no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
1 |
A dynamic mode decomposition of the saturation process in the open cavity flow
|
Vinha, N. |
|
2016 |
52 |
C |
p. 198-206 9 p. |
article |
2 |
Aerodynamic database reconstruction via gappy high order singular value decomposition
|
Moreno, Ana I. |
|
2016 |
52 |
C |
p. 115-128 14 p. |
article |
3 |
Aerodynamic performance analysis of a winged re-entry vehicle from hypersonic down to subsonic speed
|
Pezzella, Giuseppe |
|
2016 |
52 |
C |
p. 129-143 15 p. |
article |
4 |
Aeroelastic behavior of composite laminated shells with embedded SMA wires under supersonic flow
|
Donadon, Maurício V. |
|
2016 |
52 |
C |
p. 157-166 10 p. |
article |
5 |
A new viewpoint on the mechanism of transonic single-degree-of-freedom flutter
|
Gao, Chuanqiang |
|
2016 |
52 |
C |
p. 144-156 13 p. |
article |
6 |
An improved multiple model particle filtering approach for manoeuvring target tracking using airborne GMTI with geographic information
|
Yu, Miao |
|
2016 |
52 |
C |
p. 62-69 8 p. |
article |
7 |
An inverse trigonometric shear deformation theory for supersonic flutter characteristics of multilayered composite plates
|
Grover, Neeraj |
|
2016 |
52 |
C |
p. 41-51 11 p. |
article |
8 |
Development of the ball-spine inverse design algorithm to swirling viscous flow for performance improvement of an axisymmetric bend duct
|
Shumal, Mohammad |
|
2016 |
52 |
C |
p. 181-188 8 p. |
article |
9 |
Editorial Board
|
|
|
2016 |
52 |
C |
p. IFC- 1 p. |
article |
10 |
Estimation of a launch vehicle stage fallout zone with parametric and non-parametric importance sampling algorithms in presence of uncertain input distributions
|
Morio, Jérôme |
|
2016 |
52 |
C |
p. 95-101 7 p. |
article |
11 |
Evaluation of the effectiveness of typical casing treatments for a low-speed compressor by an integral method
|
Nan, Xi |
|
2016 |
52 |
C |
p. 234-242 9 p. |
article |
12 |
Flutter suppression of plates subjected to supersonic flow using passive constrained viscoelastic layers and Golla–Hughes–McTavish method
|
Cunha-Filho, A.G. |
|
2016 |
52 |
C |
p. 70-80 11 p. |
article |
13 |
Hypervelocity ballistic reference models as experimental supersonic test cases
|
Damljanović, Dijana |
|
2016 |
52 |
C |
p. 189-197 9 p. |
article |
14 |
Improved zigzag theories for laminated composite and sandwich plates with interlaminar shear stress continuity
|
Suganyadevi Sarangan, |
|
2016 |
52 |
C |
p. 243-255 13 p. |
article |
15 |
Numerical characterization of helicopter noise hemispheres
|
Gennaretti, M. |
|
2016 |
52 |
C |
p. 18-28 11 p. |
article |
16 |
Numerical optimization for stator vane settings of multi-stage compressors based on neural networks and genetic algorithms
|
Li, Bo |
|
2016 |
52 |
C |
p. 81-94 14 p. |
article |
17 |
Numerical study on effect of air throttling on combustion mode formation and transition in a dual-mode scramjet combustor
|
Tian, Ye |
|
2016 |
52 |
C |
p. 173-180 8 p. |
article |
18 |
On the validation of experimental results for the dynamic stability of re-entry capsules
|
Monteiro, João |
|
2016 |
52 |
C |
p. 224-233 10 p. |
article |
19 |
Parametric reduced order model approach for rapid dynamic loads prediction
|
Castellani, Michele |
|
2016 |
52 |
C |
p. 29-40 12 p. |
article |
20 |
Rigid-flexible-thermal coupling dynamic formulation for satellite and plate multibody system
|
Liu, Jinyang |
|
2016 |
52 |
C |
p. 102-114 13 p. |
article |
21 |
Robust off-line control allocation
|
de Almeida, Fabio A. |
|
2016 |
52 |
C |
p. 1-9 9 p. |
article |
22 |
Role of tip injection in desensitizing the compressor to the tip clearance size
|
Khaleghi, Hossein |
|
2016 |
52 |
C |
p. 10-17 8 p. |
article |
23 |
Study on real-time identification of GNSS multipath errors and its application
|
Zhu, Zhuangsheng |
|
2016 |
52 |
C |
p. 215-223 9 p. |
article |
24 |
Survivability to orbital debris of tape tethers for end-of-life spacecraft de-orbiting
|
Khan, Shaker Bayajid |
|
2016 |
52 |
C |
p. 167-172 6 p. |
article |
25 |
The effects of cross section variations on the pressure distribution around a long axisymmetric body
|
Heidari, Mohammad Reza |
|
2016 |
52 |
C |
p. 256-268 13 p. |
article |
26 |
Waypoint constrained guidance for entry vehicles
|
Liang, Zixuan |
|
2016 |
52 |
C |
p. 52-61 10 p. |
article |
27 |
XFOIL vs CFD performance predictions for high lift low Reynolds number airfoils
|
Morgado, J. |
|
2016 |
52 |
C |
p. 207-214 8 p. |
article |