| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A closed-form 3D shell solution for multilayered structures subjected to different load combinations
|
Brischetto, Salvatore
|
|
2017
|
70 |
C |
p. 29-46
18 p.
|
artikel
|
| 2 |
A complete rotor–stator coupling method for frequency domain analysis of turbomachinery unsteady flow
|
Wang, Dingxi
|
|
2017
|
70 |
C |
p. 367-377
11 p.
|
artikel
|
| 3 |
Adaptive reaching law based three-dimensional finite-time guidance law against maneuvering targets with input saturation
|
Si, YuJie
|
|
2017
|
70 |
C |
p. 198-210
13 p.
|
artikel
|
| 4 |
Aeroacoustic measurement of 30P30N high-lift configuration in the test section with Kevlar cloth and perforated plate
|
Li, Ling
|
|
2017
|
70 |
C |
p. 590-599
10 p.
|
artikel
|
| 5 |
Aerodynamic design analysis of a UAV for superficial research of volcanic environments
|
Bravo-Mosquera, Pedro David
|
|
2017
|
70 |
C |
p. 600-614
15 p.
|
artikel
|
| 6 |
Aerodynamic impact of a streamwise vortex on a propeller
|
Yang, Y.
|
|
2017
|
70 |
C |
p. 108-120
13 p.
|
artikel
|
| 7 |
Aerodynamic influences on a tethered high-altitude lighter-than-air platform system to its behavior
|
Chiba, Kazuhisa
|
|
2017
|
70 |
C |
p. 405-411
7 p.
|
artikel
|
| 8 |
A jamming tolerant BeiDou combined B1/B2 vector tracking algorithm for ultra-tightly coupled GNSS/INS systems
|
Xie, Fei
|
|
2017
|
70 |
C |
p. 265-276
12 p.
|
artikel
|
| 9 |
All-at-once approach to multifidelity polynomial chaos expansion surrogate modeling
|
Bryson, Dean E.
|
|
2017
|
70 |
C |
p. 121-136
16 p.
|
artikel
|
| 10 |
A mixed finite element and improved genetic algorithm method for maximizing buckling load of stiffened laminated composite plates
|
Vosoughi, A.R.
|
|
2017
|
70 |
C |
p. 378-387
10 p.
|
artikel
|
| 11 |
A modified elliptic integral method and its application in three-dimensional honeycombs
|
Fu, Ming-Hui
|
|
2017
|
70 |
C |
p. 88-94
7 p.
|
artikel
|
| 12 |
Analysis of key elements to evaluate the performance of a multirotor unmanned aerial–aquatic vehicle
|
Villegas, A.
|
|
2017
|
70 |
C |
p. 412-418
7 p.
|
artikel
|
| 13 |
Analytical modelling for thermo-mechanical analysis of cross-ply and angle-ply laminated composite plates
|
Joshan, Y.S.
|
|
2017
|
70 |
C |
p. 137-151
15 p.
|
artikel
|
| 14 |
An evaluation of the tip clearance effects on turbine efficiency for space propulsion applications considering liquid rocket engine using turbopumps
|
Lindquist Whitacker, Luiz Henrique
|
|
2017
|
70 |
C |
p. 55-65
11 p.
|
artikel
|
| 15 |
A novel concept for non-linear multidisciplinary aerodynamic design optimization
|
Singh, Sandeep Kr.
|
|
2017
|
70 |
C |
p. 626-635
10 p.
|
artikel
|
| 16 |
A novel crater recognition based visual navigation approach for asteroid precise pin-point landing
|
Tian, Yang
|
|
2017
|
70 |
C |
p. 1-9
9 p.
|
artikel
|
| 17 |
A robust design for a winglet based on NURBS-FFD method and PSO algorithm
|
Tao, Jun
|
|
2017
|
70 |
C |
p. 568-577
10 p.
|
artikel
|
| 18 |
Assessing the impact of relaxing cruise operations with a reduction of the minimum rate of climb and/or step climb heights
|
Dalmau, Ramon
|
|
2017
|
70 |
C |
p. 461-470
10 p.
|
artikel
|
| 19 |
Control of large amplitude vibrations of doubly curved sandwich shells composed of fuzzy fiber reinforced composite facings
|
Suresh Kumar, R.
|
|
2017
|
70 |
C |
p. 10-28
19 p.
|
artikel
|
| 20 |
Corrigendum to “Multiple Model Adaptive Complementary Filter for Attitude Estimation” [Aerospace Science and Technology 69 (2017) 574–581]
|
Kottath, Rahul
|
|
2017
|
70 |
C |
p. 644-
1 p.
