nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Active Fault Tolerant Control with self-enrichment capability for gas turbine engines
|
Mohammadi, Ehsan |
|
2016 |
56 |
C |
p. 70-89 20 p. |
artikel |
2 |
Aerodynamic force and vortex structures of flapping flexible hawkmoth-like wings
|
Ryu, YeongGyun |
|
2016 |
56 |
C |
p. 183-196 14 p. |
artikel |
3 |
A modular RANS approach for modeling hypersonic flow transition on a scramjet-forebody configuration
|
Wang, Liang |
|
2016 |
56 |
C |
p. 112-124 13 p. |
artikel |
4 |
Analytical study on the synthetic jet control of asymmetric flow field of flying wing unmanned aerial vehicle
|
Xu, Xiaoping |
|
2016 |
56 |
C |
p. 90-99 10 p. |
artikel |
5 |
An applicable formula for elastic buckling of rectangular plates under biaxial and shear loads
|
Jahanpour, Alireza |
|
2016 |
56 |
C |
p. 100-111 12 p. |
artikel |
6 |
A robust back-stepping based trajectory tracking controller for the tanker with strict posture constraints under unknown flow perturbations
|
Su, Zikang |
|
2016 |
56 |
C |
p. 34-45 12 p. |
artikel |
7 |
A simple extension of digital filter-based turbulent inflow to non-uniform structured grids
|
Dhamankar, N.S. |
|
2016 |
56 |
C |
p. 29-33 5 p. |
artikel |
8 |
ATLAS IV wing aerodynamic design: From conceptual approach to detailed optimization
|
Kontogiannis, S.G. |
|
2016 |
56 |
C |
p. 135-147 13 p. |
artikel |
9 |
Attitude tracking control for spacecraft with robust adaptive RBFNN augmenting sliding mode control
|
Zou, Yao |
|
2016 |
56 |
C |
p. 197-204 8 p. |
artikel |
10 |
Determination of stratospheric component behaviour using Finite Element model updating
|
Peeters, J. |
|
2016 |
56 |
C |
p. 22-28 7 p. |
artikel |
11 |
Dynamic extended high order sandwich panel theory for transient response of sandwich beams with carbon nanotube reinforced face sheets
|
Jedari Salami, S. |
|
2016 |
56 |
C |
p. 56-69 14 p. |
artikel |
12 |
Editorial Board
|
|
|
2016 |
56 |
C |
p. IFC- 1 p. |
artikel |
13 |
Effect of environmental radiation on the long-wave infrared signature of cruise aircraft
|
Huang, Wei |
|
2016 |
56 |
C |
p. 125-134 10 p. |
artikel |
14 |
Formation of vortices on a tubercled wing, and their effects on drag
|
Bolzon, Michael D.P. |
|
2016 |
56 |
C |
p. 46-55 10 p. |
artikel |
15 |
Influence of nature of core on vibro acoustic behavior of sandwich aerospace structures
|
Arunkumar, M.P. |
|
2016 |
56 |
C |
p. 155-167 13 p. |
artikel |
16 |
Investigation of boundary-layer ejecting for resistance to back pressure in an isolator
|
He, Yubao |
|
2016 |
56 |
C |
p. 1-13 13 p. |
artikel |
17 |
Mathematical relationship between mean cable tensions and structural parameters of deployable reflectors
|
Li, Tuanjie |
|
2016 |
56 |
C |
p. 205-211 7 p. |
artikel |
18 |
Meteoroid environment on the transfer trajectories to Mars
|
Marčeta, Dušan |
|
2016 |
56 |
C |
p. 14-21 8 p. |
artikel |
19 |
Mixing and combustion modeling of hydrogen peroxide/kerosene shear-coaxial jet flame in lab-scale rocket engine
|
Li, Sen |
|
2016 |
56 |
C |
p. 148-154 7 p. |
artikel |
20 |
Nonlinear dynamic analysis of the interaction between a two-dimensional rubberlike membrane and a liquid in a rectangular tank
|
Parasil, Worawat |
|
2016 |
56 |
C |
p. 212-222 11 p. |
artikel |
21 |
Supercritical wing design based on airfoil optimization and 2.75D transformation
|
Zhao, Tong |
|
2016 |
56 |
C |
p. 168-182 15 p. |
artikel |