| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
An adaptive sequential experiment design method for model validation
|
FANG, Ke
|
|
|
33 |
6 |
p. 1661-1672
|
artikel
|
| 2 |
A new online modelling method for aircraft engine state space model
|
PANG, Shuwei
|
|
|
33 |
6 |
p. 1756-1773
|
artikel
|
| 3 |
A new structural reliability analysis method in presence of mixed uncertainty variables
|
YOU, Lingfei
|
|
|
33 |
6 |
p. 1673-1682
|
artikel
|
| 4 |
A novel variable structure multi-model approach based on error-ambiguity decomposition
|
SHEN-TU, Han
|
|
|
33 |
6 |
p. 1731-1746
|
artikel
|
| 5 |
Application of a PCA-DBN-based surrogate model to robust aerodynamic design optimization
|
TAO, Jun
|
|
|
33 |
6 |
p. 1573-1588
|
artikel
|
| 6 |
Application of improved active disturbance rejection control algorithm in tilt quad rotor
|
WANG, Zhigang
|
|
|
33 |
6 |
p. 1625-1641
|
artikel
|
| 7 |
Corrosion mechanism investigation of TiN/Ti coating and TC4 alloy for aircraft compressor application
|
SUN, Zhiping
|
|
|
33 |
6 |
p. 1824-1835
|
artikel
|
| 8 |
Cross-sectional deformation behavior of double-ridged rectangular tube with fillers in different stages of H-typed bending
|
LIU, Chunmei
|
|
|
33 |
6 |
p. 1799-1811
|
artikel
|
| 9 |
Cross-sectional deformation of H96 brass double-ridged rectangular tube in rotary draw bending process with different yield criteria
|
XIA, Yangyang
|
|
|
33 |
6 |
p. 1788-1798
|
artikel
|
| 10 |
Editorial Board
|
|
|
|
33 |
6 |
p. ii
|
artikel
|
| 11 |
Evaluation of thermal effects on temperature-sensitive operating force of flow servo valve for fuel metering unit
|
ZHANG, Yang
|
|
|
33 |
6 |
p. 1812-1823
|
artikel
|
| 12 |
Experimental study on plasma jet deflection and energy extraction with MHD control
|
ZHAO, Kai
|
|
|
33 |
6 |
p. 1602-1610
|
artikel
|
| 13 |
Fluid structure interaction simulation of supersonic parachute inflation by an interface tracking method
|
YANG, Xue
|
|
|
33 |
6 |
p. 1692-1702
|
artikel
|
| 14 |
Hybrid integration method for highly maneuvering radar target detection based on a Markov motion model
|
ZHAO, Yingxiao
|
|
|
33 |
6 |
p. 1717-1730
|
artikel
|
| 15 |
Inside Front Cover - Aims & Scope, Copyright, Publication information, Orders & Claims, Advertising information, Author inquiries, Permissions, Funding body, Permanence of paper, Impressum (German titles only) and GFA link in double column
|
|
|
|
33 |
6 |
p. IFC
|
artikel
|
| 16 |
Inverted decoupling and LMI-based controller design for a turboprop engine with actuator dynamics
|
CHEN, Huairong
|
|
|
33 |
6 |
p. 1774-1787
|
artikel
|
| 17 |
Investigation on nonlinear lateral-torsional coupled vibration of a rotor system with substantial unbalance
|
HONG, Jie
|
|
|
33 |
6 |
p. 1642-1660
|
artikel
|
| 18 |
Model-free adaptive optimal design for trajectory tracking control of rocket-powered vehicle
|
NIE, Wenming
|
|
|
33 |
6 |
p. 1703-1716
|
artikel
|
| 19 |
Multi-block SSD based on small object detection for UAV railway scene surveillance
|
LI, Yundong
|
|
|
33 |
6 |
p. 1747-1755
|
artikel
|
| 20 |
NO x emissions of turbofan powered unmanned aerial vehicle for complete flight cycle
|
DINC, Ali
|
|
|
33 |
6 |
p. 1683-1691
|
artikel
|
| 21 |
Numerical exploration on the thermal invasion characteristics of two typical gap-cavity structures subjected to hypersonic airflow
|
LI, Zhenhuan
|
|
|
33 |
6 |
p. 1589-1601
|
artikel
|
| 22 |
Numerical simulation of compression corner flows at Mach number 9
|
PASHA, Amjad A.
|
|
|
33 |
6 |
p. 1611-1624
|
artikel
|
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