|
artikel
|
| 21 |
Distributed trajectory optimization for multiple solar-powered UAVs target tracking in urban environment by Adaptive Grasshopper Optimization Algorithm
|
Wu, Jianfa
|
|
2017
|
70 |
C |
p. 497-510
14 p.
|
artikel
|
| 22 |
Distributed UAV flocking control based on homing pigeon hierarchical strategies
|
Luo, Qinan
|
|
2017
|
70 |
C |
p. 257-264
8 p.
|
artikel
|
| 23 |
Editorial Board
|
|
|
2017
|
70 |
C |
p. IFC-
1 p.
|
artikel
|
| 24 |
Effect of energy addition parameters upon scramjet nozzle performances based on the variance analysis method
|
Ju, Shengjun
|
|
2017
|
70 |
C |
p. 511-519
9 p.
|
artikel
|
| 25 |
Experimental and numerical investigations of the effect of cellular wired core on the ballistic resistance of sandwich structures
|
Alavi Nia, A.
|
|
2017
|
70 |
C |
p. 445-452
8 p.
|
artikel
|
| 26 |
Experimental investigation of stall inception of a low speed contra rotating axial flow fan under circumferential distorted flow condition
|
Toge, Tegegn Dejene
|
|
2017
|
70 |
C |
p. 534-548
15 p.
|
artikel
|
| 27 |
Experimental study of supersonic flow over cavity with aft wall offset and cavity floor injection
|
Gautam, Tanuj
|
|
2017
|
70 |
C |
p. 211-232
22 p.
|
artikel
|
| 28 |
FDF-based combustion instability analysis for stabilization effects of a slotted plate in a multiple flame combustor
|
Oh, Seungtaek
|
|
2017
|
70 |
C |
p. 95-107
13 p.
|
artikel
|
| 29 |
Flight dynamic modeling and control for a telescopic wing morphing aircraft via asymmetric wing morphing
|
Yue, Ting
|
|
2017
|
70 |
C |
p. 328-338
11 p.
|
artikel
|
| 30 |
Gust response and body freedom flutter of a flying-wing aircraft with a passive gust alleviation device
|
Guo, S.
|
|
2017
|
70 |
C |
p. 277-285
9 p.
|
artikel
|
| 31 |
Intelligent identification and mitigation of GNSS multipath errors using adaptive BOCPD
|
Ye, Wen
|
|
2017
|
70 |
C |
p. 453-460
8 p.
|
artikel
|
| 32 |
Investigation into the influences of the low-speed flows' accuracy on RANS simulations
|
Qu, Feng
|
|
2017
|
70 |
C |
p. 578-589
12 p.
|
artikel
|
| 33 |
Investigation of flame establishment and stabilization mechanism in a kerosene fueled supersonic combustor equipped with a thin strut
|
Zhang, Junlong
|
|
2017
|
70 |
C |
p. 152-160
9 p.
|
artikel
|
| 34 |
Investigation of the effects of fuel injector locations on ignition and flame stabilization in a kerosene fueled scramjet combustor
|
Tian, Ye
|
|
2017
|
70 |
C |
p. 310-316
7 p.
|
artikel
|
| 35 |
Ionospheric delay prediction and code-carrier divergence testing for GBAS using neural network and GPS L1
|
Sayim, Irfan
|
|
2017
|
70 |
C |
p. 66-75
10 p.
|
artikel
|
| 36 |
Linear near-equilibrium glide model for unpowered entry trajectory control
|
Zhang, Ran
|
|
2017
|
70 |
C |
p. 526-533
8 p.
|
artikel
|
| 37 |
Magnetic attitude control of bias momentum spacecraft by bounded linear feedback
|
Luo, Weiwei
|
|
2017
|
70 |
C |
p. 419-427
9 p.
|
artikel
|
| 38 |
Manipulation of impact feedbacks by using Novel mechanical-adaptor mechanism for UAV undercarriage applications
|
Esa, Moustafa
|
|
2017
|
70 |
C |
p. 233-243
11 p.
|
artikel
|
| 39 |
Multi-failure theory of composite orthogrid sandwich cylinder
|
Jiang, Shu
|
|
2017
|
70 |
C |
p. 520-525
6 p.
|
artikel
|
| 40 |
Multiple UAV distributed close formation control based on in-flight leadership hierarchies of pigeon flocks
|
Qiu, Huaxin
|
|
2017
|
70 |
C |
p. 471-486
16 p.
