| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A comparison of PIV and interferometric Rayleigh scattering measurements in the near field of underexpanded sonic jets
|
Yüceil, Kemal Bülent
|
|
2017
|
67 |
C |
p. 31-40
10 p.
|
artikel
|
| 2 |
Adaptive backstepping control for air-breathing hypersonic vehicle with actuator dynamics
|
Hu, Qinglei
|
|
2017
|
67 |
C |
p. 412-421
10 p.
|
artikel
|
| 3 |
Adaptive backstepping sliding mode control for 3-DOF permanent magnet spherical actuator
|
Liu, Jingmeng
|
|
2017
|
67 |
C |
p. 62-71
10 p.
|
artikel
|
| 4 |
Aircraft vulnerability assessment against fragmentation warhead
|
Konokman, Hüseyin Emrah
|
|
2017
|
67 |
C |
p. 215-227
13 p.
|
artikel
|
| 5 |
An enhanced analytical method for the subsonic indicial lift of two-dimensional aerofoils – with numerical cross-validation
|
Berci, Marco
|
|
2017
|
67 |
C |
p. 354-365
12 p.
|
artikel
|
| 6 |
An experimental study on the low velocity impact resistance of fibre metal laminates under successive impacts with reduced energies
|
Sadighi, M.
|
|
2017
|
67 |
C |
p. 54-61
8 p.
|
artikel
|
| 7 |
Assessment of vibration–dissociation coupling models for hypersonic nonequilibrium simulations
|
Hao, Jiaao
|
|
2017
|
67 |
C |
p. 433-442
10 p.
|
artikel
|
| 8 |
CFD-based aeroelastic reduced-order modeling robust to structural parameter variations
|
Winter, Maximilian
|
|
2017
|
67 |
C |
p. 13-30
18 p.
|
artikel
|
| 9 |
Command filtered backstepping sliding mode control for the hose whipping phenomenon in aerial refueling
|
He, Qiusheng
|
|
2017
|
67 |
C |
p. 495-505
11 p.
|
artikel
|
| 10 |
Correlated optimum lift coefficient and thrust-vector angle for longitudinal performance
|
Bovet, Laurent
|
|
2017
|
67 |
C |
p. 141-143
3 p.
|
artikel
|
| 11 |
Deployment simulation of foldable origami membrane structures
|
Cai, Jianguo
|
|
2017
|
67 |
C |
p. 343-353
11 p.
|
artikel
|
| 12 |
Dual-quaternion based distributed coordination control of six-DOF spacecraft formation with collision avoidance
|
Huang, Xu
|
|
2017
|
67 |
C |
p. 443-455
13 p.
|
artikel
|
| 13 |
Dynamic characteristics of a cryogenic nitrogen swirl injector under supercritical conditions
|
Kang, Jeongseok
|
|
2017
|
67 |
C |
p. 398-411
14 p.
|
artikel
|
| 14 |
Dynamic stability of rolling missile with proportional navigation & PI autopilot considering parasitic radome loop
|
Zheng, Duo
|
|
2017
|
67 |
C |
p. 41-48
8 p.
|
artikel
|
| 15 |
Editorial Board
|
|
|
2017
|
67 |
C |
p. IFC-
1 p.
|
artikel
|
| 16 |
Exact solution of thermal buckling and post buckling of composite and SMA hybrid composite beam by layerwise theory
|
Bayat, Yahya
|
|
2017
|
67 |
C |
p. 484-494
11 p.
|
artikel
|
| 17 |
Experimental and numerical investigation on hysteresis characteristics and formation mechanism for a variable geometry dual-mode combustor
|
Feng, Shuo
|
|
2017
|
67 |
C |
p. 96-104
9 p.
|
artikel
|
| 18 |
Experimental study of pyrolysis–combustion coupling in a regeneratively cooled combustor: System dynamics analysis
|
Taddeo, L.
|
|
2017
|
67 |
C |
p. 473-483
11 p.
|
artikel
|
| 19 |
Experimental validation of quadrotor simulation tool for flight within building wakes
|
Raza, Syed Ali
|
|
2017
|
67 |
C |
p. 169-180
12 p.
|
artikel
|
| 20 |
Fault severity recognition of aviation piston pump based on feature extraction of EEMD paving and optimized support vector regression model
|
Lu, Chuanqi
|
|
2017
|
67 |
C |
p. 105-117
13 p.
|
artikel
|
| 21 |
Flexible satellite attitude maneuver via constrained torque distribution and active vibration suppression
|
Cao, Xibin
|
|
2017
|
67 |
C |
p. 387-397
11 p.
|
artikel
|
| 22 |
Formation flying on quasi-halo orbits in restricted Sun–Earth/Moon system
|
Xu, Ming
|
|
2017
|
67 |
C |
p. 118-125
8 p.
|
artikel
|
| 23 |
Global optimization of benchmark aerodynamic cases using physics-based surrogate models
|
Iuliano, Emiliano
|
|
2017
|
67 |
C |
p. 273-286
14 p.
