| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A coupling finite difference/particle method for the resolution of 2D Navier-Stokes equations in velocity-vorticity form
|
Shen, Wen-Zhong
|
|
1997
|
|
2 |
p. 97-109
13 p.
|
artikel
|
| 2 |
Adaptive and neural control of a wing section using leading- and trailing-edge surfaces
|
Gujjula, Sushma
|
|
2005
|
|
2 |
p. 161-171
11 p.
|
artikel
|
| 3 |
Adaptive processing at the subarray level
|
Combaud, M.
|
|
1999
|
|
2 |
p. 93-105
13 p.
|
artikel
|
| 4 |
Adaptive space-time process in radar applications
|
Appel, Jean
|
|
1997
|
|
2 |
p. 151-161
11 p.
|
artikel
|
| 5 |
Aeroacoustics research in Europe—1996 highlights
|
Delfs, J.
|
|
1998
|
|
2 |
p. 145-154
10 p.
|
artikel
|
| 6 |
Aerodynamic design of the high-lift-wing for a Megaliner aircraft
|
Reckzeh, Daniel
|
|
2003
|
|
2 |
p. 107-119
13 p.
|
artikel
|
| 7 |
Aerodynamic parameter estimation from flight data applying extended and unscented Kalman filter
|
Chowdhary, Girish
|
|
2010
|
|
2 |
p. 106-117
12 p.
|
artikel
|
| 8 |
Aerospace launch vehicle control: an intelligent adaptive approach
|
Mehrabian, Ali Reza
|
|
2006
|
|
2 |
p. 149-155
7 p.
|
artikel
|
| 9 |
Aerothermodynamics for reusable launch systems
|
Weiland, C
|
|
2004
|
|
2 |
p. 101-110
10 p.
|
artikel
|
| 10 |
Aerothermodynamic study of UHTC-based thermal protection systems
|
Savino, Raffaele
|
|
2005
|
|
2 |
p. 151-160
10 p.
|
artikel
|
| 11 |
A low risk reentry: looking backward to step forward
|
Monti, R.
|
|
2006
|
|
2 |
p. 156-167
12 p.
|
artikel
|
| 12 |
A method of optimization for the distorted model of star map based on improved genetic algorithm
|
Wei, Quan
|
|
2011
|
|
2 |
p. 103-107
5 p.
|
artikel
|
| 13 |
A mode matching-integral equation technique for the analysis and design of corrugated horns
|
Coccioli, R
|
|
1998
|
|
2 |
p. 121-128
8 p.
|
artikel
|
| 14 |
Analysis of the static pressure distribution on a laminar flow nacelle based on euler calculations and flight measurements
|
Riedel, H
|
|
1998
|
|
2 |
p. 129-143
15 p.
|
artikel
|
| 15 |
A new efficient technology of aerodynamic design based on CFD driven optimization
|
Epstein, Boris
|
|
2006
|
|
2 |
p. 100-110
11 p.
|
artikel
|
| 16 |
A new micromechanics based CDM model and its application to CMC's
|
Chaboche, J.-L.
|
|
2002
|
|
2 |
p. 131-145
15 p.
|
artikel
|
| 17 |
An experimental study of transonic shock/boundary layer interactions subject to downstream pressure perturbations
|
Bruce, P.J.K.
|
|
2010
|
|
2 |
p. 134-142
9 p.
|
artikel
|
| 18 |
Application of Pressure Sensitive Paint (PSP) for the determination of the instantaneous pressure field of models in a wind tunnel
|
Klein, Christian
|
|
2000
|
|
2 |
p. 103-109
7 p.
|
artikel
|
| 19 |
Applying the principle of integrated navigation systems to estimating the motion of large vehicles
|
Wagner, Jörg F
|
|
2004
|
|
2 |
p. 155-166
12 p.
|
artikel
|
| 20 |
Architecture of a multistatic FMCW direction-finding radar
|
Alivizatos, Emmanouil G.
|
|
2008
|
|
2 |
p. 169-176
8 p.
|
artikel
|
| 21 |
A reduced order of complete aeroelastic model for limit cycle oscillations
|
Dardel, Morteza
|
|
2010
|
|
2 |
p. 95-105
11 p.
|
artikel
|
| 22 |
Behavior of wake vortices near the ground over a large range of Reynolds numbers
|
Türk, L
|
|
1999
|
|
2 |
p. 71-81
11 p.
|
artikel
|
| 23 |
BIRD flies over Colombia
|
Moreno, Oscar
|
|
2006
|
|
2 |
p. 144-148
5 p.
|
artikel
|
| 24 |
CFD – a key element of helicopter activities at the IAG
|
Wagner, Siegfried
|
|
2004
|
|
2 |
p. 121-130
10 p.
|
artikel
|
| 25 |
CFD-simulation of the flow through a fluidic element
|
Reisch, Uwe
|
|
2000
|
|
2 |
p. 111-123
13 p.
