| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A design analysis of vertical stabilisers for Blended Wing Body aircraft
|
Larkin, Geoffrey
|
|
2017
|
64 |
C |
p. 237-252
16 p.
|
artikel
|
| 2 |
An adaptive fully-Lagrangian meshless method for incompressible laminar flow airfoil studies
|
Khorasanizade, Sh.
|
|
2017
|
64 |
C |
p. 161-170
10 p.
|
artikel
|
| 3 |
An approach of drag force decrease for combined cylinder AD bodies under the action of microwave and laser energy deposition
|
Azarova, O.A.
|
|
2017
|
64 |
C |
p. 154-160
7 p.
|
artikel
|
| 4 |
A robust nonlinear output feedback control method for limit cycle oscillation suppression using synthetic jet actuators
|
Ramos-Pedroza, Natalie
|
|
2017
|
64 |
C |
p. 16-23
8 p.
|
artikel
|
| 5 |
Bounded finite-time attitude tracking control for rigid spacecraft via output feedback
|
Zhang, Jian
|
|
2017
|
64 |
C |
p. 75-84
10 p.
|
artikel
|
| 6 |
Editorial Board
|
|
|
2017
|
64 |
C |
p. IFC-
1 p.
|
artikel
|
| 7 |
Effect of structural dynamic characteristics on fatigue and damage tolerance of aerospace grade composite materials
|
Anwar, Waqas
|
|
2017
|
64 |
C |
p. 39-51
13 p.
|
artikel
|
| 8 |
Guidance and control for high dynamic rotating artillery rockets
|
de Celis, Raúl
|
|
2017
|
64 |
C |
p. 204-212
9 p.
|
artikel
|
| 9 |
In-flight adaptive modeling using polynomial LPV approach for turbofan engine dynamic behavior
|
Lu, Feng
|
|
2017
|
64 |
C |
p. 223-236
14 p.
|
artikel
|
| 10 |
Modeling the electrostatic charging of a helicopter during hovering in dusty atmosphere
|
Grosshans, Holger
|
|
2017
|
64 |
C |
p. 31-38
8 p.
|
artikel
|
| 11 |
Multigrid cell-centered techniques for high-order incompressible flow numerical solutions
|
Mathioudakis, Emmanuel N.
|
|
2017
|
64 |
C |
p. 85-101
17 p.
|
artikel
|
| 12 |
Multi-objective reliability-based design optimization approach of complex structure with multi-failure modes
|
Song, Lu-Kai
|
|
2017
|
64 |
C |
p. 52-62
11 p.
|
artikel
|
| 13 |
Nonlinear vibration of compressed and thermally postbuckled nanotube-reinforced composite plates resting on elastic foundations
|
Shen, Hui-Shen
|
|
2017
|
64 |
C |
p. 63-74
12 p.
|
artikel
|
| 14 |
Numerical and experimental investigation of improving combustion performance of variable geometry dual-mode combustor
|
Feng, Shuo
|
|
2017
|
64 |
C |
p. 213-222
10 p.
|
artikel
|
| 15 |
Numerical simulations on the ERICA tiltrotor
|
Jimenez Garcia, Antonio
|
|
2017
|
64 |
C |
p. 171-191
21 p.
|
artikel
|
| 16 |
Radial basis function mesh deformation based on dynamic control points
|
Niu, Jianping
|
|
2017
|
64 |
C |
p. 122-132
11 p.
|
artikel
|
| 17 |
Robust dynamic output feedback control for attitude stabilization of spacecraft with nonlinear perturbations
|
Liu, Chuang
|
|
2017
|
64 |
C |
p. 102-121
20 p.
|
artikel
|
| 18 |
Self-evolving fuzzy model-based controller with online structure and parameter learning for hypersonic vehicle
|
Rong, Hai-Jun
|
|
2017
|
64 |
C |
p. 1-15
15 p.
|
artikel
|
| 19 |
Simulation of the dynamic response of GLARE plates subjected to low velocity impact using a linearized spring–mass model
|
Bikakis, George S.E.
|
|
2017
|
64 |
C |
p. 24-30
7 p.
|
artikel
|
| 20 |
Supporting system interference on aerodynamic characteristics of an aircraft model in a low-speed wind tunnel
|
Ocokoljić, Goran
|
|
2017
|
64 |
C |
p. 133-146
14 p.
|
artikel
|
| 21 |
Wing geometry and kinematic parameters optimization of flapping wing hovering flight for minimum energy
|
Ke, Xijun
|
|
2017
|
64 |
C |
p. 192-203
12 p.
|
artikel
|
| 22 |
X-ray pulsar signal de-noising for impulse noise using wavelet packet
|
Xiuping, Liu
|
|
2017
|
64 |
C |
p. 147-153
7 p.
|
artikel
|
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