| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active boundary layer tripping using oscillatory vorticity generator
|
Yehoshua, Tal
|
|
2006
|
|
3 |
p. 175-180
6 p.
|
artikel
|
| 2 |
Adaptive nonlinear control system design for helicopter robust command augmentation
|
Lee, S.
|
|
2005
|
|
3 |
p. 241-251
11 p.
|
artikel
|
| 3 |
Aeroacoustic analysis of high tip-speed rotating blades
|
Ianniello, Sandro
|
|
2001
|
|
3 |
p. 179-192
14 p.
|
artikel
|
| 4 |
Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds
|
Qin, Z.
|
|
2002
|
|
3 |
p. 195-208
14 p.
|
artikel
|
| 5 |
A fast response probe system for in-flight measurements of atmospheric turbulence
|
Lemonis, Georges
|
|
2002
|
|
3 |
p. 233-243
11 p.
|
artikel
|
| 6 |
A lunar exploration architecture using lunar libration point one
|
Yazdi, Kian
|
|
2008
|
|
3 |
p. 231-240
10 p.
|
artikel
|
| 7 |
A methodology for multi-objective design assessment and flight control synthesis tuning
|
Joos, H.-D.
|
|
1999
|
|
3 |
p. 161-176
16 p.
|
artikel
|
| 8 |
Analysis and tuning of a ‘Total Energy Control System’ control law using eigenstructure assignment
|
Faleiro, L.F.
|
|
1999
|
|
3 |
p. 127-140
14 p.
|
artikel
|
| 9 |
Analysis of the second vorticity confinement scheme
|
Costes, M.
|
|
2008
|
|
3 |
p. 203-213
11 p.
|
artikel
|
| 10 |
An optimization approach to vibration reduction in helicopter rotors with multiple active trailing edge flaps
|
Viswamurthy, Sathyamangalam Ramanarayanan
|
|
2004
|
|
3 |
p. 185-194
10 p.
|
artikel
|
| 11 |
Arc-jet testing of ultra-high-temperature-ceramics
|
Savino, Raffaele
|
|
2010
|
|
3 |
p. 178-187
10 p.
|
artikel
|
| 12 |
A simplified trajectory analysis model for small satellite payload recovery from low Earth orbit
|
Lu, Frank K.
|
|
2003
|
|
3 |
p. 231-237
7 p.
|
artikel
|
| 13 |
A thorough experimental investigation of shock/shock interferences in high Mach number flows
|
Boldyrev, Serge M
|
|
2001
|
|
3 |
p. 167-178
12 p.
|
artikel
|
| 14 |
Autonomous navigation and guidance for landing on asteroids
|
Li, Shuang
|
|
2006
|
|
3 |
p. 239-247
9 p.
|
artikel
|
| 15 |
A view finder control system for an earth observation satellite
|
Steyn, Willem H.
|
|
2006
|
|
3 |
p. 248-255
8 p.
|
artikel
|
| 16 |
Comments on the paper: Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control
|
Li, Shihua
|
|
2011
|
|
3 |
p. 193-195
3 p.
|
artikel
|
| 17 |
Comments on the Paper: Velocity changes of the Giotto spacecraft during the comet flybys: On the interpretation of perturbed Doppler data, by Pätzold and Bird
|
Porsche, Herbert
|
|
2001
|
|
3 |
p. 243-244
2 p.
|
artikel
|
| 18 |
Compression of aerodynamic databases using high-order singular value decomposition
|
Lorente, L.S.
|
|
2010
|
|
3 |
p. 168-177
10 p.
|
artikel
|
| 19 |
Control of a decelerating boundary layer. Part 1: Optimization of passive vortex generators
|
Godard, G.
|
|
2006
|
|
3 |
p. 181-191
11 p.
|
artikel
|
| 20 |
Cutting cost of lunar logistics
|
Koelle, H.Hermann
|
|
1997
|
|
3 |
p. 225-231
7 p.
|
artikel
|
| 21 |
Design and ground-based simulation of an H ∞ limited authority flight control system for the Westland Lynx Helicopter
|
Turner, Matthew C.
|
|
2001
|
|
3 |
p. 221-234
14 p.