|
artikel
|
| 26 |
Comparison between two approaches for the simulation of delamination growth in a D.C.B. specimen
|
Roudolff, F.
|
|
2002
|
|
2 |
p. 123-130
8 p.
|
artikel
|
| 27 |
Comparison of static and dynamic fluid-structure interaction solutions in the case of a highly flexible modern transport aircraft wing
|
Girodroux-Lavigne, P.
|
|
2003
|
|
2 |
p. 121-133
13 p.
|
artikel
|
| 28 |
Computation of unsteady nozzle flow resulting from fluctuating back-pressure using euler equations
|
Gerolymos, G.A
|
|
1998
|
|
2 |
p. 91-105
15 p.
|
artikel
|
| 29 |
Conceptual design and flight simulation of space stations
|
Bertrand, Reinhold
|
|
2001
|
|
2 |
p. 147-163
17 p.
|
artikel
|
| 30 |
Crushing of conical composites shells: a numerical analysis of the governing factors
|
Morthorst, Marion
|
|
2006
|
|
2 |
p. 127-135
9 p.
|
artikel
|
| 31 |
Demonstration by PIV of the non-reproducibility of the flow field around an airfoil pitching under deep dynamic stall conditions and consequences thereof
|
Wernert, P
|
|
1997
|
|
2 |
p. 125-135
11 p.
|
artikel
|
| 32 |
Density measurements in ballistic re-entry
|
Büchner, S
|
|
1997
|
|
2 |
p. 137-149
13 p.
|
artikel
|
| 33 |
Design of precision balance and aerodynamic characteristic measurement system for micro aerial vehicles
|
Suhariyono, Arief
|
|
2006
|
|
2 |
p. 92-99
8 p.
|
artikel
|
| 34 |
Dual-code solution procedure for efficient computing equilibrium hypersonic axisymmetric laminar flows
|
Hejranfar, Kazem
|
|
2008
|
|
2 |
p. 135-149
15 p.
|
artikel
|
| 35 |
Editorial
|
|
|
1998
|
|
2 |
p. 77-
1 p.
|
artikel
|
| 36 |
Editorial Board
|
|
|
2010
|
|
2 |
p. IFC-
1 p.
|
artikel
|
| 37 |
Editorial Board
|
|
|
2008
|
|
2 |
p. IFC-
1 p.
|
artikel
|
| 38 |
Editorial Board
|
|
|
2004
|
|
2 |
p. IFC-
1 p.
|
artikel
|
| 39 |
Editorial Board
|
|
|
2006
|
|
2 |
p. CO2-
1 p.
|
artikel
|
| 40 |
Editorial Board
|
|
|
2005
|
|
2 |
p. CO2-
1 p.
|
artikel
|
| 41 |
Editorial Board
|
|
|
2011
|
|
2 |
p. IFC-
1 p.
|
artikel
|
| 42 |
Efficient roll control using distributed control surfaces and aeroelastic effects
|
Carlsson, Martin
|
|
2005
|
|
2 |
p. 143-150
8 p.
|
artikel
|
| 43 |
Efficient second-order analytical solutions for airfoils in subsonic flows
|
Mateescu, D.
|
|
2005
|
|
2 |
p. 101-115
15 p.
|
artikel
|
| 44 |
Enhanced LFR-toolbox for Matlab ☆ ☆ This article was presented at ODAS 2004.
|
Hecker, Simon
|
|
2005
|
|
2 |
p. 173-180
8 p.
|
artikel
|
| 45 |
Experimental and numerical study of the Mars Sample Return Orbiter in cold laminar hypersonic flow
|
Chanetz, B.
|
|
2002
|
|
2 |
p. 115-121
7 p.
|
artikel
|
| 46 |
Experimental investigation on turbulence intensity reduction in subsonic wind tunnels
|
Ghorbanian, Kaveh
|
|
2011
|
|
2 |
p. 137-147
11 p.
|
artikel
|
| 47 |
Experimental observation and discussion of the wing rock phenomenon
|
Guglieri, G.
|
|
1997
|
|
2 |
p. 111-123
13 p.
|
artikel
|
| 48 |
Fast wavelet iterative solvers applied to the Neumann problem
|
Choquet, Rémi
|
|
2000
|
|
2 |
p. 135-145
11 p.
|
artikel
|
| 49 |
Full-flight simulator study for wake vortex hazard area investigation
|
Schwarz, Carsten Walter
|
|
2006
|
|
2 |
p. 136-143
8 p.
|
artikel
|
| 50 |
Geometric approach to capture analysis of PN guidance law
|
Li, Chao-Yong
|
|
2008
|
|
2 |
p. 177-183
7 p.
