| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active aeroelastic control with time delay for targeted flutter modes
|
Singh, Kumar Vikram
|
|
2015
|
43 |
C |
p. 281-288
8 p.
|
artikel
|
| 2 |
Aerodynamic optimisation of a camber morphing aerofoil
|
Fincham, J.H.S.
|
|
2015
|
43 |
C |
p. 245-255
11 p.
|
artikel
|
| 3 |
An active–passive acoustics approach for bond-line condition monitoring in aerospace skin stiffener panels
|
Vanniamparambil, Prashanth Abraham
|
|
2015
|
43 |
C |
p. 289-300
12 p.
|
artikel
|
| 4 |
A new approach to autonomous rendezvous for spacecraft with limited impulsive thrust: Based on switching control strategy
|
Yang, Xuebo
|
|
2015
|
43 |
C |
p. 454-462
9 p.
|
artikel
|
| 5 |
An experimental study on the interaction between free-stream turbulence and a wing-tip vortex in the near-field
|
Ahmadi-Baloutaki, Mojtaba
|
|
2015
|
43 |
C |
p. 395-405
11 p.
|
artikel
|
| 6 |
A novel optimization method for maintaining aerodynamic performances in noise reduction design
|
Tao, Jun
|
|
2015
|
43 |
C |
p. 415-422
8 p.
|
artikel
|
| 7 |
A trended Kriging model with R 2 indicator and application to design optimization
|
Kwon, Hyungil
|
|
2015
|
43 |
C |
p. 111-125
15 p.
|
artikel
|
| 8 |
Calibration of cross quadratic term of gyro accelerometer on centrifuge and error analysis
|
Wang, Shiming
|
|
2015
|
43 |
C |
p. 30-36
7 p.
|
artikel
|
| 9 |
Challenges in the development of a slow burning solid rocket booster
|
Parhi, Achutananda
|
|
2015
|
43 |
C |
p. 437-444
8 p.
|
artikel
|
| 10 |
Combustion noise characteristics of an experimental 2D trapped vortex combustor
|
Ezhil Kumar, P.K.
|
|
2015
|
43 |
C |
p. 388-394
7 p.
|
artikel
|
| 11 |
Comparison between synthetic jets and continuous jets for active flow control: Application on a NACA 0015 and a compressor stator cascade
|
De Giorgi, M.G.
|
|
2015
|
43 |
C |
p. 256-280
25 p.
|
artikel
|
| 12 |
DDES study of the aerodynamic forces and flow physics of a delta wing in static ground effect
|
Qin, Yunpeng
|
|
2015
|
43 |
C |
p. 423-436
14 p.
|
artikel
|
| 13 |
Dimensioning of automated regenerative cooling: Setting of high-end experiment
|
Taddeo, L.
|
|
2015
|
43 |
C |
p. 350-359
10 p.
|
artikel
|
| 14 |
Drag-tracking guidance for entry vehicles without drag rate measurement
|
Yan, Han
|
|
2015
|
43 |
C |
p. 372-380
9 p.
|
artikel
|
| 15 |
Dynamic stall control optimization of rotor airfoil via variable droop leading-edge
|
Zhao, Guo-qing
|
|
2015
|
43 |
C |
p. 406-414
9 p.
|
artikel
|
| 16 |
Editorial Board
|
|
|
2015
|
43 |
C |
p. IFC-
1 p.
|
artikel
|
| 17 |
Effects of suspension line on flow field around a supersonic parachute
|
Xue, Xiao-peng
|
|
2015
|
43 |
C |
p. 63-70
8 p.
|
artikel
|
| 18 |
Elastoplastic buckling analysis of thin-walled structures
|
Ruocco, Eugenio
|
|
2015
|
43 |
C |
p. 176-190
15 p.
|
artikel
|
| 19 |
Estimation of necessary laser power to deflect near-Earth asteroid using conceptual variable-laser-power ablation
|
Song, Young-Joo
|
|
2015
|
43 |
C |
p. 165-175
11 p.
|
artikel
|
| 20 |
Evaluating the longitudinal stability of an UAV using a CFD-6DOF model
|
Sandoval, Pablo
|
|
2015
|
43 |
C |
p. 463-470
8 p.
|
artikel
|
| 21 |
Experimental research on rotating detonation in liquid fuel–gaseous air mixtures
|
Kindracki, Jan
|
|
2015
|
43 |
C |
p. 445-453
9 p.
|
artikel
|
| 22 |
Experimental study of the effect of blade curvature and aspect ratio on the performance of a rotary-wing decelerator
|
Martiarena, Juan Francisco
|
|
2015
|
43 |
C |
p. 471-477
7 p.
|
artikel
|
| 23 |
Fabrication of a thermoplastic matrix composite stiffened panel by induction welding
|
Pappadà, Silvio
|
|
2015
|
43 |
C |
p. 314-320
7 p.
|
artikel
|
| 24 |
Fractional order adaptive fuzzy sliding mode controller for a position servo system subjected to aerodynamic loading and nonlinearities
|
Ullah, Nasim
|
|
2015
|
43 |
C |
p. 381-387
7 p.
