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                             107 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 Active boundary layer tripping using oscillatory vorticity generator Yehoshua, Tal
 2006
 82-83 3 p. 175-180
6 p.
 artikel
2 Adaptive nonlinear control system design for helicopter robust command augmentation Lee, S.
 2005
 82-83 3 p. 241-251
11 p.
 artikel
3 Aeroacoustic analysis of high tip-speed rotating blades Ianniello, Sandro
 2001
 82-83 3 p. 179-192
14 p.
 artikel
4 Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds Qin, Z.
 2002
 82-83 3 p. 195-208
14 p.
 artikel
5 A fast response probe system for in-flight measurements of atmospheric turbulence Lemonis, Georges
 2002
 82-83 3 p. 233-243
11 p.
 artikel
6 A lunar exploration architecture using lunar libration point one Yazdi, Kian
 2008
 82-83 3 p. 231-240
10 p.
 artikel
7 A methodology for multi-objective design assessment and flight control synthesis tuning Joos, H.-D.
 1999
 82-83 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
 82-83 3 p. 127-140
14 p.
 artikel
9 Analysis of the second vorticity confinement scheme Costes, M.
 2008
 82-83 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
 82-83 3 p. 185-194
10 p.
 artikel
11 Arc-jet testing of ultra-high-temperature-ceramics Savino, Raffaele
 2010
 82-83 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
 82-83 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
 82-83 3 p. 167-178
12 p.
 artikel
14 Autonomous navigation and guidance for landing on asteroids Li, Shuang
 2006
 82-83 3 p. 239-247
9 p.
 artikel
15 A view finder control system for an earth observation satellite Steyn, Willem H.
 2006
 82-83 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
 82-83 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
 82-83 3 p. 243-244
2 p.
 artikel
18 Compression of aerodynamic databases using high-order singular value decomposition Lorente, L.S.
 2010
 82-83 3 p. 168-177
10 p.
 artikel
19 Control of a decelerating boundary layer. Part 1: Optimization of passive vortex generators Godard, G.
 2006
 82-83 3 p. 181-191
11 p.
 artikel
20 Cutting cost of lunar logistics Koelle, H.Hermann
 1997
 82-83 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
 82-83 3 p. 221-234
14 p.
 artikel
22 Determining the far-field RCS from the response to a cylindrical wavefront Guillemot, T
 1997
 82-83 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
 82-83 3 p. 171-183
13 p.
 artikel
24 Diagnostic of YSZ in-flight particle characteristics under low pressure VPS conditions Salhi, Zahir
 2005
 82-83 3 p. 203-209
7 p.
 artikel
25 Durability of hybrid laminar flow control (HLFC) surfaces Young, Trevor
 2003
 82-83 3 p. 181-190
10 p.
 artikel
26 Editorial Board 2010
 82-83 3 p. IFC-
1 p.
 artikel
27 Editorial Board 2006
 82-83 3 p. CO2-
1 p.
 artikel
28 Editorial Board 2005
 82-83 3 p. CO2-
1 p.
 artikel
29 Editorial Board 2004
 82-83 3 p. IFC-
1 p.
 artikel
30 Editorial Board 2008
 82-83 3 p. IFC-
1 p.
 artikel
31 Editorial Board 2011
 82-83 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
 82-83 3 p. 217-221
5 p.
 artikel
33 Electrical behaviour of ceramic composite materials for aero-engine igniters Jankowiak, A.
 2006
 82-83 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
 82-83 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
 82-83 3 p. 191-204
14 p.
 artikel
36 Experimental and numerical study of the laminar separation in hypersonic flow Chanetz, B
 1998
 82-83 3 p. 205-218
14 p.
 artikel
37 Fuzzy rule based classification of polarimetric SAR data Hellmann, Martin
 2002
 82-83 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
 82-83 3 p. 177-190
14 p.
 artikel
39 Improvement of numerical methods for crash analysis in future composite aircraft design Deletombe, Eric
 2000
 82-83 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
 82-83 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
 82-83 3 p. 209-216
8 p.
 artikel
42 Inlet ground vortex aerodynamics under headwind conditions Murphy, J.P.
 2011
 82-83 3 p. 207-215
9 p.
 artikel
43 Instabilities and pressure oscillations in solid rocket motors Fabignon, Yves
 2003
 82-83 3 p. 191-200
10 p.
 artikel
44 Investigation of engine jet/wing-tip vortex interference Huppertz, Guido
 2004
 82-83 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
 82-83 3 p. 193-207
15 p.
 artikel
46 Macro/microscopic fracture characterizations of SiO2/epoxy nanocomposites Yao, X.F.
 2008
 82-83 3 p. 223-230
8 p.
 artikel
47 Materials and design concepts for high performance compressor components Leyens, Christoph
 2003
 82-83 3 p. 201-210
10 p.
 artikel
48 Maximum likelihood delay estimation in a navigation receiver for aeronautical applications Antreich, F.
 2008
 82-83 3 p. 256-267
12 p.
 artikel
49 Measurement of twist deflection in active twist rotor Riemenschneider, Johannes
 2011
 82-83 3 p. 216-223
8 p.
 artikel
50 Missile autopilot design via a modified LPV synthesis technique Biannic, J.-M.
 1999
 82-83 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
 82-83 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
 82-83 3 p. 173-188
16 p.
 artikel
53 Multimodel eigenstructure assignment in flight-control design Magni, J.-F.
 1999
 82-83 3 p. 141-151
11 p.
 artikel
54 Multiple signal tracking processes Appriou, A
 1997
 82-83 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
 82-83 3 p. 203-212
10 p.