|
artikel
|
| 51 |
Grid-optimized upwind DRP finite difference scheme on curvilinear grids for computational aeroacoustics
|
Si, Haiqing
|
|
2011
|
|
2 |
p. 90-102
13 p.
|
artikel
|
| 52 |
Helicopter H∞ control design with robust flying quality
|
Luo, Chi-Chung
|
|
2003
|
|
2 |
p. 159-169
11 p.
|
artikel
|
| 53 |
Implementation of a multi-level optimisation methodology within the e-design of a blended wing body
|
Engels, Heiko
|
|
2004
|
|
2 |
p. 145-153
9 p.
|
artikel
|
| 54 |
Improved self-alignment scheme for SINS using augmented measurement
|
Acharya, Arunasish
|
|
2011
|
|
2 |
p. 125-128
4 p.
|
artikel
|
| 55 |
Influence and characterisation of weak non-linearities in swept-sine modal testing
|
Gloth, Gerrit
|
|
2004
|
|
2 |
p. 111-120
10 p.
|
artikel
|
| 56 |
Influence of different flap settings on the wake-vortex structure of a rectangular wing with flaps and means of alleviation with wing fins
|
Schell, Ingmar
|
|
2000
|
|
2 |
p. 79-90
12 p.
|
artikel
|
| 57 |
Investigation of the stability of inviscid compressible swirling flows
|
Xia, Nan
|
|
2002
|
|
2 |
p. 99-103
5 p.
|
artikel
|
| 58 |
Investigations into incompressible steady base flows
|
Tanner, Mauri
|
|
2010
|
|
2 |
p. 126-133
8 p.
|
artikel
|
| 59 |
Magnetoconvection in fluids with suspended particles under 1g and μg
|
Siddheshwar, P.G.
|
|
2002
|
|
2 |
p. 105-114
10 p.
|
artikel
|
| 60 |
Measurement and prediction of emissions of aerosols and gaseous precursors from gas turbine engines (PartEmis): an overview
|
Wilson, Christopher William
|
|
2004
|
|
2 |
p. 131-143
13 p.
|
artikel
|
| 61 |
Measurement of annular liquid film thickness in an open-end swirl injector
|
Fu, Qing-fei
|
|
2011
|
|
2 |
p. 117-124
8 p.
|
artikel
|
| 62 |
Microstructures of ceramic composites with glass–ceramic matrices reinforced by SiC-based fibres
|
Vicens, Jean
|
|
2003
|
|
2 |
p. 135-146
12 p.
|
artikel
|
| 63 |
Modeling of the visual approach to landing using neural networks and fuzzy supervisory control
|
Entzinger, Jorg Onno
|
|
2010
|
|
2 |
p. 118-125
8 p.
|
artikel
|
| 64 |
Modelling of a solid fuel combustion chamber of a ramjet using a multi-block domain decomposition technique
|
Coelho, P.J
|
|
1998
|
|
2 |
p. 107-119
13 p.
|
artikel
|
| 65 |
Momentum wheel start-up method for HAUSAT-2 ultra-small satellite
|
Chang, Young-Keun
|
|
2006
|
|
2 |
p. 168-174
7 p.
|
artikel
|
| 66 |
Multiconstrained aerodynamic design of business jet by CFD driven optimization tool
|
Peigin, Sergey
|
|
2008
|
|
2 |
p. 125-134
10 p.
|
artikel
|
| 67 |
Multivariate interpolation for fluid-structure-interaction problems using radial basis functions
|
Beckert, Armin
|
|
2001
|
|
2 |
p. 125-134
10 p.
|
artikel
|
| 68 |
Nonlinear dynamics of a two dimensional airfoil with freeplay in an inviscid compressible flow
|
Dimitrijević, Zoran
|
|
2000
|
|
2 |
p. 125-133
9 p.
|
artikel
|
| 69 |
Nonlinear optimal control of spacecraft approaching a tumbling target
|
Xin, Ming
|
|
2011
|
|
2 |
p. 79-89
11 p.
|
artikel
|
| 70 |
Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced streamwise vorticity
|
Gerlinger, Peter
|
|
2008
|
|
2 |
p. 159-168
10 p.
|
artikel
|
| 71 |
Numerical investigation of unsteady aerodynamic characteristics of a pitching missile
|
Yang, Lizhi
|
|
2011
|
|
2 |
p. 129-136
8 p.
|
artikel
|
| 72 |
Numerical modeling of the impact on water of a flexible structure by explicit finite element method — Comparisons with Radioss numerical results and experiments
|
Ribet, H
|
|
1999
|
|
2 |
p. 83-91
9 p.
|
artikel
|
| 73 |
Numerical simulation of multistage turbine sound generation and propagation
|
Korte, Detlef
|
|
2005
|
|
2 |
p. 125-134
10 p.
