nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Adaptive fault-tolerant control of a novel ducted-fan aerial robot against partial actuator failure
|
Fan, Wei |
|
|
122 |
C |
p. |
artikel |
2 |
Aeroacoustic modeling of helicopter transonic rotor noise
|
Fu, Jinbin |
|
|
122 |
C |
p. |
artikel |
3 |
Aeroelastic evaluation of a flexible high aspect ratio wing UAV: Numerical simulation and experimental flight validation
|
Bras, M. |
|
|
122 |
C |
p. |
artikel |
4 |
A fitness sharing based ant clustering method for multimodal optimization of the aircraft longitudinal automatic carrier landing system
|
Bian, Qi |
|
|
122 |
C |
p. |
artikel |
5 |
Air-breathing rotating detonation fueled by liquid kerosene in cavity-based annular combustor
|
Meng, Haolong |
|
|
122 |
C |
p. |
artikel |
6 |
Analysis of pulsed suction flow control behavior based on a nonlinear reduced-order model
|
Lu, Weiyu |
|
|
122 |
C |
p. |
artikel |
7 |
A numerical study of oblique detonation re-stabilization by expansion waves
|
Yao, Kepeng |
|
|
122 |
C |
p. |
artikel |
8 |
A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump
|
Tonon, Daniel da Silva |
|
|
122 |
C |
p. |
artikel |
9 |
A paratrooper model sensitivity analysis for personnel airdrop
|
Ghoreyshi, Mehdi |
|
|
122 |
C |
p. |
artikel |
10 |
Choking dynamic of highly swirled flow in variable nozzle radial turbines
|
Tiseira, Andrés |
|
|
122 |
C |
p. |
artikel |
11 |
Cross-flow transition model predictions of hypersonic transition research vehicle
|
Xiang, Xing-hao |
|
|
122 |
C |
p. |
artikel |
12 |
Editorial Board
|
|
|
|
122 |
C |
p. |
artikel |
13 |
Effect of flame motion on longitudinal combustion instabilities
|
Song, Yan |
|
|
122 |
C |
p. |
artikel |
14 |
Effects of landing gear layout on the safe rollout envelope of equipped–skid aircraft
|
Liang, Taotao |
|
|
122 |
C |
p. |
artikel |
15 |
Energy harvesting from the gust response of membrane wing using piezoelectrics
|
Huang, Guangjing |
|
|
122 |
C |
p. |
artikel |
16 |
Experimental and numerical study of flow and ignition and lean blowout characteristics of jet-cooled wall flameholder in a dual-mode combustor
|
Chen, Yuqian |
|
|
122 |
C |
p. |
artikel |
17 |
Experimental and numerical study on slag deposition in solid rocket motor
|
Wang, Junlong |
|
|
122 |
C |
p. |
artikel |
18 |
Flexible spacecraft's active fault-tolerant and anti-unwinding attitude control with vibration suppression
|
Hasan, Muhammad Noman |
|
|
122 |
C |
p. |
artikel |
19 |
General passive stability criteria for a Sun-pointing attitude using the metasurface sail
|
Zhang, Peng |
|
|
122 |
C |
p. |
artikel |
20 |
Hybrid control technique applied to an aero-servo-viscoelastic simplified wing model
|
Martins, Polliana C.O. |
|
|
122 |
C |
p. |
artikel |
21 |
Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control
|
Li, Zhibing |
|
|
122 |
C |
p. |
artikel |
22 |
Improved artificial bee colony algorithm-based path planning of unmanned autonomous helicopter using multi-strategy evolutionary learning
|
Han, Zengliang |
|
|
122 |
C |
p. |
artikel |
23 |
Increased utilization of real wind fields to improve station-keeping performance of stratospheric balloon
|
Liu, Yang |
|
|
122 |
C |
p. |
artikel |
24 |
Introducing variance-based global sensitivity analysis for uncertainty enabled operational and economic aircraft technology assessment
|
Pohya, Ahmad Ali |
|
|
122 |
C |
p. |
artikel |
25 |
Investigation of load alleviation in aircraft pre-design and its influence on structural mass and fatigue
|
Handojo, V. |
|
|
122 |
C |
p. |
artikel |
26 |
Modeling and switching adaptive control for nonlinear morphing aircraft considering actuator dynamics
|
Xu, Wenfeng |
|
|
122 |
C |
p. |
artikel |
27 |
Numerical investigation of full helicopter with and without the ground effect
|
A.S.F. Silva, Paulo |
|
|
122 |
C |
p. |
artikel |
28 |
Numerical investigation on flow and film cooling characteristics of coolant injection in rotating detonation combustor
|
Tian, Jia |
|
|
122 |
C |
p. |
artikel |
29 |
On the control allocation of fully actuated multirotor aerial vehicles
|
Santos, Davi A. |
|
|
122 |
C |
p. |
artikel |
30 |
Satellite attitude PDE-based controller design considering fluid fuel sloshing in planar maneuver
|
Jokar, Meysam |
|
|
122 |
C |
p. |
artikel |
31 |
Structural static test for validation of the structural integrity of an aircraft pylon
|
Kim, Hyun-gi |
|
|
122 |
C |
p. |
artikel |
32 |
Three-dimensional flow structures and heat transfer characteristics of compressible flow over a cylindrical cavity
|
Wang, Jiangtao |
|
|
122 |
C |
p. |
artikel |
33 |
Trajectory tracking control of powered parafoil system based on sliding mode control in a complex environment
|
Sun, Qinglin |
|
|
122 |
C |
p. |
artikel |
34 |
Uncertainty propagation in flight performance of multirotor with parametric and model uncertainties
|
Lim, Daejin |
|
|
122 |
C |
p. |
artikel |
35 |
Visual experimental research on the propagation instabilities in a plane-radial rotating detonation engine
|
Xia, Zhenjuan |
|
|
122 |
C |
p. |
artikel |