| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A comparative study on acoustic damping induced by half-wave, quarter-wave, and Helmholtz resonators
|
Sohn, Chae Hoon
|
|
2011
|
|
8 |
p. 606-614
9 p.
|
artikel
|
| 2 |
Active sidestick technology – a means for improving situational awareness
|
Hanke, Dietrich
|
|
1999
|
|
8 |
p. 525-532
8 p.
|
artikel
|
| 3 |
Advanced aerothermodynamic analysis of SHEFEX I
|
Barth, Tarik
|
|
2010
|
|
8 |
p. 587-593
7 p.
|
artikel
|
| 4 |
Aerodynamics of smart flap under ground effect
|
Djavareshkian, M.H.
|
|
2011
|
|
8 |
p. 642-652
11 p.
|
artikel
|
| 5 |
Aircraft maneuverability improvement by direct lift control system application
|
Tomczyk, Andrzej
|
|
2005
|
|
8 |
p. 692-700
9 p.
|
artikel
|
| 6 |
A lightning swept stroke model: A valuable tool to investigate the lightning strike to aircraft
|
Broc, Alain
|
|
2006
|
|
8 |
p. 700-708
9 p.
|
artikel
|
| 7 |
A new approach to on-board stationkeeping of GEO-satellites
|
Park, Bong-Kyu
|
|
2005
|
|
8 |
p. 722-731
10 p.
|
artikel
|
| 8 |
An experimental investigation on the aerodynamic performances of flexible membrane wings in flapping flight
|
Hu, Hui
|
|
2010
|
|
8 |
p. 575-586
12 p.
|
artikel
|
| 9 |
Annual contents 1997
|
|
|
1998
|
|
8 |
p. 537-539
3 p.
|
artikel
|
| 10 |
Annual contents 1998
|
|
|
1998
|
|
8 |
p. 541-543
3 p.
|
artikel
|
| 11 |
Anti-skid induced aircraft landing gear instability
|
Gualdi, Stefania
|
|
2008
|
|
8 |
p. 627-637
11 p.
|
artikel
|
| 12 |
A rendezvous navigation algorithm for orbit determination, based on visual measurements by space vehicle crew members
|
Polovnikov, Oleg
|
|
2000
|
|
8 |
p. 567-575
9 p.
|
artikel
|
| 13 |
A simple and accurate method for computing stress intensity factors of collinear interacting cracks
|
Millwater, Harry R.
|
|
2010
|
|
8 |
p. 542-550
9 p.
|
artikel
|
| 14 |
Assistant systems for aircraft guidance: cognitive man-machine cooperation
|
Onken, Reiner
|
|
2001
|
|
8 |
p. 511-520
10 p.
|
artikel
|
| 15 |
A systematic approach to nonlinear rotorcraft model identification
|
Krämer, Philipp
|
|
2002
|
|
8 |
p. 579-590
12 p.
|
artikel
|
| 16 |
Author index 1997
|
|
|
1998
|
|
8 |
p. 540-
1 p.
|
artikel
|
| 17 |
Author index 1998
|
|
|
1998
|
|
8 |
p. 544-
1 p.
|
artikel
|
| 18 |
Author index Vol. 6, 2002
|
|
|
2003
|
|
8 |
p. 645-646
2 p.
|
artikel
|
| 19 |
Author index Vol. 7, 2003
|
|
|
2003
|
|
8 |
p. 651-652
2 p.
|
artikel
|
| 20 |
Author index Vol. 10, 2006
|
|
|
2006
|
|
8 |
p. 721-722
2 p.
|
artikel
|
| 21 |
Author index Vol. 9, 2005
|
|
|
2005
|
|
8 |
p. 750-751
2 p.
|
artikel
|
| 22 |
Author index Vol. 8, 2004
|
|
|
2004
|
|
8 |
p. 739-740
2 p.
|
artikel
|
| 23 |
Calculation of the transonic dip of airfoils using viscous-inviscid aerodynamic interaction method
|
Sekar, Widjaja Kresna
|
|
2005
|
|
8 |
p. 661-671
11 p.
|
artikel
|
| 24 |
Calibration of the MERIC full-polarimetric radar: theory and implementation
|
Titin-Schnaider, C.
|
|
2003
|
|
8 |
p. 633-640
8 p.
|
artikel
|
| 25 |
Chaotic artificial bee colony approach to Uninhabited Combat Air Vehicle (UCAV) path planning
|
Xu, Chunfang
|
|
2010
|
|
8 |
p. 535-541
7 p.
