| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Accuracy improvement of second-order central scheme using smart post-process filter for hybrid RANS/LES method
|
Pasandeh, Reza
|
|
2017
|
69 |
C |
p. 387-394
8 p.
|
artikel
|
| 2 |
A coupled dynamic loads analysis of satellites with an enhanced Craig–Bampton approach
|
Lim, Jae Hyuk
|
|
2017
|
69 |
C |
p. 114-122
9 p.
|
artikel
|
| 3 |
Adaptive fault tolerant attitude tracking control for miniature rotorcrafts under actuator saturation
|
Song, Zhankui
|
|
2017
|
69 |
C |
p. 27-38
12 p.
|
artikel
|
| 4 |
A ground track-based approach to design satellite constellations
|
Ortore, Emiliano
|
|
2017
|
69 |
C |
p. 458-464
7 p.
|
artikel
|
| 5 |
A hybrid fuzzy method for performance evaluation of fusion algorithms for integrated navigation system
|
Wang, Xinlong
|
|
2017
|
69 |
C |
p. 226-235
10 p.
|
artikel
|
| 6 |
Analysis of the Bauschinger effect on a multilayer helicopter blade by XFEM simulation
|
Nour, Abdelkader
|
|
2017
|
69 |
C |
p. 97-113
17 p.
|
artikel
|
| 7 |
Analysis of the plastic zone under mixed mode fracture in bonded composite repair of aircraft structures
|
Oudad, Wahid
|
|
2017
|
69 |
C |
p. 404-411
8 p.
|
artikel
|
| 8 |
Analytical stiffness model of a fluid-filled U-shaped bellows based three-parameter fluid damper for micro-vibration suppression
|
Huang, Xiuchang
|
|
2017
|
69 |
C |
p. 357-369
13 p.
|
artikel
|
| 9 |
An experimental study on the detonability of gaseous hydrocarbon fuel–oxygen mixtures in narrow channels
|
Zhang, Bo
|
|
2017
|
69 |
C |
p. 193-200
8 p.
|
artikel
|
| 10 |
A novel time integration formulation for nonlinear dynamic analysis
|
Rezaiee-Pajand, M.
|
|
2017
|
69 |
C |
p. 625-635
11 p.
|
artikel
|
| 11 |
A novel yaw control method for flying-wing aircraft in low speed regime
|
Qu, Xiaobo
|
|
2017
|
69 |
C |
p. 636-649
14 p.
|
artikel
|
| 12 |
Application of model aided inertial navigation for precise altimetry of Unmanned Aerial Vehicles in ground proximity
|
Nobahari, Hadi
|
|
2017
|
69 |
C |
p. 650-658
9 p.
|
artikel
|
| 13 |
Automatic carrier landing system based on active disturbance rejection control with a novel parameters optimizer
|
Yu, Yue
|
|
2017
|
69 |
C |
p. 149-160
12 p.
|
artikel
|
| 14 |
Autonomous safe landing-area determination for rotorcraft UAVs using multiple IR-UWB radars
|
Shin, Young Hoon
|
|
2017
|
69 |
C |
p. 617-624
8 p.
|
artikel
|
| 15 |
Ballistic impact response of fiber–metal laminates and monolithic metal plates consisting of different aluminum alloys
|
Bikakis, George S.E.
|
|
2017
|
69 |
C |
p. 201-208
8 p.
|
artikel
|
| 16 |
Canard–wing interference effects on the flight characteristics of a transonic passenger aircraft
|
Ghoreyshi, Mehdi
|
|
2017
|
69 |
C |
p. 342-356
15 p.
|
artikel
|
| 17 |
Constitutive modeling of solid propellants for three dimensional nonlinear finite element analysis
|
Tunç, Birkan
|
|
2017
|
69 |
C |
p. 290-297
8 p.
|
artikel
|
| 18 |
Deployment/retraction of the rotating Hub-Spoke Tethered Formation System
|
Huang, Panfeng
|
|
2017
|
69 |
C |
p. 495-503
9 p.
|
artikel
|
| 19 |
Detached-eddy simulation of flow past a pitching NACA 0015 airfoil with pulsed actuation
|
Wang, Liang
|
|
2017
|
69 |
C |
p. 123-135
13 p.
|
artikel
|
| 20 |
Drag reduction of supersonic blunt bodies using opposing jet and nozzle geometric variations
|
Bibi, Atiqa
|
|
2017
|
69 |
C |
p. 244-256
13 p.
|
artikel
|
| 21 |
Editorial Board
|
|
|
2017
|
69 |
C |
p. IFC-
1 p.
|
artikel
|
| 22 |
Effects of axisymmetric arc-shaped slot casing treatment on partial surge initiated instability in a transonic axial flow compressor
|
Pan, Tianyu
|
|
2017
|
69 |
C |
p. 257-268
12 p.