|
artikel
|
| 22 |
Determining the far-field RCS from the response to a cylindrical wavefront
|
Guillemot, T
|
|
1997
|
|
3 |
p. 215-223
9 p.
|
artikel
|
| 23 |
Development and application of Spalart–Allmaras one equation turbulence model to three-dimensional supersonic complex configurations
|
Deck, Sébastien
|
|
2002
|
|
3 |
p. 171-183
13 p.
|
artikel
|
| 24 |
Diagnostic of YSZ in-flight particle characteristics under low pressure VPS conditions
|
Salhi, Zahir
|
|
2005
|
|
3 |
p. 203-209
7 p.
|
artikel
|
| 25 |
Durability of hybrid laminar flow control (HLFC) surfaces
|
Young, Trevor
|
|
2003
|
|
3 |
p. 181-190
10 p.
|
artikel
|
| 26 |
Editorial Board
|
|
|
2010
|
|
3 |
p. IFC-
1 p.
|
artikel
|
| 27 |
Editorial Board
|
|
|
2006
|
|
3 |
p. CO2-
1 p.
|
artikel
|
| 28 |
Editorial Board
|
|
|
2005
|
|
3 |
p. CO2-
1 p.
|
artikel
|
| 29 |
Editorial Board
|
|
|
2004
|
|
3 |
p. IFC-
1 p.
|
artikel
|
| 30 |
Editorial Board
|
|
|
2008
|
|
3 |
p. IFC-
1 p.
|
artikel
|
| 31 |
Editorial Board
|
|
|
2011
|
|
3 |
p. IFC-
1 p.
|
artikel
|
| 32 |
Effects of the resistive patch and the uniaxial anisotropic substrate on the resonant frequency and the scattering radar cross section of a rectangular microstrip antenna
|
Boufrioua, Amel
|
|
2006
|
|
3 |
p. 217-221
5 p.
|
artikel
|
| 33 |
Electrical behaviour of ceramic composite materials for aero-engine igniters
|
Jankowiak, A.
|
|
2006
|
|
3 |
p. 207-216
10 p.
|
artikel
|
| 34 |
Evaluation of Recursive Least Squares algorithm for parameter estimation in aircraft real time applications
|
Kamali, C.
|
|
2011
|
|
3 |
p. 165-174
10 p.
|
artikel
|
| 35 |
Experimental and numerical investigation of boundary-layer and wake development in a transonic turbine cascade
|
Michelassi, V.
|
|
1998
|
|
3 |
p. 191-204
14 p.
|
artikel
|
| 36 |
Experimental and numerical study of the laminar separation in hypersonic flow
|
Chanetz, B
|
|
1998
|
|
3 |
p. 205-218
14 p.
|
artikel
|
| 37 |
Fuzzy rule based classification of polarimetric SAR data
|
Hellmann, Martin
|
|
2002
|
|
3 |
p. 217-232
16 p.
|
artikel
|
| 38 |
HHC aeroacoustic rotor tests in the German-Dutch wind tunnel: Improving physical understanding and prediction codes
|
Kube, R.
|
|
1998
|
|
3 |
p. 177-190
14 p.
|
artikel
|
| 39 |
Improvement of numerical methods for crash analysis in future composite aircraft design
|
Deletombe, Eric
|
|
2000
|
|
3 |
p. 189-199
11 p.
|
artikel
|
| 40 |
Improving the performance of model-based damage detection methods through the use of an updated analytical model
|
Keye, S.
|
|
2006
|
|
3 |
p. 199-206
8 p.
|
artikel
|
| 41 |
Influence of one and two dimensional piezoelectric actuation on active vibration control of smart panels
|
Raja, S.
|
|
2002
|
|
3 |
p. 209-216
8 p.
|
artikel
|
| 42 |
Inlet ground vortex aerodynamics under headwind conditions
|
Murphy, J.P.
|
|
2011
|
|
3 |
p. 207-215
9 p.
|
artikel
|
| 43 |
Instabilities and pressure oscillations in solid rocket motors
|
Fabignon, Yves
|
|
2003
|
|
3 |
p. 191-200
10 p.
|
artikel
|
| 44 |
Investigation of engine jet/wing-tip vortex interference
|
Huppertz, Guido
|
|
2004
|
|
3 |
p. 175-183
9 p.
