| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A concept of voice guided general aviation aircraft
|
Rogalski, Tomasz
|
|
2010
|
|
5 |
p. 321-328
8 p.
|
artikel
|
| 2 |
A critical evaluation of two Reissner–Mindlin type models for composite laminated plates
|
Yu, Wenbin
|
|
2008
|
|
5 |
p. 408-417
10 p.
|
artikel
|
| 3 |
Adaptive Blade Twist – calculations and experimental results
|
Büter, Andreas
|
|
2000
|
|
5 |
p. 309-319
11 p.
|
artikel
|
| 4 |
Adaptive control of a nonlinear aeroelastic system
|
Li, Daochun
|
|
2011
|
|
5 |
p. 343-352
10 p.
|
artikel
|
| 5 |
Adaptive maneuvering entry guidance with ground-track control
|
Sudhir, M.
|
|
2007
|
|
5 |
p. 419-431
13 p.
|
artikel
|
| 6 |
Adaptive mesh refinement computation of acoustic radiation from an engine intake
|
Huang, Xun
|
|
2008
|
|
5 |
p. 418-426
9 p.
|
artikel
|
| 7 |
Addendum to “Aeroacoustic integral methods, formulation and efficient numerical implementation”
|
Prieur, Jean
|
|
2002
|
|
5 |
p. 323-
1 p.
|
artikel
|
| 8 |
A design solution for a crashworthy landing gear with a new triggering mechanism for the plastic collapse of metallic tubes
|
Airoldi, Alessandro
|
|
2005
|
|
5 |
p. 445-455
11 p.
|
artikel
|
| 9 |
Aeroelastic optimization of an aerobatic aircraft wing structure
|
Guo, Shijun
|
|
2007
|
|
5 |
p. 396-404
9 p.
|
artikel
|
| 10 |
Aerothermodynamic behaviour of a generic nosecap model including thermomechanical structural effects
|
Mack, Andreas
|
|
2007
|
|
5 |
p. 386-395
10 p.
|
artikel
|
| 11 |
A hybrid control scheme of adaptive and variable structure for flexible spacecraft
|
Li, Zhi-Bin
|
|
2004
|
|
5 |
p. 423-430
8 p.
|
artikel
|
| 12 |
Aircraft wake vortices: a comparison of wind-tunnel data with field trial measurements by laser radar
|
Harris, Michael
|
|
2000
|
|
5 |
p. 363-370
8 p.
|
artikel
|
| 13 |
An algorithm for astro-inertial navigation using CCD star sensors
|
Ali, Jamshaid
|
|
2006
|
|
5 |
p. 449-454
6 p.
|
artikel
|
| 14 |
An alternative numerical approach for full scale characterisation for riveted joint design
|
Langrand, B.
|
|
2002
|
|
5 |
p. 343-354
12 p.
|
artikel
|
| 15 |
Analysis of SPR measurements from HART II
|
Schneider, Oliver
|
|
2005
|
|
5 |
p. 409-420
12 p.
|
artikel
|
| 16 |
A new calculation of potential energy of supporting springs and the application in design of vibrating ring gyroscope
|
Sheng, Wei
|
|
2011
|
|
5 |
p. 409-415
7 p.
|
artikel
|
| 17 |
A new procedure for aerodynamic missile designs using topological optimization approach of continuum structures
|
Luo, Zhen
|
|
2006
|
|
5 |
p. 364-373
10 p.
|
artikel
|
| 18 |
An overview of infrared thermography techniques used in large wind tunnels
|
Le Sant, Y.
|
|
2002
|
|
5 |
p. 355-366
12 p.
|
artikel
|
| 19 |
A numerical and experimental study of a transitional separation bubble
|
Häggmark, Carl P
|
|
2001
|
|
5 |
p. 317-328
12 p.
|
artikel
|
| 20 |
Application of PSP in low speed flows
|
Engler, Rolf H.
|
|
2002
|
|
5 |
p. 313-322
10 p.
|
artikel
|
| 21 |
A sidelobe level reduction (SLL) for planar array antennas with −30 dB attenuators weight precision
|
Aboul-Seoud, Ahmed Khairy
|
|
2010
|
|
5 |
p. 316-320
5 p.
|
artikel
|
| 22 |
AST Journal Special Issue ‘Rotorcraft Research’
|
|
|
2005
|
|
5 |
p. 377-378
2 p.
|
artikel
|
| 23 |
A study of the effects of welding parameters on electron beam welding in the space environment
|
Fragomeni, James M.