|
artikel
|
| 26 |
Comparison of computational and experimental results in vibroacoustic active control using piezoelectric film technology
|
Meidinger, N
|
|
1997
|
|
8 |
p. 573-580
8 p.
|
artikel
|
| 27 |
Concepts of user centered automation
|
Kraiss, Karl-Friedrich
|
|
2001
|
|
8 |
p. 505-510
6 p.
|
artikel
|
| 28 |
Contents list Vol. 6, 2002
|
|
|
2003
|
|
8 |
p. 641-644
4 p.
|
artikel
|
| 29 |
Contents list Vol. 7, 2003
|
|
|
2003
|
|
8 |
p. 647-650
4 p.
|
artikel
|
| 30 |
Contents list Vol. 10, 2006
|
|
|
2006
|
|
8 |
p. 715-719
5 p.
|
artikel
|
| 31 |
Contents list Vol. 9, 2005
|
|
|
2005
|
|
8 |
p. 745-749
5 p.
|
artikel
|
| 32 |
Contents list Vol. 8, 2004
|
|
|
2004
|
|
8 |
p. 735-738
4 p.
|
artikel
|
| 33 |
Control of forced shock-wave oscillations and separated boundary layer interaction
|
Galli, Arnaud
|
|
2005
|
|
8 |
p. 653-660
8 p.
|
artikel
|
| 34 |
Critical wake vortex encounter scenarios ☆ ☆ This article was presented at the German Aerospace Congress 2003.
|
Höhne, Gordon
|
|
2004
|
|
8 |
p. 689-701
13 p.
|
artikel
|
| 35 |
2D and 3D aerodynamic shape optimisation using the adjoint approach
|
Brezillon, J.
|
|
2004
|
|
8 |
p. 715-727
13 p.
|
artikel
|
| 36 |
Depeaking – economic optimization of air traffic systems ☆ ☆ This article was presented at the German Aerospace Congress 2004.
|
Frank, Michael
|
|
2005
|
|
8 |
p. 738-744
7 p.
|
artikel
|
| 37 |
Deployable space structure control using adaptive predictive controller with notch filter
|
Oh, Choong-Seok
|
|
2009
|
|
8 |
p. 459-465
7 p.
|
artikel
|
| 38 |
Detonation waves induced by a confined wedge
|
Lu, Frank K.
|
|
2006
|
|
8 |
p. 679-685
7 p.
|
artikel
|
| 39 |
3-D grain burnback analysis of solid propellant rocket motors: Part 1 – ballistic motor tests
|
Püskülcü, G.
|
|
2008
|
|
8 |
p. 579-584
6 p.
|
artikel
|
| 40 |
3-D grain burnback analysis of solid propellant rocket motors: Part 2 – modeling and simulations
|
Püskülcü, G.
|
|
2008
|
|
8 |
p. 585-591
7 p.
|
artikel
|
| 41 |
EDA toolbox for VHF Data Link system simulation
|
Flühr, Holger
|
|
2008
|
|
8 |
p. 599-607
9 p.
|
artikel
|
| 42 |
Editorial Board
|
|
|
2009
|
|
8 |
p. IFC-
1 p.
|
artikel
|
| 43 |
Editorial Board
|
|
|
2010
|
|
8 |
p. IFC-
1 p.
|
artikel
|
| 44 |
Editorial Board
|
|
|
2006
|
|
8 |
p. CO2-
1 p.
|
artikel
|
| 45 |
Editorial Board
|
|
|
2005
|
|
8 |
p. CO2-
1 p.
|
artikel
|
| 46 |
Editorial Board
|
|
|
2008
|
|
8 |
p. IFC-
1 p.
|
artikel
|
| 47 |
Editorial Board
|
|
|
2004
|
|
8 |
p. CO2-
1 p.
|
artikel
|
| 48 |
Editorial Board
|
|
|
2011
|
|
8 |
p. IFC-
1 p.
|
artikel
|
| 49 |
Editorial: ‘Progress in cockpit and air traffic control automation’
|
Winter, Heinz
|
|
2001
|
|
8 |
p. 493-494
2 p.
|
artikel
|
| 50 |
Effect of ceramic nozzle on performance of pulsed plasma thruster
|
Hou, Dali
|
|
2008
|
|
8 |
p. 573-578
6 p.
