Digitale Bibliotheek
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                             118 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 Ablation of solid-fuel booster nozzle materials Maisonneuve, Y
1997
4 p. 277-289
13 p.
artikel
2 About classical problems of airfoil drag Eppler, R.
2003
4 p. 289-297
9 p.
artikel
3 A branch-and-bound algorithm applied to optimal radar search pattern Dodin, Pierre
2007
4 p. 279-288
10 p.
artikel
4 Accelerated loosely-coupled CFD/CSD method for nonlinear static aeroelasticity analysis Dang, Huixue
2010
4 p. 250-258
9 p.
artikel
5 A comparison of filtering approaches for aircraft engine health estimation Simon, Dan
2008
4 p. 276-284
9 p.
artikel
6 Actuator disc modelling for helicopter rotors Le Chuiton, Frédéric
2004
4 p. 285-297
13 p.
artikel
7 A damage model for ceramic matrix composites Maire, J.F.
1997
4 p. 259-266
8 p.
artikel
8 Adaptive aeroelastic vibration suppression of a supersonic airfoil with flap Rao, V.M.
2006
4 p. 309-315
7 p.
artikel
9 Adaptive data fusion and sensor management for military applications Benaskeur, Abder Rezak
2007
4 p. 327-338
12 p.
artikel
10 A direct/functional redundancy scheme for fault detection and isolation on an aircraft Amato, Francesco
2006
4 p. 338-345
8 p.
artikel
11 Aeroelastic response of a 2-D airfoil in a compressible flow field and exposed to blast loading Marzocca, Piergiovanni
2002
4 p. 259-272
14 p.
artikel
12 A hybrid genetic approach for airborne sensor vehicle routing in real-time reconnaissance missions Berger, J.
2007
4 p. 317-326
10 p.
artikel
13 A model for the operation of nitrous oxide monopropellant Zakirov, Vadim
2008
4 p. 318-323
6 p.
artikel
14 Analysis of hypersonic compression ramp laminar flows under sharp leading edge conditions Marini, Marco
2001
4 p. 257-271
15 p.
artikel
15 Analysis of wake vortex decay mechanisms in the atmosphere Holzäpfel, Frank
2003
4 p. 263-275
13 p.
artikel
16 An epoch state filter for use with analytical orbit models of low earth satellites Montenbruck, Oliver
2000
4 p. 277-287
11 p.
artikel
17 A new analysis model for the effective stiffness of stiffened metallic panels under combined compression and shear stress ☆ ☆ This article was presented at the German Aerospace Congress 2004. Heitmann, Matthias
2006
4 p. 316-326
11 p.
artikel
18 A new design approach of PD controllers Zhang, Jingrui
2005
4 p. 329-336
8 p.
artikel
19 A new formulation of continuum damage mechanics (CDM) for composite materials Maire, J.F.
1997
4 p. 247-257
11 p.
artikel
20 A new improved solution to thermal network problem in heat-transfer analysis of spacecraft Liu, Yang
2010
4 p. 225-234
10 p.
artikel
21 An inverse code based on a residual-correction method for wing design Jiménez-Varona, José
1999
4 p. 201-214
14 p.
artikel
22 Application of GA-based neural network for attitude control of a satellite Cheng, Chin-Hsing
2010
4 p. 241-249
9 p.
artikel
23 Application of hybrid metaheuristics in sensor management de Jong, J.L.
2007
4 p. 295-302
8 p.
artikel
24 Application of infrared diode laser absorption spectroscopy to the F4 high enthalpy wind tunnel Mohamed, A
1998
4 p. 241-250
10 p.
artikel
25 Autonomous mission management for unmanned aerial vehicles Barbier, Magali
2004
4 p. 359-368
10 p.
artikel
26 CARS thermometry in high pressure rocket combustors Grisch, Frédéric
2003
4 p. 317-330
14 p.
artikel
27 Chemical composition and mass flow measurements in a supercritical reactive flow for hypersonic real-time application Gascoin, N.