|
|
2003
|
|
5 |
p. 373-384
12 p.
|
artikel
|
| 24 |
A systematic single-range controller synthesis procedure for nonlinear and multivariable liquid propellant engines
|
Mousavi Firdeh, S.R.
|
|
2006
|
|
5 |
p. 401-410
10 p.
|
artikel
|
| 25 |
A theory for incompressible two-dimensional steady base flow with application to two different problems
|
Tanner, Mauri
|
|
2003
|
|
5 |
p. 340-351
12 p.
|
artikel
|
| 26 |
A transition prediction model for boundary layers subjected to free-stream turbulence
|
Biau, Damien
|
|
2007
|
|
5 |
p. 370-375
6 p.
|
artikel
|
| 27 |
Automated pilot assistance for wake vortex encounters
|
Schwarz, C.
|
|
2011
|
|
5 |
p. 416-421
6 p.
|
artikel
|
| 28 |
CFD analysis of performance characteristics of Y-shaped diffuser with combined horizontal and vertical offsets
|
Gopaliya, Manoj Kumar
|
|
2010
|
|
5 |
p. 338-347
10 p.
|
artikel
|
| 29 |
Characterization of an acoustic liner by means of Laser Doppler Velocimetry in a subsonic flow
|
Minotti, A.
|
|
2008
|
|
5 |
p. 398-407
10 p.
|
artikel
|
| 30 |
Chimera simulations of multibladed rotors in high-speed forward flight with weak fluid-structure-coupling
|
Pahlke, Klausdieter
|
|
2005
|
|
5 |
p. 379-389
11 p.
|
artikel
|
| 31 |
Closed loop IBC results from CH-53G flight tests
|
Arnold, Uwe T.P.
|
|
2005
|
|
5 |
p. 421-435
15 p.
|
artikel
|
| 32 |
Combining subsystems in dynamical systems
|
Klevanski, I.
|
|
1997
|
|
5 |
p. 303-307
5 p.
|
artikel
|
| 33 |
Comparative study of various control methods for attitude control of a LEO satellite
|
Won, Chang-Hee
|
|
1999
|
|
5 |
p. 323-333
11 p.
|
artikel
|
| 34 |
Computation of the flow structure of an hydrogen/air mixture downstream of a steady system of shock waves
|
d'Angelo, Y
|
|
1997
|
|
5 |
p. 309-327
19 p.
|
artikel
|
| 35 |
Computer model to predict evaporation and deposition of thermal barrier coatings
|
Pereira, Vitor Emanuel de Matos Loureiro da Silva
|
|
2006
|
|
5 |
p. 442-448
7 p.
|
artikel
|
| 36 |
Conceptual study of micro-tab device in airframe noise reduction: (I) 2D computation
|
Kuo, Brian C.
|
|
2010
|
|
5 |
p. 307-315
9 p.
|
artikel
|
| 37 |
Considerations on CFD modeling for the design of re-entry vehicles
|
Longo, José M.A.
|
|
2000
|
|
5 |
p. 337-345
9 p.
|
artikel
|
| 38 |
Constrained path-planning for an aerial-towed cable system
|
Williams, Paul
|
|
2008
|
|
5 |
p. 347-354
8 p.
|
artikel
|
| 39 |
Control of a decelerating boundary layer. Part 2: Optimization of slotted jets vortex generators
|
Godard, G.
|
|
2006
|
|
5 |
p. 394-400
7 p.
|
artikel
|
| 40 |
Correlations to include heat transfer in gas turbine performance calculations
|
Riegler, C.
|
|
1999
|
|
5 |
p. 281-292
12 p.
|
artikel
|
| 41 |
Coupled simulation of heat transfer and temperature of the composite rocket nozzle wall
|
Zhang, Xiaoying
|
|
2011
|
|
5 |
p. 402-408
7 p.
|
artikel
|
| 42 |
Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test
|
Ho, Sook-Ying
|
|
2006
|
|
5 |
p. 420-426
7 p.
|
artikel
|
| 43 |
Design and experimental characterization of modern helicopters rotor brakes
|
Podratzky, Andreas
|
|
2007
|
|
5 |
p. 360-369
10 p.
|
artikel
|
| 44 |
Designing integrated guidance law for aerodynamic missiles by hybrid multi-objective evolutionary algorithm and tabu search
|
Omar, Hanafy M.