|
artikel
|
| 45 |
Laminar cold-flow model for the internal gas dynamics of a slab rocket motor
|
Majdalani, Joseph
|
|
2001
|
|
3 |
p. 193-207
15 p.
|
artikel
|
| 46 |
Macro/microscopic fracture characterizations of SiO2/epoxy nanocomposites
|
Yao, X.F.
|
|
2008
|
|
3 |
p. 223-230
8 p.
|
artikel
|
| 47 |
Materials and design concepts for high performance compressor components
|
Leyens, Christoph
|
|
2003
|
|
3 |
p. 201-210
10 p.
|
artikel
|
| 48 |
Maximum likelihood delay estimation in a navigation receiver for aeronautical applications
|
Antreich, F.
|
|
2008
|
|
3 |
p. 256-267
12 p.
|
artikel
|
| 49 |
Measurement of twist deflection in active twist rotor
|
Riemenschneider, Johannes
|
|
2011
|
|
3 |
p. 216-223
8 p.
|
artikel
|
| 50 |
Missile autopilot design via a modified LPV synthesis technique
|
Biannic, J.-M.
|
|
1999
|
|
3 |
p. 153-160
8 p.
|
artikel
|
| 51 |
MMH/NTO injection and ignition in vacuum downstream from an Aestus engine single injection element
|
Lecourt, Renaud
|
|
2004
|
|
3 |
p. 207-217
11 p.
|
artikel
|
| 52 |
Modeling the influence of inter-blade connections and variable rotor speed on the aeromechanical stability of a helicopter
|
Sela, Naftali M.
|
|
2000
|
|
3 |
p. 173-188
16 p.
|
artikel
|
| 53 |
Multimodel eigenstructure assignment in flight-control design
|
Magni, J.-F.
|
|
1999
|
|
3 |
p. 141-151
11 p.
|
artikel
|
| 54 |
Multiple signal tracking processes
|
Appriou, A
|
|
1997
|
|
3 |
p. 165-178
14 p.
|
artikel
|
| 55 |
MUSIG modeling and evaluation of nitrogen bubble coalescence in a bottom-closed vertical tube
|
Li, Xiangdong
|
|
2010
|
|
3 |
p. 203-212
10 p.
|
artikel
|
| 56 |
Near optimal guidance law for descent to a point using inverse problem approach
|
Naghash, Abolghasem
|
|
2008
|
|
3 |
p. 241-247
7 p.
|
artikel
|
| 57 |
Neural network based adaptive output feedback augmentation of existing controllers
|
Kim, Nakwan
|
|
2008
|
|
3 |
p. 248-255
8 p.
|
artikel
|
| 58 |
Non-linear implicit scheme using Newton's method for the numerical solution of the Navier-Stokes equations
|
Peter, Jacques
|
|
1998
|
|
3 |
p. 157-166
10 p.
|
artikel
|
| 59 |
Nonlinear static analysis of smart laminated composite plate
|
Hari Kishore, M.D.V.
|
|
2011
|
|
3 |
p. 224-235
12 p.
|
artikel
|
| 60 |
[No title]
|
Carpentier, Jean
|
|
2001
|
|
3 |
p. 165-
1 p.
|
artikel
|
| 61 |
Numerical optimization of helicopter rotor aerodynamic performance in hover
|
Le Pape, A.
|
|
2005
|
|
3 |
p. 191-201
11 p.
|
artikel
|
| 62 |
Numerical simulation of the influence of vibrations on a free surface flow under microgravity
|
Ballereau, P
|
|
1997
|
|
3 |
p. 191-202
12 p.
|
artikel
|
| 63 |
Numerical simulation of the lateral aerodynamics of an orbital stage at stage separation flow conditions
|
Cvrlje, Tomislav
|
|
2000
|
|
3 |
p. 157-171
15 p.
|
artikel
|
| 64 |
Numerical treatment of multi-phase flow equations with chemistry and stiff source terms
|
Navaz, Homayun K.
|
|
1998
|
|
3 |
p. 219-229
11 p.
|
artikel
|
| 65 |
Object-oriented computational model building of aircraft flight dynamics and systems
|
Moormann, D.
|
|
1999
|
|
3 |
p. 115-126
12 p.
