nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Adaptive optimization methodology based on Kriging modeling and a trust region method
|
LI, Chunna |
|
2019 |
32 |
2 |
p. 281-295 |
artikel |
2 |
A data-driven health indicator extraction method for aircraft air conditioning system health monitoring
|
SUN, Jianzhong |
|
2019 |
32 |
2 |
p. 409-416 |
artikel |
3 |
Aircraft engine fault detection based on grouped convolutional denoising autoencoders
|
FU, Xuyun |
|
2019 |
32 |
2 |
p. 296-307 |
artikel |
4 |
A model-based prognostics method for fatigue crack growth in fuselage panels
|
WANG, Yiwei |
|
2019 |
32 |
2 |
p. 396-408 |
artikel |
5 |
An efficient analytical homogenization technique for mechanical-hygrothermal responses of unidirectional composites with applications to optimization and multiscale analyses
|
WANG, Guannan |
|
2019 |
32 |
2 |
p. 382-395 |
artikel |
6 |
A novel unified model predicting flow stress and grain size evolutions during hot working of non-uniform as-cast 42CrMo billets
|
GUO, Lianggang |
|
2019 |
32 |
2 |
p. 531-545 |
artikel |
7 |
A review of chatter vibration research in milling
|
YUE, Caixu |
|
2019 |
32 |
2 |
p. 215-242 |
artikel |
8 |
A two-step weighted least-squares method for joint estimation of source and sensor locations: A general framework
|
WANG, Ding |
|
2019 |
32 |
2 |
p. 417-443 |
artikel |
9 |
Behavior and functional modeling methods of doubly salient electromagnetic generators for aircraft electrical power system applications
|
XU, Yanwu |
|
2019 |
32 |
2 |
p. 477-488 |
artikel |
10 |
Conceptual design and optimization of a tilt-rotor micro air vehicle
|
HASSANALIAN, M. |
|
2019 |
32 |
2 |
p. 369-381 |
artikel |
11 |
Editorial Board
|
|
|
2019 |
32 |
2 |
p. ii |
artikel |
12 |
Effects of splined shaft bending rigidity on cylinder tilt behaviour for high-speed electro-hydrostatic actuator pumps
|
ZHANG, Junhui |
|
2019 |
32 |
2 |
p. 499-512 |
artikel |
13 |
Effects of yaw-roll coupling ratio on lateral-directional aerodynamic characteristics
|
SHEN, Lin |
|
2019 |
32 |
2 |
p. 272-280 |
artikel |
14 |
Efficiency optimized fuel supply strategy of aircraft engine based on air-fuel ratio control
|
WANG, Yixuan |
|
2019 |
32 |
2 |
p. 489-498 |
artikel |
15 |
Event-triggered adaptive control for attitude tracking of spacecraft
|
WANG, Chenliang |
|
2019 |
32 |
2 |
p. 454-462 |
artikel |
16 |
Experimental study of rotating gliding arc discharge plasma-assisted combustion in an aero-engine combustion chamber
|
HE, Liming |
|
2019 |
32 |
2 |
p. 337-346 |
artikel |
17 |
Identification of the state-space model and payload mass parameter of a flexible space manipulator using a recursive subspace tracking method
|
NI, Zhiyu |
|
2019 |
32 |
2 |
p. 513-530 |
artikel |
18 |
Impact of reduced frequency on the time lag in pressure distribution over a supercritical airfoil in a pitch-pause-return motion
|
ESLAMI, Haghighat Z. |
|
2019 |
32 |
2 |
p. 243-252 |
artikel |
19 |
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
|
|
|
2019 |
32 |
2 |
p. IFC |
artikel |
20 |
Numerical study on flow control of ship airwake and rotor airload during helicopter shipboard landing
|
SHI, Yongjie |
|
2019 |
32 |
2 |
p. 324-336 |
artikel |
21 |
Predicting lean blow-off of bluffbody stabilized flames based on Damköhler number
|
WANG, Zhonghao |
|
2019 |
32 |
2 |
p. 308-323 |
artikel |
22 |
Reliable flight performance assessment of multirotor based on interacting multiple model particle filter and health degree
|
ZHAO, Zhiyao |
|
2019 |
32 |
2 |
p. 444-453 |
artikel |
23 |
Robust decentralized control design for aircraft engines: A fractional type
|
PAN, Muxuan |
|
2019 |
32 |
2 |
p. 347-360 |
artikel |
24 |
Safety assessment of approximate segregated parallel operation on closely spaced parallel runways
|
LIU, Fei |
|
2019 |
32 |
2 |
p. 463-476 |
artikel |
25 |
Service life prediction of AP/Al/HTPB solid rocket propellant with consideration of softening aging behavior
|
ADEL, Walid M. |
|
2019 |
32 |
2 |
p. 361-368 |
artikel |
26 |
Sliding mode control design for oblique wing aircraft in wing skewing process
|
YUE, Ting |
|
2019 |
32 |
2 |
p. 263-271 |
artikel |
27 |
Thermal state calculation of chamber in small thrust liquid rocket engine for steady state pulsed mode
|
VOROBYEV, Alexey Gennadievich |
|
2019 |
32 |
2 |
p. 253-262 |
artikel |