|
|
2010
|
|
5 |
p. 356-363
8 p.
|
artikel
|
| 45 |
Dynamic stall on a supercritical airfoil
|
Geissler, W.
|
|
2005
|
|
5 |
p. 390-399
10 p.
|
artikel
|
| 46 |
Editorial
|
Carpentier, J.
|
|
1999
|
|
5 |
p. 259-
1 p.
|
artikel
|
| 47 |
Editorial Board
|
|
|
2010
|
|
5 |
p. IFC-
1 p.
|
artikel
|
| 48 |
Editorial Board
|
|
|
2006
|
|
5 |
p. CO2-
1 p.
|
artikel
|
| 49 |
Editorial Board
|
|
|
2005
|
|
5 |
p. CO2-
1 p.
|
artikel
|
| 50 |
Editorial Board
|
|
|
2004
|
|
5 |
p. IFC-
1 p.
|
artikel
|
| 51 |
Editorial Board
|
|
|
2008
|
|
5 |
p. IFC-
1 p.
|
artikel
|
| 52 |
Editorial Board
|
|
|
2007
|
|
5 |
p. IFC-
1 p.
|
artikel
|
| 53 |
Editorial Board
|
|
|
2011
|
|
5 |
p. IFC-
1 p.
|
artikel
|
| 54 |
Effects of externally mounted stores on aeroelasticity of advanced swept cantilevered aircraft wings
|
Gern, Frank H
|
|
1998
|
|
5 |
p. 321-333
13 p.
|
artikel
|
| 55 |
Equilibrium state of trailing vortices: two-dimensional model of a far-field vortex wake
|
Likhachev, Oleg A
|
|
2001
|
|
5 |
p. 329-338
10 p.
|
artikel
|
| 56 |
Erratum to “Autonomous navigation and guidance for landing on asteroids” [Aerospace Science and Technology 10 (2006) 239–247]
|
Li, Shuang
|
|
2008
|
|
5 |
p. 427-
1 p.
|
artikel
|
| 57 |
Estimates of convection velocity of large turbulent structures in supersonic mixing layers
|
Barre, S
|
|
1997
|
|
5 |
p. 355-366
12 p.
|
artikel
|
| 58 |
Exhaust jet mixing and condensation effects in the near field of aircraft wakes
|
Garnier, F
|
|
1999
|
|
5 |
p. 271-280
10 p.
|
artikel
|
| 59 |
Experiences with dynamic load simulation by means of modal forces in the presence of structural non-linearities
|
Göge, Dennis
|
|
2006
|
|
5 |
p. 411-419
9 p.
|
artikel
|
| 60 |
FHS, the new research helicopter: Ready for service
|
Kaletka, Jürgen
|
|
2005
|
|
5 |
p. 456-467
12 p.
|
artikel
|
| 61 |
Flow control using various plasma and aerodynamic approaches (Short review)
|
Fomin, V.M
|
|
2004
|
|
5 |
p. 411-421
11 p.
|
artikel
|
| 62 |
Flow predictions around a missile with lattice wings using the actuator disc concept
|
Reynier, Philippe
|
|
2004
|
|
5 |
p. 377-388
12 p.
|
artikel
|
| 63 |
Fluid data presentation for gas turbine performance calculations using tables
|
Barcis, B.
|
|
1997
|
|
5 |
p. 329-340
12 p.
|
artikel
|
| 64 |
Flutter control of a composite plate with piezoelectric multilayered actuators
|
Raja, S.
|
|
2006
|
|
5 |
p. 435-441
7 p.
|
artikel
|
| 65 |
Frictionless liquid sloshing in circular cylindrical container configurations
|
Bauer, H.F
|
|
1999
|
|
5 |
p. 301-311
11 p.
|
artikel
|
| 66 |
Full scale experimental characterisation for riveted joint design
|
Langrand, B.
|
|
2002
|
|
5 |
p. 333-342
10 p.
|
artikel
|
| 67 |
Guidelines for implementing Detached-Eddy Simulation using different models
|
Bunge, Ulf
|
|
2007
|
|
5 |
p. 376-385
10 p.
|
artikel
|
| 68 |
Handling qualities assessment of the effects of tail boom strakes on the Bell 412 helicopter
|
Gubbels, Arthur W.
|
|
2005
|
|
5 |
p. 436-444
9 p.
|
artikel
|
| 69 |
High-enthalpy hypersonic project at ONERA
|
Chanetz, Bruno
|
|
2000
|
|
5 |
p. 347-361
15 p.
