nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A new observer-based chattering-free sliding mode guidance law
|
Behnamgol, Vahid |
|
2016 |
230 |
8 |
p. 1486-1495 |
artikel |
2 |
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
|
Xiao, Yabin |
|
2016 |
230 |
8 |
p. 1496-1506 |
artikel |
3 |
Investigation of adding fins to external stores for improving the flutter characteristics of a wing/store configuration
|
Amoozgar, MR |
|
2016 |
230 |
8 |
p. 1507-1517 |
artikel |
4 |
Multiobjective optimization for collision avoidance maneuver using a genetic algorithm
|
Seong, Jae-Dong |
|
2016 |
230 |
8 |
p. 1438-1447 |
artikel |
5 |
Nonlinear dynamic modeling in low frequency and control system stability domain determination for a LPE
|
Jafargholi, Ali |
|
2016 |
230 |
8 |
p. 1467-1485 |
artikel |
6 |
Numerical investigation of plasma actuated and non-actuated Gurney flaps on aerodynamic characteristics of a plunging airfoil
|
MahboubiDoust, A |
|
2016 |
230 |
8 |
p. 1423-1437 |
artikel |
7 |
Numerical modeling of adhesively bonded composite patch repair of cracked aluminum panels with concept of CZM and XFEM
|
Talebi, Behnam |
|
2016 |
230 |
8 |
p. 1448-1466 |
artikel |
8 |
Numerical study of passive cavity control on high-pressure ratio single expansion ramp nozzle under over-expansion condition
|
Zhou, Li |
|
2016 |
230 |
8 |
p. 1409-1422 |
artikel |
9 |
Optimisation of a 180° U-shaped bend shape for a turbine blade cooling passage leading to a pressure loss coefficient of approximately 0.6
|
Namgoong, Howoong |
|
2016 |
230 |
8 |
p. 1371-1384 |
artikel |
10 |
Parametric reduced-order model approach for simulation and optimization of aeroelastic systems with structural nonlinearities
|
Castellani, Michele |
|
2016 |
230 |
8 |
p. 1359-1370 |
artikel |
11 |
Pose measurement of nozzle based on laser range finders for capturing satellite
|
Zhang, Yu |
|
2016 |
230 |
8 |
p. 1385-1396 |
artikel |
12 |
Research on generalized inertial navigation system damping technology based on dual-model mean
|
Hongyang, He |
|
2016 |
230 |
8 |
p. 1518-1527 |
artikel |
13 |
The design and performance evaluation of axial ventilator with honeycomb in the turbofan engine lubrication system
|
Jingyu, Zhao |
|
2016 |
230 |
8 |
p. 1397-1408 |
artikel |