| no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
| 1 |
Adaptive decoupling control of hypersonic vehicle using fuzzy-neural network observer
|
Bai, Chen
|
|
2016
|
230 |
7 |
p. 1216-1223
|
article
|
| 2 |
Aerodynamic performance improvement of the UAS-S4 Éhecatl morphing airfoil using novel optimization techniques
|
Gabor, Oliviu Sugar
|
|
2016
|
230 |
7 |
p. 1164-1180
|
article
|
| 3 |
Aero engine compressor fouling effects for short- and long-haul missions
|
Igie, Uyioghosa
|
|
2016
|
230 |
7 |
p. 1312-1324
|
article
|
| 4 |
Aeroservoelastic modeling and analysis of a six-DOF hypersonic flight vehicle
|
Zong, Qun
|
|
2016
|
230 |
7 |
p. 1240-1251
|
article
|
| 5 |
A novel topology optimization method for composite beams
|
Ren, Yiru
|
|
2016
|
230 |
7 |
p. 1153-1163
|
article
|
| 6 |
Bifurcation analysis of the asymmetric rolling missiles
|
Sun, Huadong
|
|
2016
|
230 |
7 |
p. 1273-1283
|
article
|
| 7 |
Computational investigation of the flow structure over a pitching delta wing at supersonic speeds
|
Hadidoolabi, Mostafa
|
|
2016
|
230 |
7 |
p. 1334-1347
|
article
|
| 8 |
Experimental investigation of particle damper-based vibration suppression in printed circuit board for spacecraft applications
|
Veeramuthuvel, P
|
|
2016
|
230 |
7 |
p. 1299-1311
|
article
|
| 9 |
Experimental research on a rotary-valved air-breathing pulse detonation engine
|
Wu, Yu-Wen
|
|
2016
|
230 |
7 |
p. 1325-1333
|
article
|
| 10 |
Fast local representation of gravity anomaly along flight trajectory
|
Zhou, Huan
|
|
2016
|
230 |
7 |
p. 1201-1215
|
article
|
| 11 |
Flow past a moderately heated horizontal cylinder at low Reynolds number
|
Ajith Kumar, S
|
|
2016
|
230 |
7 |
p. 1224-1239
|
article
|
| 12 |
Impact of interaction between cavity flow and mainstream on the performance of a model trapped vortex combustor
|
Wu, Zejun
|
|
2016
|
230 |
7 |
p. 1181-1200
|
article
|
| 13 |
Investigation of the unsteady flow of a transonic compressor using the nonlinear harmonic method
|
Zhang, Peng
|
|
2016
|
230 |
7 |
p. 1263-1272
|
article
|
| 14 |
Reducing transonic wind tunnel sting interference effects for concealed store release testing
|
Doig, Graham
|
|
2016
|
230 |
7 |
p. 1284-1298
|
article
|
| 15 |
The effect of edge profile on delta wing flow
|
Mat, Shabudin Bin
|
|
2016
|
230 |
7 |
p. 1252-1262
|
article
|
| 16 |
Updating of finite element model of aircraft structure according results of ground vibration test
|
Cecrdle, Jiri
|
|
2016
|
230 |
7 |
p. 1348-1356
|
article
|
Journal description