|
artikel
|
| 51 |
Effect of non-uniform basic temperature gradient on the onset of Marangoni convection in a fluid with suspended particles
|
Rudraiah, Nanjundappa
|
|
2000
|
|
8 |
p. 517-523
7 p.
|
artikel
|
| 52 |
Effect of wall suction on leading edge contamination
|
Arnal, D
|
|
1997
|
|
8 |
p. 505-517
13 p.
|
artikel
|
| 53 |
e N transition prediction for 3D wing configurations using database methods and a local, linear stability code
|
Krumbein, Andreas
|
|
2008
|
|
8 |
p. 592-598
7 p.
|
artikel
|
| 54 |
ESTIMA – an integrated software tool for nonlinear parameter estimation
|
Jategaonkar, Ravindra
|
|
2002
|
|
8 |
p. 565-578
14 p.
|
artikel
|
| 55 |
Estimation of moving heat sources with a three-dimensional unsteady inverse method
|
Nortershauser, David
|
|
2001
|
|
8 |
p. 529-540
12 p.
|
artikel
|
| 56 |
Euler computation of the nearfield wake vortex of an aircraft in take-off configuration
|
Stumpf, Eike
|
|
2000
|
|
8 |
p. 535-543
9 p.
|
artikel
|
| 57 |
Evaluation of airborne data link communication
|
Müller, Thomas
|
|
2001
|
|
8 |
p. 521-527
7 p.
|
artikel
|
| 58 |
Evolution of Ni-based superalloys for single crystal gas turbine blade applications
|
Caron, Pierre
|
|
1999
|
|
8 |
p. 513-523
11 p.
|
artikel
|
| 59 |
Experimental investigation of hot and cold side jet interaction with a supersonic cross-flow
|
Stahl, Bernhard
|
|
2009
|
|
8 |
p. 488-496
9 p.
|
artikel
|
| 60 |
Experimental investigation of isolated inlets for high agile missiles
|
Herrmann, Dirk
|
|
2006
|
|
8 |
p. 659-667
9 p.
|
artikel
|
| 61 |
Experimental investigations on hull-fin interferences of the LOTTE airship
|
Funk, Peter
|
|
2003
|
|
8 |
p. 603-610
8 p.
|
artikel
|
| 62 |
Flap contour optimization for highly integrated SERN nozzles
|
Gruhn, Patrick
|
|
2000
|
|
8 |
p. 555-565
11 p.
|
artikel
|
| 63 |
Flexible aircraft model identification for control law design
|
Bucharles, A
|
|
2002
|
|
8 |
p. 591-598
8 p.
|
artikel
|
| 64 |
Flow visualization study of an airship model using a water towing tank
|
Beheshti, Behnam H.
|
|
2009
|
|
8 |
p. 450-458
9 p.
|
artikel
|
| 65 |
Free oscillations and response of a viscous liquid in a rigid circular cylindrical tank
|
Bauer, Helmut F.
|
|
1999
|
|
8 |
p. 495-512
18 p.
|
artikel
|
| 66 |
Fuel mass penalty due to generators and fuel cells as energy source of the all-electric aircraft ☆ ☆ This article was presented at the German Aerospace Congress 2005. ☆☆ ☆☆ The article was published in a similar form previously at the German Aerospace Congress. Discrepancies between the results come due to slight changes in the engine and the flight performance model.
|
Dollmayer, Jürgen
|
|
2006
|
|
8 |
p. 686-694
9 p.
|
artikel
|
| 67 |
Gaseous cavity at the base of an underwater projectile
|
Dyment, A
|
|
1998
|
|
8 |
p. 489-504
16 p.
|
artikel
|
| 68 |
Grid-optimized upwind dispersion-relation-preserving scheme on non-uniform Cartesian grids for computational aeroacoustics
|
Si, Hai-qing
|
|
2008
|
|
8 |
p. 608-617
10 p.
|
artikel
|
| 69 |
Hazard criteria for wake vortex encounters during approach
|
Luckner, Robert
|
|
2004
|
|
8 |
p. 673-687
15 p.
|
artikel
|
| 70 |
Identification of a 2D turbulent wind spectrum
|
Mouyon, Ph
|
|
2002
|
|
8 |
p. 599-605
7 p.
|
artikel
|
| 71 |
Improvement of forebody/inlet integration for hypersonic vehicle
|
Bissinger, N.C
|
|
1998
|
|
8 |
p. 505-514
10 p.