2010
4 p. 266-275
10 p.
artikel
28 Code verification/validation with respect to experimental data banks Benay, Richard
2003
4 p. 239-262
24 p.
artikel
29 Comparative controller design of an aerial robot Zarafshan, P.
2010
4 p. 276-282
7 p.
artikel
30 Comparative modeling study and experimental results of atomic oxygen recombination on silica-based surfaces at high temperature Bedra, Larbi
2005
4 p. 318-328
11 p.
artikel
31 Constraint-based conceptual design and automated sensitivity analysis for airship concept studies Rudolph, Stephan
2004
4 p. 333-345
13 p.
artikel
32 Control of approach and landing phase for reentry vehicle using fuzzy logic Min, Chan-oh
2011
4 p. 269-282
14 p.
artikel
33 Coupled simulation of flow-structure interaction in turbomachinery Carstens, Volker
2003
4 p. 298-306
9 p.
artikel
34 Cruise altitude flexibility of jet transport aircraft Filippone, Antonio
2010
4 p. 283-294
12 p.
artikel
35 Cryogenic rocket engine research within the National Technology Program TEKAN at the German Aerospace Center Mayer, Wolfgang O.H
2001
4 p. 273-282
10 p.
artikel
36 Curvature driven two-dimensional multi-objective optimization of compressor blade sections Sommer, Lars
2011
4 p. 334-342
9 p.
artikel
37 Data fusion for ground moving target tracking Koller, Jost
2007
4 p. 261-270
10 p.
artikel
38 Design of a boundary layer suction device for a supersonic quiet wind tunnel by numerical simulation Benay, R.
2004
4 p. 255-271
17 p.
artikel
39 DSP implementation of integrated store-and-forward APRS payload and OBDH subsystems for low-cost small satellite Addaim, A.
2008
4 p. 308-317
10 p.
artikel
40 Dynamical behaviors and relative trajectories of the spacecraft formation flying Baoyin, H.
2002
4 p. 295-301
7 p.
artikel
41 Dynamic behavior of electrodynamic tether deorbit system on elliptical orbit and its control by Lorentz force Yamaigiwa, Yoshiki
2005
4 p. 366-373
8 p.
artikel
42 Dynamic responses to landing impact at different key segments in selected body positions Liu, Bingkun
2008
4 p. 331-336
6 p.
artikel
43 Editorial Board 2010
4 p. IFC-
1 p.
artikel
44 Editorial Board 2008
4 p. IFC-
1 p.
artikel
45 Editorial Board 2004
4 p. IFC-
1 p.
artikel
46 Editorial Board 2006
4 p. CO2-
1 p.
artikel
47 Editorial Board 2005
4 p. CO2-
1 p.
artikel
48 Editorial Board 2007
4 p. IFC-
1 p.
artikel
49 Editorial Board 2011
4 p. IFC-
1 p.
artikel
50 Electrochemical sensors and sensor module for studying biological systems in space vehicles Oelβner, W.
1997
4 p. 291-296
6 p.
artikel
51 Experimental and numerical investigations of controlled transition in low-speed free flight Nitsche, Wolfgang
2001
4 p. 245-255
11 p.
artikel
52 Experimental and numerical study of forced shock-wave oscillations in a transonic channel Bur, R.
2006
4 p. 265-278
14 p.
artikel
53 Experimental and software tools to forecast radiative and conductive thermal transfer in partially transparent material deposed on rotating blades for turbine engine Demange, Didier
2004
4 p. 321-331
11 p.
artikel
54 Experimental dynamic load simulation by means of modal force combination Sinapius, J.M.
1997
4 p. 267-275
9 p.
artikel
55 Experimental investigation of side jet interaction with a supersonic cross flow Stahl, B.
2008
4 p. 269-275
7 p.
artikel
56 Finite element analysis and distributed control of laminated composite shells using LQR/IMSC approach Bhattacharya, Partha
2002
4 p. 273-281
9 p.
artikel
57 Flight control system design considering rate saturation Duda, Holger
1998
4 p. 265-275
11 p.
artikel
58 Flightpath predictor for minimum pilot compensation Sachs, G
1999
4 p. 247-257
11 p.
artikel
59 Global cost of assignment in the TBM framework for association of uncertain ID reports Ristic, Branko
2007
4 p. 303-309
7 p.
artikel
60 GPS based prediction of the instantaneous impact point for sounding rockets Montenbruck, Oliver
2002
4 p. 283-294
12 p.
artikel
61 Hydroelastic vibration of partially liquid-filled circular cylindrical shells under combined internal pressure and axial compression Sabri, Farhad
2011
4 p. 237-248
12 p.