|
artikel
|
| 66 |
On real-time pseudo-dynamic sub-structure testing: algorithm, numerical and experimental results
|
Bayer, Veit
|
|
2005
|
|
3 |
p. 223-232
10 p.
|
artikel
|
| 67 |
On some stochastic methods applied to aeroservoelasticity
|
Poirion, Fabrice
|
|
2000
|
|
3 |
p. 201-214
14 p.
|
artikel
|
| 68 |
On the practical application of the PSE approach to linear stability analysis
|
Langlois, M
|
|
1998
|
|
3 |
p. 167-176
10 p.
|
artikel
|
| 69 |
On the use of geometry design variables in the MDO analysis of wing structures with aeroelastic constraints on stability and response
|
Mastroddi, Franco
|
|
2011
|
|
3 |
p. 196-206
11 p.
|
artikel
|
| 70 |
Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamics
|
Gursul, I.
|
|
2005
|
|
3 |
p. 181-189
9 p.
|
artikel
|
| 71 |
Optimization of an air cushion vehicle bag and finger skirt using genetic algorithms
|
Chung, Joon
|
|
2004
|
|
3 |
p. 219-229
11 p.
|
artikel
|
| 72 |
Output feedback nonlinear control of an aeroelastic system with unsteady aerodynamics
|
Bhoir, Nilesh
|
|
2004
|
|
3 |
p. 195-205
11 p.
|
artikel
|
| 73 |
Overview of some optimal control methods adapted to expendable and reusable launch vehicle trajectories
|
Berend, Nicolas
|
|
2006
|
|
3 |
p. 222-232
11 p.
|
artikel
|
| 74 |
Physical limits of solar collectors in deflecting Earth-threatening asteroids
|
Kahle, Ralph
|
|
2006
|
|
3 |
p. 256-263
8 p.
|
artikel
|
| 75 |
Polymer dynamics applied to PEEK matrix composite welding
|
Lamèthe, Jean-Florent
|
|
2005
|
|
3 |
p. 233-240
8 p.
|
artikel
|
| 76 |
Preliminary study of a pulse normal detonation wave engine
|
Li, Jian-ling
|
|
2010
|
|
3 |
p. 161-167
7 p.
|
artikel
|
| 77 |
Quaternion based model for momentum biased nadir pointing spacecraft
|
Yang, Yaguang
|
|
2010
|
|
3 |
p. 199-202
4 p.
|
artikel
|
| 78 |
Reduced dynamic orbit determination using GPS code and carrier measurements
|
Montenbruck, Oliver
|
|
2005
|
|
3 |
p. 261-271
11 p.
|
artikel
|
| 79 |
Reynolds number effects on flow characteristics and aerodynamic performances of a swept-back wing
|
Yen, Shun C.
|
|
2011
|
|
3 |
p. 155-164
10 p.
|
artikel
|
| 80 |
Robust and optimal attitude stabilization of spacecraft with external disturbances
|
Park, Yonmook
|
|
2005
|
|
3 |
p. 253-259
7 p.
|
artikel
|
| 81 |
Shock control on a swept wing
|
Birkemeyer, Jochen
|
|
2000
|
|
3 |
p. 147-156
10 p.
|
artikel
|
| 82 |
Shock wave – boundary layer interaction control by wall ventilation
|
Doerffer, Piotr P.
|
|
2003
|
|
3 |
p. 171-179
9 p.
|
artikel
|
| 83 |
Simulation of convective heat flux and heat penetration for a spacecraft at re-entry
|
Meese, Ernst Arne
|
|
2002
|
|
3 |
p. 185-194
10 p.
|
artikel
|
| 84 |
SINS/ANS integration for augmented performance navigation solution using unscented Kalman filtering
|
Ali, Jamshaid
|
|
2006
|
|
3 |
p. 233-238
6 p.
|
artikel
|
| 85 |
Solar electric energy supply at high altitude
|
Knaupp, Werner
|
|
2004
|
|
3 |
p. 245-254
10 p.
|
artikel
|
| 86 |
Spacecraft orbit determination using GPS navigation solutions
|
Yoon, Jae-Cheol
|
|
2000
|
|
3 |
p. 215-221
7 p.
|
artikel
|
| 87 |
Special issue “Flight control law design”
|
Grübel, Georg
|
|
1999
|
|
3 |
p. 111-113
3 p.