|
artikel
|
| 24 |
Identification of the transient temperature and stress distribution in an atmospheric reentry capsule assuming temperature-dependent material properties
|
Duda, Piotr
|
|
2017
|
67 |
C |
p. 265-272
8 p.
|
artikel
|
| 25 |
Large amplitude free flexural vibration analysis of finite element modeled FGM plates using new hyperbolic shear and normal deformation theory
|
Gupta, Ankit
|
|
2017
|
67 |
C |
p. 287-308
22 p.
|
artikel
|
| 26 |
Linear adaptive actuator failure compensation for wing rock motion control
|
Boulouma, Sabri
|
|
2017
|
67 |
C |
p. 155-168
14 p.
|
artikel
|
| 27 |
LPI optimization framework for search radar network based on information fusion
|
Hosseini Andargoli, Seyed Mehdi
|
|
2017
|
67 |
C |
p. 206-214
9 p.
|
artikel
|
| 28 |
Modeling and nonlinear control for air-breathing hypersonic vehicle with variable geometry inlet
|
Dou, Liqian
|
|
2017
|
67 |
C |
p. 422-432
11 p.
|
artikel
|
| 29 |
Multi-kernel neural networks for nonlinear unsteady aerodynamic reduced-order modeling
|
Kou, Jiaqing
|
|
2017
|
67 |
C |
p. 309-326
18 p.
|
artikel
|
| 30 |
Multi-resolution visual fiducial and assistant navigation system for unmanned aerial vehicle landing
|
Yu, Chong
|
|
2017
|
67 |
C |
p. 249-256
8 p.
|
artikel
|
| 31 |
On the accuracy of RANS, DES and LES turbulence models for predicting drag reduction with Base Bleed technology
|
Nicolás-Pérez, F.
|
|
2017
|
67 |
C |
p. 126-140
15 p.
|
artikel
|
| 32 |
Optimal discretization of feedback control in missile formation
|
Wu, Yun-jie
|
|
2017
|
67 |
C |
p. 456-472
17 p.
|
artikel
|
| 33 |
Optimal speed-profile determination for aircraft trajectories
|
Saucier, Antoine
|
|
2017
|
67 |
C |
p. 327-342
16 p.
|
artikel
|
| 34 |
Performance based multidisciplinary design optimization of morphing aircraft
|
Afonso, Frederico
|
|
2017
|
67 |
C |
p. 1-12
12 p.
|
artikel
|
| 35 |
Precise real-time navigation of LEO satellites using a single-frequency GPS receiver and ultra-rapid ephemerides
|
Sun, Xiucong
|
|
2017
|
67 |
C |
p. 228-236
9 p.
|
artikel
|
| 36 |
Propagation mechanism analysis of navigation errors caused by initial state errors for long-range vehicles
|
Zheng, Xu
|
|
2017
|
67 |
C |
p. 378-386
9 p.
|
artikel
|
| 37 |
Shape effects of single axisymmetric cavity in a circular duct on flow induced acoustic oscillations
|
Thirumoorthy, M.
|
|
2017
|
67 |
C |
p. 181-192
12 p.
|
artikel
|
| 38 |
Space robot active collision avoidance maneuver under thruster failure
|
Qi, Yongqiang
|
|
2017
|
67 |
C |
p. 72-77
6 p.
|
artikel
|
| 39 |
State dependent multiple model-based particle filtering for ballistic missile tracking in a low-observable environment
|
Yu, Miao
|
|
2017
|
67 |
C |
p. 144-154
11 p.
|
artikel
|
| 40 |
Target threat level assessment based on cloud model under fuzzy and uncertain conditions in air combat simulation
|
Ma, Shidong
|
|
2017
|
67 |
C |
p. 49-53
5 p.
|
artikel
|
| 41 |
The impact of tandem rotor blades on the performance of transonic axial compressors
|
Mohsen, Mohamed
|
|
2017
|
67 |
C |
p. 237-248
12 p.
|
artikel
|
| 42 |
The spray characteristics of an open-end swirl injector at ambient pressure
|
Chen, Chen
|
|
2017
|
67 |
C |
p. 78-87
10 p.
|
artikel
|
| 43 |
Three-dimensional cooperative guidance law for multiple missiles with finite-time convergence
|
Song, Junhong
|
|
2017
|
67 |
C |
p. 193-205
13 p.
|
artikel
|
| 44 |
Trajectory optimization for a ramjet-powered vehicle in ascent phase via the Gauss pseudospectral method
|
Yang, Shengbo
|
|
2017
|
67 |
C |
p. 88-95
8 p.
|
artikel
|
| 45 |
Transient analysis on ignition process of catalytic hybrid rocket motor
|
Cai, Guobiao
|
|
2017
|
67 |
C |
p. 366-377
12 p.
|
artikel
|
| 46 |
Unified attitude control for spacecraft under velocity and control constraints
|
Hu, Qinglei
|
|
2017
|
67 |
C |
p. 257-264
8 p.
|
artikel
|
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