|
artikel
|
| 70 |
Hybrid propulsion system for formation flying using electrostatic forces
|
Saaj, C.M.
|
|
2010
|
|
5 |
p. 348-355
8 p.
|
artikel
|
| 71 |
In-flight investigations of atmospheric turbulence
|
Riedel, H
|
|
1998
|
|
5 |
p. 301-319
19 p.
|
artikel
|
| 72 |
In orbit nano-g measurements, lessons for future space missions
|
Touboul, P
|
|
2004
|
|
5 |
p. 431-441
11 p.
|
artikel
|
| 73 |
In-situ laser-induced incandescence of soot in an aero-engine exhaust: Comparison with certification style measurements
|
Black, John D.
|
|
2010
|
|
5 |
p. 329-337
9 p.
|
artikel
|
| 74 |
Kinematic GPS positioning of LEO satellites using ionosphere-free single frequency measurements
|
Montenbruck, Oliver
|
|
2003
|
|
5 |
p. 396-405
10 p.
|
artikel
|
| 75 |
Lift and rolling moment of a finite wing due to sinusoidal and stochastical turbulence
|
Schänzer, G.
|
|
1997
|
|
5 |
p. 341-354
14 p.
|
artikel
|
| 76 |
Local flow in the vicinity of an aircraft in gliding flight
|
Dierks, Maik
|
|
2000
|
|
5 |
p. 299-308
10 p.
|
artikel
|
| 77 |
Low speed maximum lift and flow control
|
van der Burg, J.W
|
|
2004
|
|
5 |
p. 389-400
12 p.
|
artikel
|
| 78 |
Measuring simulation fidelity through an adaptive pilot model
|
Padfield, Gareth
|
|
2005
|
|
5 |
p. 400-408
9 p.
|
artikel
|
| 79 |
Metamodels for aerothermodynamic design optimization of hypersonic spiked blunt bodies
|
Ahmed, M.Y.M.
|
|
2010
|
|
5 |
p. 364-376
13 p.
|
artikel
|
| 80 |
Microstructure and properties of electron beam welded joint of Ti–22Al–25Nb/TC11
|
Tan, Lijun
|
|
2010
|
|
5 |
p. 302-306
5 p.
|
artikel
|
| 81 |
Minimum-time space missions with solar electric propulsion
|
Quarta, Alessandro A.
|
|
2011
|
|
5 |
p. 381-392
12 p.
|
artikel
|
| 82 |
Navier–Stokes computation of heat transfer and aero-heating modeling for supersonic projectiles
|
Cayzac, Roxan
|
|
2006
|
|
5 |
p. 374-384
11 p.
|
artikel
|
| 83 |
Nonlinear dynamic modeling and simulation of an atmospheric re-entry spacecraft ☆ ☆ This paper was first presented in the 4th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, Noordwijk, The Netherlands, 18–21 October 1999. This is an updated and extended version.
|
Wu, Shu-Fan
|
|
2001
|
|
5 |
p. 365-381
17 p.
|
artikel
|
| 84 |
Numerical experiments on the accuracy of a discontinuous Galerkin method for the Euler equations
|
Berde, B
|
|
1998
|
|
5 |
p. 279-288
10 p.
|
artikel
|
| 85 |
Numerical investigation of the shock interaction effect on the lateral jet controlled missile
|
Min, Byung-Young
|
|
2006
|
|
5 |
p. 385-393
9 p.
|
artikel
|
| 86 |
Numerically analyzing more efficiently high-lift aerodynamics of wing/body model with omni-tree Cartesian grids
|
Sang, Weimin
|
|
2011
|
|
5 |
p. 375-380
6 p.
|
artikel
|
| 87 |
Numerical prediction and wind tunnel experiment for a pitching unmanned combat air vehicle
|
Cummings, Russell M.
|
|
2008
|
|
5 |
p. 355-364
10 p.
|
artikel
|
| 88 |
Numerical simulation of transverse side jet interaction with supersonic free stream
|
Aswin, G.
|
|
2010
|
|
5 |
p. 295-301
7 p.
|
artikel
|
| 89 |
Numerical studies of a non-linear aeroelastic system with plunging and pitching freeplays in supersonic/hypersonic regimes
|
Abbas, Laith K.
|
|
2007
|
|
5 |
p. 405-418
14 p.
|
artikel
|
| 90 |
On the sensitization of turbulence models to rotation and curvature
|
Spalart, P.R.
