| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active aeroelastic control over a four control surface wing model
|
Cavagna, L.
|
|
2009
|
|
7 |
p. 374-382
9 p.
|
artikel
|
| 2 |
Active separation control: an overview of Reynolds and Mach numbers effects
|
Seifert, Avi
|
|
2004
|
|
7 |
p. 569-582
14 p.
|
artikel
|
| 3 |
Adaptive backstepping control for optimal descent with embedded autonomy
|
Li, Maodeng
|
|
2011
|
|
7 |
p. 589-594
6 p.
|
artikel
|
| 4 |
A dual-wheel multi-mode spacecraft actuator for near-minimum-time large angle slew maneuvers
|
Steyn, Willem H.
|
|
2008
|
|
7 |
p. 545-554
10 p.
|
artikel
|
| 5 |
Advanced optical diagnostics applied to dynamic flames and turbulent jets
|
Grisch, F.
|
|
2002
|
|
7 |
p. 465-479
15 p.
|
artikel
|
| 6 |
Aeroacoustic integral methods, formulation and efficient numerical implementation
|
Prieur, Jean
|
|
2001
|
|
7 |
p. 457-468
12 p.
|
artikel
|
| 7 |
Aerodynamic aspects of engine-aircraft integration of transport aircraft
|
Hoheisel, H.
|
|
1997
|
|
7 |
p. 475-487
13 p.
|
artikel
|
| 8 |
Aerodynamic benefits of adaptive wing technology
|
Stanewsky, Egon
|
|
2000
|
|
7 |
p. 439-452
14 p.
|
artikel
|
| 9 |
Aeroelastic stability analysis of a bird-damaged aeroengine fan assembly
|
Kim, Michael
|
|
2001
|
|
7 |
p. 469-482
14 p.
|
artikel
|
| 10 |
A family of CFD boundary conditions to simulate separation control
|
Geissler, Wolfgang
|
|
2010
|
|
7 |
p. 494-504
11 p.
|
artikel
|
| 11 |
Airfoils with boundary layer suction, design and off-design cases
|
Eppler, Richard
|
|
1999
|
|
7 |
p. 403-415
13 p.
|
artikel
|
| 12 |
An efficient aerodynamic boundary element method for aeroelastic simulations and its experimental validation
|
Eller, David
|
|
2003
|
|
7 |
p. 532-539
8 p.
|
artikel
|
| 13 |
An evaluation of RANS turbulence modelling for aerodynamic applications
|
Catalano, Pietro
|
|
2003
|
|
7 |
p. 493-509
17 p.
|
artikel
|
| 14 |
A new assessment method for the comprehensive stealth performance of penetration aircrafts
|
Li, Ying
|
|
2011
|
|
7 |
p. 511-518
8 p.
|
artikel
|
| 15 |
A new steering law for redundant control moment gyroscope clusters
|
Tekinalp, Ozan
|
|
2005
|
|
7 |
p. 626-634
9 p.
|
artikel
|
| 16 |
An experimental investigation of the effects of turbulence generators attached to an axial swirler nozzle on mixing and combustion
|
Lee, C.W.
|
|
2002
|
|
7 |
p. 517-520
4 p.
|
artikel
|
| 17 |
An iterative method for decision fusion in multiple sensor systems
|
Aziz, Ashraf M.
|
|
2010
|
|
7 |
p. 487-493
7 p.
|
artikel
|
| 18 |
Application of multi-objective optimization to axial compressor preliminary design ☆ ☆ This article was presented at the German Aerospace Congress 2005.
|
Keskin, Akin
|
|
2006
|
|
7 |
p. 581-589
9 p.
|
artikel
|
| 19 |
Assessment of explicit algebraic Reynolds-stress turbulence models in aerodynamic computations
|
Franke, Martin
|
|
2005
|
|
7 |
p. 573-581
9 p.
|
artikel
|
| 20 |
Associative parametric CAE methods in the aircraft pre-design ☆ ☆ This article was presented at the German Aerospace Congress 2004.
|
Ledermann, Christof
|
|
2005
|
|
7 |
p. 641-651
11 p.
|
artikel
|
| 21 |
AST Special Issue “Combustion”
|
Kuentzmann Dr, Paul
|
|
2002
|
|
7 |
p. 463-
1 p.
|
artikel
|
| 22 |
Attitude control of a satellite with redundant thrusters
|
Jin, Jaehyun
|
|
2006
|
|
7 |
p. 644-651
8 p.