|
artikel
|
| 23 |
Evaluation of failure probability under parameter epistemic uncertainty: application to aerospace system reliability assessment
|
Chabridon, Vincent
|
|
2017
|
69 |
C |
p. 526-537
12 p.
|
artikel
|
| 24 |
Experimental and computational analysis of a tangent ogive slender body at incompressible speeds
|
Schoombie, Janine
|
|
2017
|
69 |
C |
p. 474-484
11 p.
|
artikel
|
| 25 |
Experimental and frequency-domain study of acoustic damping of single-layer perforated plates
|
Wu, Gang
|
|
2017
|
69 |
C |
p. 432-438
7 p.
|
artikel
|
| 26 |
Experimental and numerical studies of ammonium dinitramide based liquid propellant combustion in space thruster
|
Jing, Liyue
|
|
2017
|
69 |
C |
p. 161-170
10 p.
|
artikel
|
| 27 |
Experimental investigation of the impact of a propeller on a streamwise impinging vortex
|
Yang, Y.
|
|
2017
|
69 |
C |
p. 582-594
13 p.
|
artikel
|
| 28 |
Fast real-time three-dimensional wind estimation for fixed-wing aircraft
|
Hong, Haichao
|
|
2017
|
69 |
C |
p. 674-685
12 p.
|
artikel
|
| 29 |
Finite element model updating of liquid rocket engine nozzle based on modal test results obtained from 3-D SLDV technique
|
Yan, Song
|
|
2017
|
69 |
C |
p. 412-418
7 p.
|
artikel
|
| 30 |
Finite-time formation control for a group of quadrotor aircraft
|
Du, Haibo
|
|
2017
|
69 |
C |
p. 609-616
8 p.
|
artikel
|
| 31 |
Free vibration analysis of deep doubly curved open shells using the Ritz method
|
Malekzadeh Fard, K.
|
|
2017
|
69 |
C |
p. 136-148
13 p.
|
artikel
|
| 32 |
Free vibration of conical shells with intermediate ring support
|
Bagheri, H.
|
|
2017
|
69 |
C |
p. 321-332
12 p.
|
artikel
|
| 33 |
Fruit fly impact on an aerodynamic surface: Types of outcomes and residue components
|
Krishnan, K. Ghokulla
|
|
2017
|
69 |
C |
p. 181-192
12 p.
|
artikel
|
| 34 |
Health structure monitoring for the design of an innovative UAS fixed wing through inverse finite element method (iFEM)
|
Papa, Umberto
|
|
2017
|
69 |
C |
p. 439-448
10 p.
|
artikel
|
| 35 |
Hybrid RANS/LES of a supersonic combustor
|
Makowka, Konrad
|
|
2017
|
69 |
C |
p. 563-573
11 p.
|
artikel
|
| 36 |
Influence of equivalence ratio on plasma assisted detonation initiation by alternating current dielectric barrier discharge under rich burn condition
|
Zhou, Siyin
|
|
2017
|
69 |
C |
p. 504-512
9 p.
|
artikel
|
| 37 |
Influence of leading edge tubercles on aerodynamic characteristics of a high aspect-ratio UAV
|
Sudhakar, S.
|
|
2017
|
69 |
C |
p. 281-289
9 p.
|
artikel
|
| 38 |
Limit cycle of low spinning projectiles induced by the backlash of actuators
|
Zhou, Wei
|
|
2017
|
69 |
C |
p. 595-601
7 p.
|
artikel
|
| 39 |
Line-of-sight nonlinear model predictive control for autonomous rendezvous in elliptical orbit
|
Li, Peng
|
|
2017
|
69 |
C |
p. 236-243
8 p.
|
artikel
|
| 40 |
Minimum time state consensus for cooperative attack of multi-missile systems
|
Liu, Xing
|
|
2017
|
69 |
C |
p. 87-96
10 p.
|
artikel
|
| 41 |
Mission performance analysis of a conceptual coaxial rotorcraft for air taxi applications
|
Enconniere, J.
|
|
2017
|
69 |
C |
p. 1-14
14 p.
|
artikel
|
| 42 |
Modeling effects of membrane tension on dynamic stall for thin membrane wings
|
Alioli, Mattia
|
|
2017
|
69 |
C |
p. 419-431
13 p.
|
artikel
|
| 43 |
Model predictive control for autonomous rendezvous and docking with a tumbling target
|
Li, Qi
|
|
2017
|
69 |
C |
p. 700-711
12 p.
|
artikel
|
| 44 |
Model reduction for flight dynamics simulations using computational fluid dynamics
|
Pagliuca, Giampaolo
|
|
2017
|
69 |
C |
p. 15-26
12 p.
|
artikel
|
| 45 |
Modern approach to study trends in global ultraviolet index maps variation over solar cycles by the complementary use of time series, mathematical metrics and artificial neural networks
|
Latosińska, Magdalena
|
|
2017
|
69 |
C |
p. 48-59
12 p.