|
artikel
|
| 41 |
New approach to study nonlinear dynamic response and vibration of sandwich composite cylindrical panels with auxetic honeycomb core layer
|
Duc, Nguyen Dinh
|
|
2017
|
70 |
C |
p. 396-404
9 p.
|
artikel
|
| 42 |
N-objective genetic algorithm to obtain accurate equivalent single layer models with layerwise capabilities for challenging sandwich plates
|
Yarasca, J.
|
|
2017
|
70 |
C |
p. 170-188
19 p.
|
artikel
|
| 43 |
Novel adaptive surrogate model based on LRPIM for probabilistic analysis of turbine disc
|
Mao, Jianxing
|
|
2017
|
70 |
C |
p. 76-87
12 p.
|
artikel
|
| 44 |
Numerical evaluation of transient flow characteristics in a transonic centrifugal compressor with vaned diffuser
|
Zamiri, Ali
|
|
2017
|
70 |
C |
p. 244-256
13 p.
|
artikel
|
| 45 |
Numerical investigation of spray characteristics of an air-blast atomizer with dynamic mesh
|
Shafaee, Maziar
|
|
2017
|
70 |
C |
p. 351-358
8 p.
|
artikel
|
| 46 |
Numerical study on jet-wake vortex interaction of aircraft configuration
|
Misaka, Takashi
|
|
2017
|
70 |
C |
p. 615-625
11 p.
|
artikel
|
| 47 |
On-line attitude perturbation estimation in the earth-orbiting satellite
|
Hassani, Mehdi
|
|
2017
|
70 |
C |
p. 189-197
9 p.
|
artikel
|
| 48 |
Optimal small satellite orbit design based on robust multi-objective optimization method
|
Pu, Mingjun
|
|
2017
|
70 |
C |
p. 339-350
12 p.
|
artikel
|
| 49 |
Optimization and analysis of hypersonic leading edge geometries
|
Hinman, W. Schuyler
|
|
2017
|
70 |
C |
p. 549-558
10 p.
|
artikel
|
| 50 |
Performance evaluation of different air distribution systems in an aircraft cabin mockup
|
Zhang, Yongzhi
|
|
2017
|
70 |
C |
p. 359-366
8 p.
|
artikel
|
| 51 |
Performance of a novel heat based model for spacecraft attitude estimation
|
Labibian, A.
|
|
2017
|
70 |
C |
p. 317-327
11 p.
|
artikel
|
| 52 |
Quasi-one-dimensional modeling of pressure effects in supersonic nozzles
|
Maicke, Brian A.
|
|
2017
|
70 |
C |
p. 161-169
9 p.
|
artikel
|
| 53 |
Reduced-order modeling analysis of shell structures buckling using a co-rotational solid-shell element
|
Liang, Ke
|
|
2017
|
70 |
C |
p. 435-444
10 p.
|
artikel
|
| 54 |
Relative hovering analysis about an elliptical perturbed orbit with consideration of dynamic air drag and oblate earth
|
Bakhtiari, M.
|
|
2017
|
70 |
C |
p. 286-299
14 p.
|
artikel
|
| 55 |
Robust autopilot design for STT missiles with multiple disturbances using twisting control
|
Han, Tuo
|
|
2017
|
70 |
C |
p. 428-434
7 p.
|
artikel
|
| 56 |
Target detection in sea clutter via weighted averaging filter on the Riemannian manifold
|
Hua, Xiaoqiang
|
|
2017
|
70 |
C |
p. 47-54
8 p.
|
artikel
|
| 57 |
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine
|
Li, Huixin
|
|
2017
|
70 |
C |
p. 636-643
8 p.
|
artikel
|
| 58 |
The frequency characteristics of the shear layer oscillation in hybrid rocket post-chamber
|
Lee, Sulha
|
|
2017
|
70 |
C |
p. 388-395
8 p.
|
artikel
|
| 59 |
Trajectory optimization for solar sail in cislunar navigation constellation with minimal lightness number
|
Pan, Xiao
|
|
2017
|
70 |
C |
p. 559-567
9 p.
|
artikel
|
| 60 |
Vibration suppression-based attitude control for flexible spacecraft
|
Wang, Zhaohui
|
|
2017
|
70 |
C |
p. 487-496
10 p.
|
artikel
|
| 61 |
Zone-based reliability analysis on fatigue life of GH720Li turbine disk concerning uncertainty quantification
|
Wang, Rongqiao
|
|
2017
|
70 |
C |
p. 300-309
10 p.
|
artikel
|
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