artikel
62 Identification technique of constitutive model parameters for crashworthiness modelling Langrand, B.
1999
4 p. 215-227
13 p.
artikel
63 Improved aerodynamic design of turbomachinery bladings by numerical optimization Burguburu, Stéphane
2003
4 p. 277-287
11 p.
artikel
64 Integrating air transport elicits the need to harmonise software certification while maintaining safety and achieving security Kesseler, Ernst
2004
4 p. 347-358
12 p.
artikel
65 Interaction of wake vortices with the ground Puel, Florent
2000
4 p. 239-247
9 p.
artikel
66 Intercalibration of optical satellites – a case study with MOMS and SPOT ☆ ☆ This article was presented at ODAS 2000. Schroeder, Manfred
2001
4 p. 305-315
11 p.
artikel
67 Interference-fit riveting technique in fiber composite laminates Cao, Zengqiang
2006
4 p. 327-330
4 p.
artikel
68 Investigation of the fatigue life and crack growth in torque tightened bolted joints Chakherlou, T.N.
2011
4 p. 304-313
10 p.
artikel
69 Irradiation test results of components selected from novel optical Rotman lens configuration for space systems Zalevsky, Zeev
2011
4 p. 261-268
8 p.
artikel
70 Lateral flight control design for a highly flexible aircraft using nonsmooth optimization Simões, A.M.
2011
4 p. 314-322
9 p.
artikel
71 Linear approximations of relations between preliminary design parameters for utility helicopters Kallinderis, Y.
2010
4 p. 235-240
6 p.
artikel
72 Mass estimation of transport aircraft wingbox structures with a CAD/CAE-based multidisciplinary process Hürlimann, F.
2011
4 p. 323-333
11 p.
artikel
73 Methodology for the development of combined energy and attitude control systems for satellites Varatharajoo, Renuganth
2002
4 p. 303-311
9 p.
artikel
74 Modeling unsteady and perturbed combustion of heterogeneous composite propellants Favale, G.
2008
4 p. 285-294
10 p.
artikel
75 Motion compensation and autofocus of range/Doppler or bidimensional processing for airborne synthetic aperture radar Cantalloube, H
1998
4 p. 251-263
13 p.
artikel
76 Multiple ground target tracking Pannetier, B.
2007
4 p. 271-278
8 p.
artikel
77 Multi-scale modelling of silicon carbide reinforced titanium MMCs: Application to advanced compressor design Carrere, Nicolas
2003
4 p. 307-315
9 p.
artikel
78 Numerical simulation of isothermal flow in axisymmetric turbulent opposed jets Abdel-Fattah, A.
2011
4 p. 283-292
10 p.
artikel
79 Numerical simulation of turbulent flow around helicopter ducted tail rotor Cao, Yihua
2005
4 p. 300-306
7 p.
artikel
80 On drag and lift analysis of transport aircraft from wind tunnel measurements van der Vooren, J.
2008
4 p. 337-345
9 p.
artikel
81 On scheduling a multifunction radar Winter, Émilie
2007
4 p. 289-294
6 p.
artikel
82 On the spatial structure of global linear instabilities and their experimental identification Theofilis, Vassilios
2000
4 p. 249-262
14 p.
artikel
83 Operator scheduling strategies in supervisory control of multiple UAVs Cummings, M.L.
2007
4 p. 339-348
10 p.
artikel
84 Optimal input design for aircraft parameter estimation Jauberthie, Carine
2006
4 p. 331-337
7 p.
artikel
85 Optimization method for sensor planning Janez, Fabrice
2007
4 p. 310-316
7 p.
artikel
86 Orbital rendezvous using two-step sliding mode control Park, Jong-Uk
1999
4 p. 239-245
7 p.
artikel
87 Parameter identification with a controlled free flying model of a spaceplane Kirschstein, Stefan
2005
4 p. 348-356
9 p.
artikel
88 Periodic motion suppression based on control of wing rock in aircraft lateral dynamics Abdulwahab, Emad N.
2008
4 p. 295-301
7 p.
artikel
89 Probabilistic transient thermal analysis of an atmospheric reentry vehicle structure Nakamura, Toshiya
2006
4 p. 346-354
9 p.