|
artikel
|
| 74 |
Numerical simulation of roll induced moment of cruciform tactical missiles
|
Ben Khelil, Saloua
|
|
2001
|
|
2 |
p. 109-124
16 p.
|
artikel
|
| 75 |
Numerical simulations of the unsteady flowfield of helicopter rotors on moving embedded grids
|
Zhao, Qi-Jun
|
|
2005
|
|
2 |
p. 117-124
8 p.
|
artikel
|
| 76 |
ONERA micronewton thrust balance: Analytical modelling and parametric analysis
|
Rocca, Simone
|
|
2011
|
|
2 |
p. 148-154
7 p.
|
artikel
|
| 77 |
Performance of a single-cylinder diesel engine using oxygen-enriched intake air at simulated high-altitude conditions
|
Perez, Peter L.
|
|
2010
|
|
2 |
p. 83-94
12 p.
|
artikel
|
| 78 |
Relative orbit design and control of formation around displaced solar orbits
|
Gong, Shengping
|
|
2008
|
|
2 |
p. 195-201
7 p.
|
artikel
|
| 79 |
Robust aeroelastic control of flapped wing systems using a sliding mode observer
|
Na, Sungsoo
|
|
2006
|
|
2 |
p. 120-126
7 p.
|
artikel
|
| 80 |
Sector imaging radar for enhanced vision
|
Krieger, Gerhard
|
|
2003
|
|
2 |
p. 147-158
12 p.
|
artikel
|
| 81 |
Some physical aspects of separation bubble on a rounded backward-facing step
|
Bao, Feng
|
|
2004
|
|
2 |
p. 83-91
9 p.
|
artikel
|
| 82 |
Stability analysis of the nonlinear dynamics of flexible aircraft
|
Siepenkötter, N.
|
|
2005
|
|
2 |
p. 135-141
7 p.
|
artikel
|
| 83 |
Structural sizing for an unconventional, environment-friendly aircraft configuration within integrated conceptual design
|
Werner-Westphal, C.
|
|
2008
|
|
2 |
p. 184-194
11 p.
|
artikel
|
| 84 |
The creation of lift by sharp-edged delta wings. An analysis of a self-adaptive numerical simulation using the concept of vorticity content
|
Hentschel, R.
|
|
1998
|
|
2 |
p. 79-90
12 p.
|
artikel
|
| 85 |
The Frequency Scaling Algorithm and interferometric Spotlight SAR processing
|
Mittermayer, Josef
|
|
2002
|
|
2 |
p. 147-158
12 p.
|
artikel
|
| 86 |
The research of EMU glove heating system
|
Ding, Li
|
|
2004
|
|
2 |
p. 93-99
7 p.
|
artikel
|
| 87 |
Thermo-mechanical design aspects for primary composite structures of large transport aircraft
|
Petersen, Dieter
|
|
2001
|
|
2 |
p. 135-146
12 p.
|
artikel
|
| 88 |
The thrust and lift of an ornithopter's membrane wings with simple flapping motion
|
Lin, Che-Shu
|
|
2006
|
|
2 |
p. 111-119
9 p.
|
artikel
|
| 89 |
The turbulent decay of trailing vortex pairs in stably stratified environments
|
Holzäpfel, Frank
|
|
2001
|
|
2 |
p. 95-108
14 p.
|
artikel
|
| 90 |
Time-shared scheme design for attitude control system during space separation
|
Xia, Xiwang
|
|
2011
|
|
2 |
p. 108-116
9 p.
|
artikel
|
| 91 |
Turbulent near-wake development behind a flat plate
|
Subaschandar, N.
|
|
1999
|
|
2 |
p. 61-70
10 p.
|
artikel
|
| 92 |
Two-dimensional viscous vortex flow around a circular cylinder
|
Rouvreau, Sébastien
|
|
2001
|
|
2 |
p. 85-94
10 p.
|
artikel
|
| 93 |
Type III and type IV shock/shock interferences: theoretical and experimental aspects
|
Grasso, Francesco
|
|
2003
|
|
2 |
p. 93-106
14 p.
|
artikel
|
| 94 |
Unsteadiness in shock wave boundary layer interactions with separation
|
Dussauge, Jean-Paul
|
|
2006
|
|
2 |
p. 85-91
7 p.
|
artikel
|
| 95 |
Unsteady pressure fluctuations in the boattail region of a heat shield
|
Mehta, R.C.
|
|
2000
|
|
2 |
p. 91-102
12 p.
|
artikel
|
| 96 |
Velocity changes of the Giotto spacecraft induced during the flybys of the comets P/Halley and P/Grigg-Skjellerup
|
Porsche, H
|
|
1999
|
|
2 |
p. 107-110
4 p.
|
artikel
|
| 97 |
Water vapor condensation in forced convection flow over an airfoil
|
Karabelas, S.J.
|
|
2008
|
|
2 |
p. 150-158
9 p.
|
artikel
|
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