|
artikel
|
| 23 |
Buffet and buffeting control in transonic flow
|
Caruana, D.
|
|
2005
|
|
7 |
p. 605-616
12 p.
|
artikel
|
| 24 |
Calculation of G I for a multidirectional composite double cantilever beam on two-parametric elastic foundation
|
Shokrieh, M.M.
|
|
2011
|
|
7 |
p. 534-543
10 p.
|
artikel
|
| 25 |
Closed loop roll control using aeroelastic information
|
Cronander, Carin
|
|
2000
|
|
7 |
p. 481-494
14 p.
|
artikel
|
| 26 |
Cold spray deposition: Significance of particle impact phenomena
|
Klinkov, Sergei Vladimirovich
|
|
2005
|
|
7 |
p. 582-591
10 p.
|
artikel
|
| 27 |
Collocation of two GEO satellites and one inclined GSO satellite
|
Lee, Byoung-Sun
|
|
2000
|
|
7 |
p. 507-515
9 p.
|
artikel
|
| 28 |
Concept and numerical model of a highly efficient thruster for a small reaction control system
|
Boronin, E.V
|
|
1998
|
|
7 |
p. 451-459
9 p.
|
artikel
|
| 29 |
Controller design for high-order descriptor linear systems based on requirements on tracking performance and disturbance rejection
|
Liu, Yicheng
|
|
2009
|
|
7 |
p. 364-373
10 p.
|
artikel
|
| 30 |
Control of shear perturbation in coaxial swirling turbulent jets
|
Lee, Wonjoong
|
|
2010
|
|
7 |
p. 472-486
15 p.
|
artikel
|
| 31 |
Correlations for heat generation and outer ring temperature of high speed and highly loaded ball bearings in an aero-engine
|
Flouros, Michael
|
|
2006
|
|
7 |
p. 611-617
7 p.
|
artikel
|
| 32 |
Design and aerodynamic analysis of a flapping-wing micro aerial vehicle
|
Tsai, Bor-Jang
|
|
2009
|
|
7 |
p. 383-392
10 p.
|
artikel
|
| 33 |
Design and CFD analysis of a regenerator for a turboshaft helicopter engine
|
Kumar Cheeda, Vijaya
|
|
2008
|
|
7 |
p. 524-534
11 p.
|
artikel
|
| 34 |
Design of a high precision differential altitude sensor (Statoskop)
|
Abdelmoula, Fethi
|
|
2001
|
|
7 |
p. 483-491
9 p.
|
artikel
|
| 35 |
Development of an electro-optical system for small UAV
|
Kim, Jong-hun
|
|
2010
|
|
7 |
p. 505-511
7 p.
|
artikel
|
| 36 |
Discontinuous Galerkin methods for computational aerodynamics — 3D adaptive flow simulation with the DLR PADGE code
|
Hartmann, R.
|
|
2010
|
|
7 |
p. 512-519
8 p.
|
artikel
|
| 37 |
Doppler global velocimetry for the analysis of combustor flows
|
Schodl, Richard
|
|
2002
|
|
7 |
p. 481-493
13 p.
|
artikel
|
| 38 |
Dynamic CAD objects for structural optimization in preliminary aircraft design
|
Ledermann, Christof
|
|
2006
|
|
7 |
p. 601-610
10 p.
|
artikel
|
| 39 |
Editorial Board
|
|
|
2010
|
|
7 |
p. IFC-
1 p.
|
artikel
|
| 40 |
Editorial Board
|
|
|
2006
|
|
7 |
p. CO2-
1 p.
|
artikel
|
| 41 |
Editorial Board
|
|
|
2005
|
|
7 |
p. CO2-
1 p.
|
artikel
|
| 42 |
Editorial Board
|
|
|
2004
|
|
7 |
p. IFC-
1 p.
|
artikel
|
| 43 |
Editorial Board
|
|
|
2008
|
|
7 |
p. IFC-
1 p.
|
artikel
|
| 44 |
Editorial Board
|
|
|
2009
|
|
7 |
p. IFC-
1 p.
|
artikel
|
| 45 |
Editorial Board
|
|
|
2011
|
|
7 |
p. IFC-
1 p.
|
artikel
|
| 46 |
Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)
|
Elsayed, Omer A.
|
|
2011
|
|
7 |
p. 555-566
12 p.
|
artikel
|
| 47 |
Effects of active cooling on the metal thermal protection systems
|
Liu, Shuang
|
|
2011
|
|
7 |
p. 526-533
8 p.