artikel
90 Pulsatory phenomenon in a thrust optimized contour nozzle Nebbache, A.
2006
4 p. 295-308
14 p.
artikel
91 Reduced environmental impact by lowered cruise altitude for liquid hydrogen-fuelled aircraft Svensson, Fredrik
2004
4 p. 307-320
14 p.
artikel
92 Reduction of shock induced boundary layer separation in hypersonic inlets using bleed Schulte, Dirk
1998
4 p. 231-239
9 p.
artikel
93 Redundancy management of fault tolerant aircraft system architectures – reliability synthesis and analysis of degraded system states Rehage, Dominick
2005
4 p. 337-347
11 p.
artikel
94 Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control Jin, Erdong
2008
4 p. 324-330
7 p.
artikel
95 Robust incipient fault identification of aircraft engine rotor based on wavelet and fraction Wang, Zhongsheng
2010
4 p. 221-224
4 p.
artikel
96 Russian Academy of Sciences Siberian Branch Thermophysics and Aeromechanics publications in 2004 2005
4 p. 374-376
3 p.
artikel
97 Simulation and optimization of stall control for an airfoil with a synthetic jet Duvigneau, Régis
2006
4 p. 279-287
9 p.
artikel
98 Simulation of noise generation due to blade row interaction in a high speed compressor Uslu, Sitki
2004
4 p. 299-306
8 p.
artikel
99 Spatial object classification by radar measurements Morio, Jérôme
2010
4 p. 259-265
7 p.
artikel
100 Special Issue Sensor Management in Complex Systems Appriou, Alain
2007
4 p. 259-260
2 p.
artikel
101 Standard Telemetry Processing – an object oriented approach using Software Design Patterns Herrmann, Anita
2000
4 p. 289-297
9 p.
artikel
102 Streamwise vorticity in viscous, compressible, steady flow about aircraft van der Vooren, J.
2006
4 p. 288-294
7 p.
artikel
103 Structural shape parametric optimization for an internal structural-acoustic problem Soize, Christian
2000
4 p. 263-275
13 p.
artikel
104 Surface pressure measurements by using pressure-sensitive paints Le Sant, Y.
2005
4 p. 285-299
15 p.
artikel
105 Tactical air warfare: Generic model for aircraft susceptibility to infrared guided missiles Sonawane, Hemant R.
2011
4 p. 249-260
12 p.
artikel
106 The HART II test – measurement of helicopter rotor wakes van der Wall, Berend G
2004
4 p. 273-284
12 p.
artikel
107 The MEGAFLOW project Kroll, Norbert
2000
4 p. 223-237
15 p.
artikel
108 The OPTIS satellite – improved tests of Special and General Relativity Scheithauer, Silvia
2005
4 p. 357-365
9 p.
artikel
109 Thermo-capillary convection in a flowing liquid jet Bauer, Helmut F.
1997
4 p. 233-246
14 p.
artikel
110 Thermophysics and Aeromechanics Author index of publications in 2005 2006
4 p. 355-358
4 p.
artikel
111 Transonic flutter computations for the NLR 7301 supercritical airfoil Weber, Stefan
2001
4 p. 293-304
12 p.
artikel
112 Use of finite-element models for preparation of ground vibration test Gloth, Gerrit
2001
4 p. 283-291
9 p.
artikel
113 Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver Hu, Qinglei
2005
4 p. 307-317
11 p.
artikel
114 Velocity and position error compensation using strapdown inertial navigation system/celestial navigation system integration based on ensemble neural network Xu, Fan
2008
4 p. 302-307
6 p.
artikel
115 Vibrational relaxation of CO2 (m, n l , p) in a CO2-N2 mixture. Part 1: Survey of available data Joly, V
1999
4 p. 229-238
10 p.
artikel
116 Vibration and damping analysis of orthotropic cylindrical shells with electrorheological core layer Yeh, Jia-Yi
2011
4 p. 293-303
11 p.
artikel
117 Wake-vortex characteristics of military-type aircraft measured at airport oberpfaffenhofen using the DLR laser doppler anemometer Köpp, F
1999
4 p. 191-199
9 p.
artikel
118 Wind tunnel–flight correlation for laminar wings in adiabatic and heating flow conditions Stock, Hans W.
2002
4 p. 245-257
13 p.
artikel
                             118 gevonden resultaten
 
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