|
|
1997
|
|
5 |
p. 297-302
6 p.
|
artikel
|
| 91 |
On the stability of flexible aircraft
|
Tuzcu, İlhan
|
|
2008
|
|
5 |
p. 376-384
9 p.
|
artikel
|
| 92 |
Operational value-adding to AVHRR data over Europe: methods, results, and prospects
|
Dech, S.W
|
|
1998
|
|
5 |
p. 335-346
12 p.
|
artikel
|
| 93 |
Optimal task space control design of a Stewart manipulator for aircraft stall recovery
|
Omran, Ashraf
|
|
2011
|
|
5 |
p. 353-365
13 p.
|
artikel
|
| 94 |
Optimization method for mission analysis of aeroassisted orbital transfer vehicles
|
Bérend, Nicolas
|
|
2007
|
|
5 |
p. 432-441
10 p.
|
artikel
|
| 95 |
Passive control applied to Prandtl–Meyer expansion flow with homogeneous condensation
|
Kim, H.D
|
|
2004
|
|
5 |
p. 369-376
8 p.
|
artikel
|
| 96 |
Prediction of active flow control performance on airfoils and wings
|
Ekaterinaris, John A
|
|
2004
|
|
5 |
p. 401-410
10 p.
|
artikel
|
| 97 |
Predictive control for the attitude maneuver of a flexible spacecraft
|
Bang, Hyochoong
|
|
2004
|
|
5 |
p. 443-452
10 p.
|
artikel
|
| 98 |
Preliminary analysis of the flow inside a three-port wave rotor by means of a numerical model
|
Fatsis, A
|
|
1998
|
|
5 |
p. 289-300
12 p.
|
artikel
|
| 99 |
Real time numerical dynamic orbit determination of geostationary satellite for time synchronization service
|
Kim, Bang-Yeop
|
|
2003
|
|
5 |
p. 385-395
11 p.
|
artikel
|
| 100 |
Research and dynamic simulation of docking locks with contact-impact
|
Chen, Meng
|
|
2003
|
|
5 |
p. 364-372
9 p.
|
artikel
|
| 101 |
Selecting and scheduling observations of agile satellites
|
Lemaı̂tre, Michel
|
|
2002
|
|
5 |
p. 367-381
15 p.
|
artikel
|
| 102 |
Stochastic axial compressor variable geometry schedule optimisation
|
Gallar, Luis
|
|
2011
|
|
5 |
p. 366-374
9 p.
|
artikel
|
| 103 |
Strategies for in-orbit calibration of drag-free control systems
|
Guilherme, Michel Silas
|
|
2008
|
|
5 |
p. 365-375
11 p.
|
artikel
|
| 104 |
Structural optimization of an aeroelastically tailored composite flat plate made of woven fiberglass/epoxy
|
Attaran, A.
|
|
2011
|
|
5 |
p. 393-401
9 p.
|
artikel
|
| 105 |
Studies on the influence of outboard flaps on the vortex wake of a rectangular wing
|
Haverkamp, S
|
|
2003
|
|
5 |
p. 331-339
9 p.
|
artikel
|
| 106 |
Technology approach to aero engine noise reduction
|
Neise, Wolfgang
|
|
2003
|
|
5 |
p. 352-363
12 p.
|
artikel
|
| 107 |
Temperature measurements by coherent anti-Stokes Raman spectroscopy in hydrogen-fuelled scramjet combustor
|
Vereschagin, Konstantin A
|
|
2001
|
|
5 |
p. 347-355
9 p.
|
artikel
|
| 108 |
The effect of HHC on the vortex convection in the wake of a helicopter rotor
|
van der Wall, Berend G.
|
|
2000
|
|
5 |
p. 321-336
16 p.
|
artikel
|
| 109 |
The flutter of an airfoil with cubic structural and aerodynamic non-linearities
|
Ding, Qian
|
|
2006
|
|
5 |
p. 427-434
8 p.
|
artikel
|
| 110 |
The incompressible base flow
|
Tanner, Mauri
|
|
2011
|
|
5 |
p. 422-423
2 p.
|
artikel
|
| 111 |
The knot factor method and its applications in blade measurement
|
Ye, Peiqing
|
|
2006
|
|
5 |
p. 359-363
5 p.
|
artikel
|
| 112 |
Thermodynamic analysis of gas turbines topped with wave rotors
|
Fatsis, A.
|
|
1999
|
|
5 |
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