|
artikel
|
| 48 |
E/I-vector separation for safe switching of the GRACE formation
|
Montenbruck, Oliver
|
|
2006
|
|
7 |
p. 628-635
8 p.
|
artikel
|
| 49 |
Erratum to “Drag/thrust analysis of jet-propelled transonic transport aircraft; Definition of physical drag components” [Aerospace Science and Technology 8 (6) (2004) 545–556]
|
van der Vooren, J.
|
|
2004
|
|
7 |
p. 671-
1 p.
|
artikel
|
| 50 |
Evader maneuver on consideration of energy consumption in flight vehicle interception scenarios
|
Guo, Yang
|
|
2011
|
|
7 |
p. 519-525
7 p.
|
artikel
|
| 51 |
Excitation of instabilities in the wake of an airfoil by means of active winglets ☆ ☆ This article was presented at the German Aerospace Congress 2005.
|
Kauertz, Sebastian
|
|
2006
|
|
7 |
p. 551-562
12 p.
|
artikel
|
| 52 |
Experimental and numerical simulations of idealized aircraft cabin flows
|
Günther, Gero
|
|
2006
|
|
7 |
p. 563-573
11 p.
|
artikel
|
| 53 |
Experimental and numerical study of the Mars Pathfinder vehicle
|
Bur, R.
|
|
2003
|
|
7 |
p. 510-516
7 p.
|
artikel
|
| 54 |
Experimental investigation of a pitching airfoil in transonic flow ☆ ☆ This article was presented at the German Aerospace Congress 2002.
|
Hillenherms, C.
|
|
2004
|
|
7 |
p. 583-590
8 p.
|
artikel
|
| 55 |
Experimental investigation of a single trapped-vortex combustor with a slight temperature raise
|
Xing, Fei
|
|
2010
|
|
7 |
p. 520-525
6 p.
|
artikel
|
| 56 |
Experimental study on the PRE-X vehicle focusing on the transitional shock-wave/boundary-layer interactions
|
Bur, R.
|
|
2009
|
|
7 |
p. 393-401
9 p.
|
artikel
|
| 57 |
Fusion algorithm of correlated local estimates
|
Qiu, Hong Zhuan
|
|
2004
|
|
7 |
p. 619-626
8 p.
|
artikel
|
| 58 |
GPS clock correction estimation for near real-time orbit determination applications
|
Bock, H.
|
|
2009
|
|
7 |
p. 415-422
8 p.
|
artikel
|
| 59 |
Hole size and crack length models for spacecraft walls under oblique hypervelocity projectile impact
|
Schonberg, William P.
|
|
1999
|
|
7 |
p. 461-471
11 p.
|
artikel
|
| 60 |
Hydrodynamic simulation of a stationary plasma thruster in steady state regime
|
Mirshams, M.
|
|
2009
|
|
7 |
p. 402-405
4 p.
|
artikel
|
| 61 |
Identification of modal parameters, generalized and effective masses during base-driven tests
|
Füllekrug, U
|
|
1998
|
|
7 |
p. 469-480
12 p.
|
artikel
|
| 62 |
Identification of the high-temperature impact/friction of aeroengine blades and cases by micro Raman spectroscopy
|
Colomban, Philippe
|
|
1999
|
|
7 |
p. 447-459
13 p.
|
artikel
|
| 63 |
Ignition of cryogenic H2/LOX sprays
|
Gurliat, O.
|
|
2003
|
|
7 |
p. 517-531
15 p.
|
artikel
|
| 64 |
In-orbit repositioning of multiple solar sail spacecraft
|
Mengali, Giovanni
|
|
2008
|
|
7 |
p. 506-514
9 p.
|
artikel
|
| 65 |
Instrumentation of remote controlled airship “Lotte” for in-flight measurements
|
Kungl, Peter
|
|
2004
|
|
7 |
p. 599-610
12 p.
|
artikel
|
| 66 |
Inverse method in tilt-rotor optimization
|
Soykasap, Ömer
|
|
2001
|
|
7 |
p. 437-444
8 p.
|
artikel
|
| 67 |
Investigation of dynamic stall onset
|
Geissler, W.
|
|
2006
|
|
7 |
p. 590-600
11 p.
|
artikel
|
| 68 |
Low-NOx Combustor Development pursued within the scope of the Engine 3E German national research program in a cooperative effort among engine Manufacturer MTU, University of Karlsruhe and DLR German Aerospace Research Center
|
Zarzalis, Nikolaos
|
|
2002
|
|
7 |
p. 531-544
14 p.