|
artikel
|
| 46 |
Multi-objective optimization in graceful performance degradation and its application in spacecraft attitude fault-tolerant control
|
Moradi, Rouzbeh
|
|
2017
|
69 |
C |
p. 465-473
9 p.
|
artikel
|
| 47 |
Multi objective optimization of sound transmission across laminated composite cylindrical shell lined with porous core investigating Non-dominated Sorting Genetic Algorithm
|
Talebitooti, R.
|
|
2017
|
69 |
C |
p. 269-280
12 p.
|
artikel
|
| 48 |
Multiple Model Adaptive Complementary Filter for Attitude Estimation
|
Kottath, Rahul
|
|
2017
|
69 |
C |
p. 574-581
8 p.
|
artikel
|
| 49 |
Nonlinear forward path tracking controller for helicopter with slung load
|
El-Ferik, Sami
|
|
2017
|
69 |
C |
p. 602-608
7 p.
|
artikel
|
| 50 |
Numerical investigation of effects of angle-of-attack on a parachute-like two-body system
|
Xue, Xiaopeng
|
|
2017
|
69 |
C |
p. 370-386
17 p.
|
artikel
|
| 51 |
Optimal short-range rendezvous using on–off constant thrust
|
Zhang, Gang
|
|
2017
|
69 |
C |
p. 209-217
9 p.
|
artikel
|
| 52 |
Optimization approach for identification of dynamic parameters of localized joints of aircraft assembled structures
|
Hernández, S.
|
|
2017
|
69 |
C |
p. 538-549
12 p.
|
artikel
|
| 53 |
Parametric studies on elastoplastic buckling of rectangular FGM thin plates
|
BeikMohammadlou, Hassan
|
|
2017
|
69 |
C |
p. 513-525
13 p.
|
artikel
|
| 54 |
Performance analysis of realistic true proportional navigation against maneuvering targets using Lyapunov-like approach
|
Li, Ke-Bo
|
|
2017
|
69 |
C |
p. 333-341
9 p.
|
artikel
|
| 55 |
Prescribed performance interceptor guidance with terminal line of sight angle constraint accounting for missile autopilot lag
|
Lyu, Shi
|
|
2017
|
69 |
C |
p. 171-180
10 p.
|
artikel
|
| 56 |
Quasi-1D analysis and performance estimation of a sub-scale RBCC engine with chemical equilibrium
|
Kim, Hye-Sung
|
|
2017
|
69 |
C |
p. 39-47
9 p.
|
artikel
|
| 57 |
Rarefied aerodynamics of a deployable re-entry capsule
|
Mungiguerra, Stefano
|
|
2017
|
69 |
C |
p. 395-403
9 p.
|
artikel
|
| 58 |
Regressor time-shifting to identify longitudinal stability and control derivatives of the Jetstream 3102
|
Yusuf, Sezsy
|
|
2017
|
69 |
C |
p. 218-225
8 p.
|
artikel
|
| 59 |
Revisiting the One-shot method for modeling limit cycle oscillations: Extension to two-degree-of-freedom systems
|
Li, Hang
|
|
2017
|
69 |
C |
p. 686-699
14 p.
|
artikel
|
| 60 |
Simulations of an aircraft with constant and pulsed blowing flow control at the engine/wing junction
|
Hue, David
|
|
2017
|
69 |
C |
p. 659-673
15 p.
|
artikel
|
| 61 |
Supersonic flow control via plasma, electric and magnetic impacts
|
Lapushkina, T.A.
|
|
2017
|
69 |
C |
p. 313-320
8 p.
|
artikel
|
| 62 |
The development of a new model to simulate the dispersion of rocket exhaust clouds
|
Sperandio Nascimento, Erick Giovani
|
|
2017
|
69 |
C |
p. 298-312
15 p.
|
artikel
|
| 63 |
The flowfield and performance analyses of turbine-based combined cycle inlet mode transition at critical/subcritical conditions
|
Liu, Jun
|
|
2017
|
69 |
C |
p. 485-494
10 p.
|
artikel
|
| 64 |
The research on active flow control method with vibration diaphragm on a NACA0012 airfoil at different stalled angles of attack
|
Di, Guangqiang
|
|
2017
|
69 |
C |
p. 76-86
11 p.
|
artikel
|
| 65 |
Topology control in self-organized optical satellite networks based on minimum weight spanning tree
|
Zheng, Yongxing
|
|
2017
|
69 |
C |
p. 449-457
9 p.
|
artikel
|
| 66 |
Vibration behaviors of functionally graded rectangular plates with porosities and moving in thermal environment
|
Wang, Yan Qing
|
|
2017
|
69 |
C |
p. 550-562
13 p.
|
artikel
|
| 67 |
Wing/canard interference of a close-coupled canard configuration in static ground effect
|
Qin, Yunpeng
|
|
2017
|
69 |
C |
p. 60-75
16 p.
|
artikel
|
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