nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Aerodynamic performance enhancement of a flying wing using nanosecond pulsed DBD plasma actuator
|
Han, Menghu |
|
2015 |
28 |
2 |
p. 377-384 8 p. |
artikel |
2 |
Aerodynamic shape optimization for alleviating dynamic stall characteristics of helicopter rotor airfoil
|
Wang, Qing |
|
2015 |
28 |
2 |
p. 346-356 11 p. |
artikel |
3 |
A new landing impact attenuation seat in manned spacecraft biologically-inspired by felids
|
Yu, Hui |
|
2015 |
28 |
2 |
p. 434-446 13 p. |
artikel |
4 |
An inertial parameter identification method of eliminating system damping effect for a six-degree-of-freedom parallel manipulator
|
Tian, Tixian |
|
2015 |
28 |
2 |
p. 582-592 11 p. |
artikel |
5 |
An LMI-based decoupling control for electromagnetic formation flight
|
Huang, Xianlin |
|
2015 |
28 |
2 |
p. 508-517 10 p. |
artikel |
6 |
A novel fault tolerant permanent magnet synchronous motor with improved optimal torque control for aerospace application
|
Guo, Hong |
|
2015 |
28 |
2 |
p. 535-544 10 p. |
artikel |
7 |
Atomization mechanism of a charged viscoelastic liquid sheet
|
Liu, Lujia |
|
2015 |
28 |
2 |
p. 403-409 7 p. |
artikel |
8 |
Attitude coordination for spacecraft formation with multiple communication delays
|
Guo, Yaohua |
|
2015 |
28 |
2 |
p. 527-534 8 p. |
artikel |
9 |
A two-stage approach for managing actuators redundancy and its application to fault tolerant flight control
|
Zhong, Lunlong |
|
2015 |
28 |
2 |
p. 469-477 9 p. |
artikel |
10 |
Development of Kabila rocket: A radioisotope heated thermionic plasma rocket engine
|
Mboyi, Kalomba |
|
2015 |
28 |
2 |
p. 427-433 7 p. |
artikel |
11 |
Development process of muzzle flows including a gun-launched missile
|
Zhuo, Changfei |
|
2015 |
28 |
2 |
p. 385-393 9 p. |
artikel |
12 |
Drop test and crash simulation of a civil airplane fuselage section
|
Liu, Xiaochuan |
|
2015 |
28 |
2 |
p. 447-456 10 p. |
artikel |
13 |
Dynamics modeling and control of a transport aircraft for ultra-low altitude airdrop
|
Liu, Ri |
|
2015 |
28 |
2 |
p. 478-487 10 p. |
artikel |
14 |
Dynamic tensile behavior of AZ31B magnesium alloy at ultra-high strain rates
|
Geng, Changjian |
|
2015 |
28 |
2 |
p. 593-599 7 p. |
artikel |
15 |
Effects of cerium salts on corrosion behaviors of Si–Zr hybrid sol–gel coatings
|
Yu, Mei |
|
2015 |
28 |
2 |
p. 600-608 9 p. |
artikel |
16 |
Experimental investigation of laser peening on TiAl alloy microstructure and properties
|
Qiao, Hongchao |
|
2015 |
28 |
2 |
p. 609-616 8 p. |
artikel |
17 |
Experimental study of an aircraft fuel tank inerting system
|
Cai, Yan |
|
2015 |
28 |
2 |
p. 394-402 9 p. |
artikel |
18 |
Flow separation control on swept wing with nanosecond pulse driven DBD plasma actuators
|
Zhao, Guangyin |
|
2015 |
28 |
2 |
p. 368-376 9 p. |
artikel |
19 |
IFC (Editorial Board)
|
|
|
2015 |
28 |
2 |
p. IFC- 1 p. |
artikel |
20 |
Impulse feature extraction method for machinery fault detection using fusion sparse coding and online dictionary learning
|
Deng, Sen |
|
2015 |
28 |
2 |
p. 488-498 11 p. |
artikel |
21 |
Numerical analysis and optimization of boundary layer suction on airfoils
|
Shi, Yayun |
|
2015 |
28 |
2 |
p. 357-367 11 p. |
artikel |
22 |
Numerical simulation of RCS for carrier electronic warfare airplanes
|
Yue, Kuizhi |
|
2015 |
28 |
2 |
p. 545-555 11 p. |
artikel |
23 |
Practical compensation for nonlinear dynamic thrust measurement system
|
Chen, Lin |
|
2015 |
28 |
2 |
p. 418-426 9 p. |
artikel |
24 |
Response regimes of narrow-band stochastic excited linear oscillator coupled to nonlinear energy sink
|
Xiong, Huai |
|
2015 |
28 |
2 |
p. 457-468 12 p. |
artikel |
25 |
Robust control for constant thrust rendezvous under thrust failure
|
Qi, Yongqiang |
|
2015 |
28 |
2 |
p. 518-526 9 p. |
artikel |
26 |
Selective laser melting of Al–8.5Fe–1.3V–1.7Si alloy: Investigation on the resultant microstructure and hardness
|
Zheng, Lijing |
|
2015 |
28 |
2 |
p. 564-569 6 p. |
artikel |
27 |
Specific grinding energy and surface roughness of nanoparticle jet minimum quantity lubrication in grinding
|
Zhang, Dongkun |
|
2015 |
28 |
2 |
p. 570-581 12 p. |
artikel |
28 |
Strategic flight assignment approach based on multi-objective parallel evolution algorithm with dynamic migration interval
|
Zhang, Xuejun |
|
2015 |
28 |
2 |
p. 556-563 8 p. |
artikel |
29 |
Study of amplification coefficient in a water-cooling Gardon-type heat power measuring apparatus
|
Li, Miao |
|
2015 |
28 |
2 |
p. 410-417 8 p. |
artikel |
30 |
Transfer element method with application to acoustic design of aeroengine nacelle
|
Wang, Xiaoyu |
|
2015 |
28 |
2 |
p. 327-345 19 p. |
artikel |
31 |
UMR: A utility-maximizing routing algorithm for delay-sensitive service in LEO satellite networks
|
Lu, Yong |
|
2015 |
28 |
2 |
p. 499-507 9 p. |
artikel |