|
artikel
|
| 69 |
Mechanical investigation of a multi-layer reflectarray for Ku-band space antennas
|
Datashvili, Leri
|
|
2006
|
|
7 |
p. 618-627
10 p.
|
artikel
|
| 70 |
MIRACLE – a joint DLR/ONERA effort on harmonization and development of industrial and research aerodynamic computational environment
|
Cambier, L.
|
|
2008
|
|
7 |
p. 555-566
12 p.
|
artikel
|
| 71 |
Modeling and control issues for autonomous aerial refueling for UAVs using a probe–drogue refueling system
|
Fravolini, Mario Luca
|
|
2004
|
|
7 |
p. 611-618
8 p.
|
artikel
|
| 72 |
Modeling of anisotropic turbulence in rapid rotation
|
Schiestel, R
|
|
1997
|
|
7 |
p. 441-451
11 p.
|
artikel
|
| 73 |
Modelling of the atomization of a plain liquid fuel jet in crossflow at gas turbine conditions
|
Rachner, Michael
|
|
2002
|
|
7 |
p. 495-506
12 p.
|
artikel
|
| 74 |
Model simulations of fuel sulfur conversion efficiencies in an aircraft engine: Dependence on reaction rate constants and initial species mixing ratios
|
Tremmel, Hans Georg
|
|
1999
|
|
7 |
p. 417-430
14 p.
|
artikel
|
| 75 |
Navigation and steering during manual rendezvous with the space station
|
Polovnikov, Oleg
|
|
2004
|
|
7 |
p. 645-651
7 p.
|
artikel
|
| 76 |
New microstructures in ceramic materials from the melt for high temperature applications
|
Mazerolles, Léo
|
|
2008
|
|
7 |
p. 499-505
7 p.
|
artikel
|
| 77 |
Numerical approach for assessment of dynamic strength for riveted joints
|
Langrand, Bertrand
|
|
1999
|
|
7 |
p. 431-446
16 p.
|
artikel
|
| 78 |
Numerical investigation of turbulent hydrogen combustion in a SCRAMJET using flamelet modeling
|
Oevermann, Michael
|
|
2000
|
|
7 |
p. 463-480
18 p.
|
artikel
|
| 79 |
Numerical simulation of the reactive two-phase flow in a kerosene/air tubular combustor
|
Zamuner, B.
|
|
2002
|
|
7 |
p. 521-529
9 p.
|
artikel
|
| 80 |
Numerical study of buffet and transonic flutter on the NLR 7301 airfoil
|
Geissler, W.
|
|
2003
|
|
7 |
p. 540-550
11 p.
|
artikel
|
| 81 |
On-ground aircraft control design using a parameter-varying anti-windup approach
|
Roos, Clément
|
|
2010
|
|
7 |
p. 459-471
13 p.
|
artikel
|
| 82 |
On the validation of high enthalpy wind tunnel simulations
|
Sagnier, P.
|
|
1998
|
|
7 |
p. 425-437
13 p.
|
artikel
|
| 83 |
Operational limits for reusable space transportation systems due to physical boundaries of C/SiC materials
|
Hald, Hermann
|
|
2003
|
|
7 |
p. 551-559
9 p.
|
artikel
|
| 84 |
Operational use of guided reentry capsules – system design solutions and mission safety considerations ☆ ☆ This article was presented at the German Aerospace Congress 2002.
|
Burkhardt, Johannes
|
|
2004
|
|
7 |
p. 635-644
10 p.
|
artikel
|
| 85 |
Optimal air-launching rocket design using system trades and a multi-disciplinary optimization approach
|
Choi, Young Chang
|
|
2009
|
|
7 |
p. 406-414
9 p.
|
artikel
|
| 86 |
Optimal trajectory planning for flight through microburst wind shears
|
Pourtakdoust, Seid H.
|
|
2011
|
|
7 |
p. 567-576
10 p.
|
artikel
|
| 87 |
Optimized design of an active extrados structure for an experimental morphing laminar wing
|
Coutu, Daniel
|
|
2010
|
|
7 |
p. 451-458
8 p.
|
artikel
|
| 88 |
PD-fuzzy formation control for spacecraft formation flying in elliptical orbits
|
Pengji, Wang
|
|
2003
|
|
7 |
p. 561-566
6 p.
