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