|
artikel
|
| 25 |
Hygrothermal analysis of a rotating smart exponentially graded cylindrical shell with imperfect bonding supported by an elastic foundation
|
Saadatfar, M.
|
|
2015
|
43 |
C |
p. 37-50
14 p.
|
artikel
|
| 26 |
Interaction of microwave and laser discharge resulting “heat spots” with supersonic combined cylinder bodies
|
Azarova, O.A.
|
|
2015
|
43 |
C |
p. 343-349
7 p.
|
artikel
|
| 27 |
Maneuver characteristics analysis for hypersonic glide vehicles
|
Li, Guanghua
|
|
2015
|
43 |
C |
p. 321-328
8 p.
|
artikel
|
| 28 |
Modeling and analysis of dynamics for spacecraft relative motion actuated by inter-satellite non-contacting force
|
Zhang, Yuan-wen
|
|
2015
|
43 |
C |
p. 236-244
9 p.
|
artikel
|
| 29 |
Numerical analysis of hypersonic flows around blunt-nosed models and a space vehicle
|
Saldivar Massimi, Heriberto
|
|
2015
|
43 |
C |
p. 360-371
12 p.
|
artikel
|
| 30 |
Parametric and nonparametric system identification of an experimental turbojet engine
|
Tavakolpour-Saleh, A.R.
|
|
2015
|
43 |
C |
p. 21-29
9 p.
|
artikel
|
| 31 |
PID guidance law design using short time stability approach
|
Golestani, Mehdi
|
|
2015
|
43 |
C |
p. 71-76
6 p.
|
artikel
|
| 32 |
Pseudo steady state filters for target tracking with polar measurements
|
Abdelkrim, Meche
|
|
2015
|
43 |
C |
p. 14-20
7 p.
|
artikel
|
| 33 |
Radially accelerated trajectories for variable mass spacecraft
|
Quarta, Alessandro A.
|
|
2015
|
43 |
C |
p. 219-225
7 p.
|
artikel
|
| 34 |
RBF neural network based second-order sliding mode guidance for Mars entry under uncertainties
|
Li, Shuang
|
|
2015
|
43 |
C |
p. 226-235
10 p.
|
artikel
|
| 35 |
Relative positioning of spacecraft in intense ionospheric conditions by GPS
|
Tancredi, U.
|
|
2015
|
43 |
C |
p. 191-198
8 p.
|
artikel
|
| 36 |
Robust attitude maneuver control of spacecraft with reaction wheel low-speed friction compensation
|
Wu, Shunan
|
|
2015
|
43 |
C |
p. 213-218
6 p.
|
artikel
|
| 37 |
Robust optimal sliding mode control for spacecraft position and attitude maneuvers
|
Pukdeboon, Chutiphon
|
|
2015
|
43 |
C |
p. 329-342
14 p.
|
artikel
|
| 38 |
Stochastic optimal control for aircraft conflict resolution under wind uncertainty
|
Matsuno, Yoshinori
|
|
2015
|
43 |
C |
p. 77-88
12 p.
|
artikel
|
| 39 |
Structural behaviour modelling of bolted joints in composite laminates subjected to cyclic loading
|
Scarselli, G.
|
|
2015
|
43 |
C |
p. 89-95
7 p.
|
artikel
|
| 40 |
Supercritical natural laminar flow airfoil optimization for regional aircraft wing design
|
Zhang, Yufei
|
|
2015
|
43 |
C |
p. 152-164
13 p.
|
artikel
|
| 41 |
Surrogate models and mixtures of experts in aerodynamic performance prediction for aircraft mission analysis
|
Liem, Rhea P.
|
|
2015
|
43 |
C |
p. 126-151
26 p.
|
artikel
|
| 42 |
The aerodynamic design evaluation of a blended-wing-body configuration
|
Dehpanah, Payam
|
|
2015
|
43 |
C |
p. 96-110
15 p.
|
artikel
|
| 43 |
The evaluation of a detached eddy simulation based on the k–ω– υ 2 ¯ –f model with three flow configurations
|
Mirzaei, M.
|
|
2015
|
43 |
C |
p. 199-212
14 p.
|
artikel
|
| 44 |
Three dimensional graded finite element elasticity shear buckling analysis of FGM annular sector plates
|
Asemi, K.
|
|
2015
|
43 |
C |
p. 1-13
13 p.
|
artikel
|
| 45 |
Towards analysis and predicting maps of ultraviolet index from experimental astronomical parameters (solar elevation, total ozone level, aerosol index, reflectivity). Artificial neural networks global scale approach
|
Latosińska, Jolanta Natalia
|
|
2015
|
43 |
C |
p. 301-313
13 p.
|
artikel
|
| 46 |
Wing weight model for conceptual design of nonplanar configurations
|
Andrews, Stephen A.
|
|
2015
|
43 |
C |
p. 51-62
12 p.
|
artikel
|
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