|
artikel
|
| 89 |
Performance and preliminary life test of a low power hydrazine engineering design model arcjet
|
Tang, Hai-bin
|
|
2011
|
|
7 |
p. 577-588
12 p.
|
artikel
|
| 90 |
Planning and scheduling algorithms for the COSMO-SkyMed constellation
|
Bianchessi, Nicola
|
|
2008
|
|
7 |
p. 535-544
10 p.
|
artikel
|
| 91 |
Preliminary study to raise axial flow compressors up to the context-awareness standards
|
Aryana, Babak
|
|
2008
|
|
7 |
p. 515-523
9 p.
|
artikel
|
| 92 |
Preventing runway incursions and conflicts
|
Singh, G.K.
|
|
2004
|
|
7 |
p. 653-670
18 p.
|
artikel
|
| 93 |
Pulse modulation for attitude control with thrusters subject to switching restrictions ☆ ☆ This article should be presented at the German Aerospace Congress 2005.
|
Kienitz, Karl Heinz
|
|
2005
|
|
7 |
p. 635-640
6 p.
|
artikel
|
| 94 |
Realization of an optimized wing camber by using formvariable flap structures
|
Monner, Hans Peter
|
|
2001
|
|
7 |
p. 445-455
11 p.
|
artikel
|
| 95 |
Real time drag minimization using redundant control surfaces
|
Jacobsen, Marianne
|
|
2006
|
|
7 |
p. 574-580
7 p.
|
artikel
|
| 96 |
Regression rate estimation for standard-flow hybrid rocket engines
|
Greatrix, David R.
|
|
2009
|
|
7 |
p. 358-363
6 p.
|
artikel
|
| 97 |
Rendezvous phasing special-point maneuvers mixed discrete-continuous optimization using simulated annealing
|
Luo, Ya-Zhong
|
|
2006
|
|
7 |
p. 652-658
7 p.
|
artikel
|
| 98 |
Research on integrated optimization design of hypersonic cruise vehicle
|
Che, Jing
|
|
2008
|
|
7 |
p. 567-572
6 p.
|
artikel
|
| 99 |
Role of parallelism in wavelet analysis of radar imaging
|
Roisin, M
|
|
1997
|
|
7 |
p. 489-501
13 p.
|
artikel
|
| 100 |
Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering
|
Liu, Hui
|
|
2006
|
|
7 |
p. 636-643
8 p.
|
artikel
|
| 101 |
Solar sail transfer trajectory from L1 point to sub-L1 point
|
Gong, Shengping
|
|
2011
|
|
7 |
p. 544-554
11 p.
|
artikel
|
| 102 |
Solution of viscous flow over heat shield using structured grid
|
Mehta, R.C.
|
|
1998
|
|
7 |
p. 415-423
9 p.
|
artikel
|
| 103 |
Space and time organisation of a shock wave/turbulent boundary layer interaction
|
Dupont, P.
|
|
2005
|
|
7 |
p. 561-572
12 p.
|
artikel
|
| 104 |
Spray characteristics of a liquid–liquid coaxial swirl atomizer at different mass flow rates
|
Soltani, M.R.
|
|
2005
|
|
7 |
p. 592-604
13 p.
|
artikel
|
| 105 |
Synthesis of copper chromite catalyst
|
Kawamoto, Aparecida M.
|
|
2004
|
|
7 |
p. 591-598
8 p.
|
artikel
|
| 106 |
Tethered dual spacecraft configuration: a solution to attitude control problems
|
Kumar, Krishna
|
|
2000
|
|
7 |
p. 495-505
11 p.
|
artikel
|
| 107 |
The anchoring of gaseous jet diffusion flames in stagnant air
|
Kurdyumov, Vadim
|
|
2002
|
|
7 |
p. 507-516
10 p.
|
artikel
|
| 108 |
The study on electromagnetic compatibility of DC electric motor in HAPS
|
Geng, Junping
|
|
2005
|
|
7 |
p. 617-625
9 p.
|
artikel
|
| 109 |
The total minimum impulse for orbit atmospheric plane change
|
Marinescu, A
|
|
1998
|
|
7 |
p. 461-467
7 p.
|
artikel
|
| 110 |
Three-dimensional measurement of velocity, velocity gradients and related properties in turbulent flows
|
Lemonis, G.
|
|
1997
|
|
7 |
p. 453-461
9 p.
|
artikel
|
| 111 |
Tightly coupled GPS/INS integration for missile applications
|
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