|
artikel
|
| 88 |
Stability rating tests for the length-optimization of baffles in a liquid propellant combustion chamber using a pulse gun
|
Kim, Hong Jip
|
|
2008
|
|
3 |
p. 214-222
9 p.
|
artikel
|
| 89 |
State interpolation for on-board navigation systems
|
Montenbruck, Oliver
|
|
2001
|
|
3 |
p. 209-220
12 p.
|
artikel
|
| 90 |
State of the art and perspectives for oxide/oxide composites
|
Parlier, Michel
|
|
2003
|
|
3 |
p. 211-221
11 p.
|
artikel
|
| 91 |
Stochastic analysis of two dimensional nonlinear panels with structural damping under random excitation
|
Fazelzadeh, Seyed Ahmad
|
|
2006
|
|
3 |
p. 192-198
7 p.
|
artikel
|
| 92 |
Strategy for upper-stage pitch-over maneuver control
|
de Castro Leite Filho, Waldemar
|
|
2003
|
|
3 |
p. 223-230
8 p.
|
artikel
|
| 93 |
Structural health monitoring R&D at the “European Research Establishments in Aeronautics” (EREA)
|
Balageas, Daniel L.
|
|
2002
|
|
3 |
p. 159-170
12 p.
|
artikel
|
| 94 |
System analysis of jet engines of high supersonic flight velocities
|
Kozlaykov, V.V.
|
|
1997
|
|
3 |
p. 179-182
4 p.
|
artikel
|
| 95 |
Tests of the JAPHAR dual mode ramjet engine
|
Dessornes, O.
|
|
2005
|
|
3 |
p. 211-221
11 p.
|
artikel
|
| 96 |
The development of a preliminary structural design optimization method of an aircraft wing-box skin-stringer panels
|
Chintapalli, Sridhar
|
|
2010
|
|
3 |
p. 188-198
11 p.
|
artikel
|
| 97 |
The Iron Bird for the Fairchild-Dornier 728
|
Gerkens, T
|
|
2004
|
|
3 |
p. 231-243
13 p.
|
artikel
|
| 98 |
The motion of fast spinning rigid body about a fixed point with definite natural frequency
|
Ismail, .A.I.
|
|
1997
|
|
3 |
p. 183-190
8 p.
|
artikel
|
| 99 |
The significant role of simulation in satellite development and verification ☆ ☆ This article was presented at the German Aerospace Congress 2003.
|
Hendricks, Reinhard
|
|
2005
|
|
3 |
p. 273-283
11 p.
|
artikel
|
| 100 |
The thermal environment encountered in space by a multifunctional solar array
|
Foster, J.A.
|
|
2010
|
|
3 |
p. 213-219
7 p.
|
artikel
|
| 101 |
μ Tools for flight control robustness assessment
|
Döll, C.
|
|
1999
|
|
3 |
p. 177-189
13 p.
|
artikel
|
| 102 |
Towards an optimal concept for numerical codes simulating thrust chamber processes in high pressure chemical propulsion systems
|
Schley, C.-A.
|
|
1997
|
|
3 |
p. 203-213
11 p.
|
artikel
|
| 103 |
Tuned mass dampers for flight vehicle components subjected to rocket noise
|
Jain, P.C.
|
|
2011
|
|
3 |
p. 175-182
8 p.
|
artikel
|
| 104 |
Tuning of fuzzy fuel controller for aero-engine thrust regulation and safety considerations using genetic algorithm
|
Montazeri-Gh, Morteza
|
|
2011
|
|
3 |
p. 183-192
10 p.
|
artikel
|
| 105 |
Unsteady airload of an airfoil with variable camber
|
Mesarič, Mihael
|
|
2004
|
|
3 |
p. 167-174
8 p.
|
artikel
|
| 106 |
Velocity changes of the Giotto spacecraft during the comet flybys: on the interpretation of perturbed Doppler data
|
Pätzold, M
|
|
2001
|
|
3 |
p. 235-241
7 p.
|
artikel
|
| 107 |
Vortex topology of wing tip blowing
|
Margaris, P.
|
|
2010
|
|
3 |
p. 143-160
18 p.
|
artikel
|
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