|
artikel
|
| 72 |
Increasing robustness, reliability and ergonomics in speech interfaces for aerial control systems
|
Ferreiros, Javier
|
|
2009
|
|
8 |
p. 423-430
8 p.
|
artikel
|
| 73 |
Index
|
|
|
1999
|
|
8 |
p. 533-535
3 p.
|
artikel
|
| 74 |
Index
|
|
|
1999
|
|
8 |
p. 537-
1 p.
|
artikel
|
| 75 |
Inflatable kites using the concept of Tensairity
|
Breuer, Joep C.M.
|
|
2010
|
|
8 |
p. 557-563
7 p.
|
artikel
|
| 76 |
Instability and unsteadiness of aircraft wake vortices
|
Jacquin, L.
|
|
2003
|
|
8 |
p. 577-593
17 p.
|
artikel
|
| 77 |
Interference-free wind tunnel testing of jet propelled missiles
|
Korst, H.H.
|
|
1998
|
|
8 |
p. 481-488
8 p.
|
artikel
|
| 78 |
Internal fuselage noise: comparison of computations and tests on a Falcon airframe
|
Guillaumie, Laurent
|
|
2000
|
|
8 |
p. 545-554
10 p.
|
artikel
|
| 79 |
Lift coefficient prediction at high angle of attack using recurrent neural network
|
Suresh, S.
|
|
2003
|
|
8 |
p. 595-602
8 p.
|
artikel
|
| 80 |
Lightning strike to helicopters during winter thunderstorms over North Sea
|
Broc, A.
|
|
2005
|
|
8 |
p. 686-691
6 p.
|
artikel
|
| 81 |
Man-machine-interface in modern transport systems from an aviation safety perspective
|
Baberg, Thomas W
|
|
2001
|
|
8 |
p. 495-504
10 p.
|
artikel
|
| 82 |
Material optimization: bridging the gap between conceptual and preliminary design
|
Hörnlein, H.R.E.M
|
|
2001
|
|
8 |
p. 541-554
14 p.
|
artikel
|
| 83 |
Modeling the moisture effects of solid ingredients on composite propellant properties
|
Iqbal, Muhammad Mazhar
|
|
2006
|
|
8 |
p. 695-699
5 p.
|
artikel
|
| 84 |
Modelling and design of wing tip devices at various flight conditions using a databased aerodynamic prediction tool ☆ ☆ This article was presented at the German Aerospace Congress 2004.
|
Büscher, Alexander
|
|
2006
|
|
8 |
p. 668-678
11 p.
|
artikel
|
| 85 |
Modelling of perforated plate aerodynamics performance
|
Doerffer, Piotr P.
|
|
2000
|
|
8 |
p. 525-534
10 p.
|
artikel
|
| 86 |
Multiobjective Target Feedback Loop / Loop Transfer Recovery (TFL/LTR) design with application to aircraft lateral control in high incidence regime
|
Kienitz, K.H.
|
|
1998
|
|
8 |
p. 515-523
9 p.
|
artikel
|
| 87 |
New asymmetry monitoring techniques: Effects on attitude control
|
Borello, Lorenzo
|
|
2009
|
|
8 |
p. 475-487
13 p.
|
artikel
|
| 88 |
New criterion for aircraft susceptibility to infrared guided missiles
|
Rao, G. Arvind
|
|
2005
|
|
8 |
p. 701-712
12 p.
|
artikel
|
| 89 |
[No title]
|
Thomas, Fred
|
|
2003
|
|
8 |
p. 567-
1 p.
|
artikel
|
| 90 |
[No title]
|
Thielecke, Frank
|
|
2002
|
|
8 |
p. 563-
1 p.
|
artikel
|
| 91 |
Novel intelligent water drops optimization approach to single UCAV smooth trajectory planning
|
Duan, Haibin
|
|
2009
|
|
8 |
p. 442-449
8 p.
|
artikel
|
| 92 |
On the free-vibration of rotating composite beams using a higher-order shear formulation
|
Chandiramani, N.K
|
|
2002
|
|
8 |
p. 545-561
17 p.
|
artikel
|
| 93 |
Optimal control in the east/west station-keeping manoeuvres for geostationary satellites
|
Romero, Pilar
|
|
2004
|
|
8 |
p. 729-734
6 p.
|
artikel
|
| 94 |
Optimization of the tether-assisted return mission of a guided re-entry capsule
|
Zimmermann, Frank
|
|
2005
|
|
8 |
p. 713-721
9 p.