 artikel
56 Near optimal guidance law for descent to a point using inverse problem approach Naghash, Abolghasem
 2008
 82-83 3 p. 241-247
7 p.
 artikel
57 Neural network based adaptive output feedback augmentation of existing controllers Kim, Nakwan
 2008
 82-83 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
 82-83 3 p. 157-166
10 p.
 artikel
59 Nonlinear static analysis of smart laminated composite plate Hari Kishore, M.D.V.
 2011
 82-83 3 p. 224-235
12 p.
 artikel
60 [No title] Carpentier, Jean
 2001
 82-83 3 p. 165-
1 p.
 artikel
61 Numerical optimization of helicopter rotor aerodynamic performance in hover Le Pape, A.
 2005
 82-83 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
 82-83 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
 82-83 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
 82-83 3 p. 219-229
11 p.
 artikel
65 Object-oriented computational model building of aircraft flight dynamics and systems Moormann, D.
 1999
 82-83 3 p. 115-126
12 p.
 artikel
66 On real-time pseudo-dynamic sub-structure testing: algorithm, numerical and experimental results Bayer, Veit
 2005
 82-83 3 p. 223-232
10 p.
 artikel
67 On some stochastic methods applied to aeroservoelasticity Poirion, Fabrice
 2000
 82-83 3 p. 201-214
14 p.
 artikel
68 On the practical application of the PSE approach to linear stability analysis Langlois, M
 1998
 82-83 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
 82-83 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
 82-83 3 p. 181-189
9 p.
 artikel
71 Optimization of an air cushion vehicle bag and finger skirt using genetic algorithms Chung, Joon
 2004
 82-83 3 p. 219-229
11 p.
 artikel
72 Output feedback nonlinear control of an aeroelastic system with unsteady aerodynamics Bhoir, Nilesh
 2004
 82-83 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
 82-83 3 p. 222-232
11 p.
 artikel
74 Physical limits of solar collectors in deflecting Earth-threatening asteroids Kahle, Ralph
 2006
 82-83 3 p. 256-263
8 p.
 artikel
75 Polymer dynamics applied to PEEK matrix composite welding Lamèthe, Jean-Florent
 2005
 82-83 3 p. 233-240
8 p.
 artikel
76 Preliminary study of a pulse normal detonation wave engine Li, Jian-ling
 2010
 82-83 3 p. 161-167
7 p.
 artikel
77 Quaternion based model for momentum biased nadir pointing spacecraft Yang, Yaguang
 2010
 82-83 3 p. 199-202
4 p.
 artikel
78 Reduced dynamic orbit determination using GPS code and carrier measurements Montenbruck, Oliver
 2005
 82-83 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
 82-83 3 p. 155-164
10 p.
 artikel
80 Robust and optimal attitude stabilization of spacecraft with external disturbances Park, Yonmook
 2005
 82-83 3 p. 253-259
7 p.
 artikel
81 Shock control on a swept wing Birkemeyer, Jochen
 2000
 82-83 3 p. 147-156
10 p.
 artikel
82 Shock wave – boundary layer interaction control by wall ventilation Doerffer, Piotr P.
 2003
 82-83 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
 82-83 3 p. 185-194
10 p.
 artikel
84 SINS/ANS integration for augmented performance navigation solution using unscented Kalman filtering Ali, Jamshaid
 2006
 82-83 3 p. 233-238
6 p.
 artikel
85 Solar electric energy supply at high altitude Knaupp, Werner
 2004
 82-83 3 p. 245-254
10 p.
 artikel
86 Spacecraft orbit determination using GPS navigation solutions Yoon, Jae-Cheol
 2000
 82-83 3 p. 215-221
7 p.
 artikel
87 Special issue “Flight control law design” Grübel, Georg
 1999
 82-83 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
 82-83 3 p. 214-222
9 p.
 artikel
89 State interpolation for on-board navigation systems Montenbruck, Oliver
 2001
 82-83 3 p. 209-220
12 p.
 artikel
90 State of the art and perspectives for oxide/oxide composites Parlier, Michel
 2003
 82-83 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
 82-83 3 p. 192-198
7 p.
 artikel
92 Strategy for upper-stage pitch-over maneuver control de Castro Leite Filho, Waldemar
 2003
 82-83 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
 82-83 3 p. 159-170
12 p.
 artikel
94 System analysis of jet engines of high supersonic flight velocities Kozlaykov, V.V.
 1997
 82-83 3 p. 179-182
4 p.
 artikel
95 Tests of the JAPHAR dual mode ramjet engine Dessornes, O.
 2005
 82-83 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
 82-83 3 p. 188-198
11 p.
 artikel
97 The Iron Bird for the Fairchild-Dornier 728 Gerkens, T
 2004
 82-83 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
 82-83 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
 82-83 3 p. 273-283
11 p.
 artikel
100 The thermal environment encountered in space by a multifunctional solar array Foster, J.A.
 2010
 82-83 3 p. 213-219
7 p.
 artikel
101 μ Tools for flight control robustness assessment Döll, C.
 1999
 82-83 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
 82-83 3 p. 203-213
11 p.
 artikel
103 Tuned mass dampers for flight vehicle components subjected to rocket noise Jain, P.C.
 2011
 82-83 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
 82-83 3 p. 183-192
10 p.
 artikel
105 Unsteady airload of an airfoil with variable camber Mesarič, Mihael
 2004
 82-83 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
 82-83 3 p. 235-241
7 p.
 artikel
107 Vortex topology of wing tip blowing Margaris, P.
 2010
 82-83 3 p. 143-160
18 p.
 artikel
                             107 gevonden resultaten
 
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