zhang, Huanqing
|
|
2017
|
63 |
C |
p. 54-62
|
artikel
|
| 22 |
LES study on the shape effect of ground obstacles on wake vortex dissipation
|
Wang, C.H. John
|
|
2017
|
63 |
C |
p. 245-258
|
artikel
|
| 23 |
Nonlinear aeroelastic scaling of high aspect-ratio wings
|
Spada, Christian
|
|
2017
|
63 |
C |
p. 363-371
|
artikel
|
| 24 |
Nonlinear control of sway in a tethered satellite system via attitude control of the main satellite
|
Yousefian, Peyman
|
|
2017
|
63 |
C |
p. 317-327
|
artikel
|
| 25 |
Nonlinear vibrations and stability analysis of a rotor on high-static-low-dynamic-stiffness supports using method of multiple scales
|
Navazi, H.M.
|
|
2017
|
63 |
C |
p. 259-265
|
artikel
|
| 26 |
Numerical investigation of a HPT with different rotor tip configurations in terms of pressure ratio and efficiency
|
da Silva, Lucilene Moraes
|
|
2017
|
63 |
C |
p. 33-40
|
artikel
|
| 27 |
Numerical investigation of characteristic frequency excited highly underexpanded jets
|
Li, Xiaopeng
|
|
2017
|
63 |
C |
p. 304-316
|
artikel
|
| 28 |
Online optimal midcourse trajectory modification algorithm for hypersonic vehicle interceptions
|
Zhou, Jin
|
|
2017
|
63 |
C |
p. 266-277
|
artikel
|
| 29 |
Optimal recursive estimation for networked descriptor systems with packet dropouts, multiplicative noises and correlated noises
|
Wang, Xin
|
|
2017
|
63 |
C |
p. 41-53
|
artikel
|
| 30 |
Optimum active twist input scenario for performance improvement and vibration reduction of a helicopter rotor
|
You, Younghyun
|
|
2017
|
63 |
C |
p. 18-32
|
artikel
|
| 31 |
Reduced order unsteady aerodynamic model of a rigid aerofoil in gust encounters
|
Zhou, Qiang
|
|
2017
|
63 |
C |
p. 203-213
|
artikel
|
| 32 |
Reply “Comment on the paper “Nonlinear radiation effects on squeezing flow of a Casson fluid between parallel disks, Syed Tauseef Mohyud-Din, Sheikh Irfanullah Khan, Aerospace Science and Technology 48 (2016) 186–192”
|
Mohyud-Din, Syed Tauseef
|
|
2017
|
63 |
C |
p. 100
|
artikel
|
| 33 |
Tether tension control law design during orbital transfer via small-gain theorem
|
Liu, Helong
|
|
2017
|
63 |
C |
p. 191-202
|
artikel
|
| 34 |
Three-dimensional compressor blading design improvements in low-speed model testing
|
Zhang, Chenkai
|
|
2017
|
63 |
C |
p. 179-190
|
artikel
|
| 35 |
Unsteady aerodynamic and optimal kinematic analysis of a micro flapping wing rotor
|
Li, H.
|
|
2017
|
63 |
C |
p. 167-178
|
artikel
|
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