|
artikel
|
| 95 |
Optimum detection and location estimation of target lines in the range-time space of a search radar
|
Moqiseh, A.
|
|
2011
|
|
8 |
p. 627-634
8 p.
|
artikel
|
| 96 |
Optimum Gurney flap height determination for “lost-lift” recovery in compressible dynamic stall control
|
Chandrasekhara, M.S.
|
|
2010
|
|
8 |
p. 551-556
6 p.
|
artikel
|
| 97 |
Orbital steady motions of a system of two bodies with an elastic connection
|
Abrarova, E.V
|
|
1998
|
|
8 |
p. 525-535
11 p.
|
artikel
|
| 98 |
Oscillations of a viscous liquid in a cylindrical container
|
Bauer, Helmut F
|
|
1997
|
|
8 |
p. 519-532
14 p.
|
artikel
|
| 99 |
Performance prediction and flowfield analysis of rotors in hover, using a coupled Euler/boundary layer method
|
Beaumier, Philippe
|
|
1999
|
|
8 |
p. 473-484
12 p.
|
artikel
|
| 100 |
Prediction of aerodynamic characteristics of an aircraft model with and without winglet using fuzzy logic technique
|
Hossain, Altab
|
|
2011
|
|
8 |
p. 595-605
11 p.
|
artikel
|
| 101 |
Quadratic extended Kalman filter approach for GPS/INS integration
|
Wang, Wei
|
|
2006
|
|
8 |
p. 709-713
5 p.
|
artikel
|
| 102 |
RANS analysis of the low-Reynolds number flow around the SD7003 airfoil
|
Catalano, P.
|
|
2011
|
|
8 |
p. 615-626
12 p.
|
artikel
|
| 103 |
Robust and efficient computation of turbulent flows around civil transport aircraft at flight Reynolds numbers
|
Fassbender, Jens K.
|
|
2005
|
|
8 |
p. 672-680
9 p.
|
artikel
|
| 104 |
Shimmy analysis of a simple aircraft nose landing gear model using different mathematical methods
|
Somieski, Gerhard
|
|
1997
|
|
8 |
p. 545-555
11 p.
|
artikel
|
| 105 |
Simulation of asymmetric landing and typical ground maneuvers for large transport aircraft
|
Khapane, Prashant Dilip
|
|
2003
|
|
8 |
p. 611-619
9 p.
|
artikel
|
| 106 |
Simulation of streamwise vortices at the flaps of re-entry vehicles
|
Lüdeke, Heinrich
|
|
2004
|
|
8 |
p. 703-714
12 p.
|
artikel
|
| 107 |
Simulation of unsteady combustion in a LOX-GH2 fueled rocket engine
|
Masquelet, M.
|
|
2009
|
|
8 |
p. 466-474
9 p.
|
artikel
|
| 108 |
Simultaneous spacecraft attitude and orbit estimation using magnetic field vector measurements
|
Abdelrahman, Mohammad
|
|
2011
|
|
8 |
p. 653-669
17 p.
|
artikel
|
| 109 |
Solar sail trajectories with piecewise-constant steering laws
|
Mengali, Giovanni
|
|
2009
|
|
8 |
p. 431-441
11 p.
|
artikel
|
| 110 |
Solving a radiation problem with forward speed using a lifting surface method with a Green's function
|
Nontakaew, U
|
|
1997
|
|
8 |
p. 533-543
11 p.
|
artikel
|
| 111 |
Spacecraft optimal rendezvous controller design using simulated annealing
|
Luo, Ya-zhong
|
|
2005
|
|
8 |
p. 732-737
6 p.
|
artikel
|
| 112 |
Structural assessment of a solid propellant rocket motor: Effects of aging and damage
|
Yıldırım, H.C.
|
|
2011
|
|
8 |
p. 635-641
7 p.
|
artikel
|
| 113 |
Technology review of aeroengine pollutant emissions
|
Wulff, A.
|
|
1997
|
|
8 |
p. 557-572
16 p.
|
artikel
|
| 114 |
Theoretical aerothermal concepts for configuration design of hypersonic vehicles
|
Mahulikar, Shripad P.
|
|
2005
|
|
8 |
p. 681-685
5 p.
|
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| 115 |
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Hubner, J.P.
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2011
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p. 670-680
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|
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| 116 |
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Séraudie, A.
|
|
2003
|
|
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p. 569-576
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|
artikel
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| 117 |
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Sachs, G
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p. 621-631
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| 118 |
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| 119 |
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Díaz, J.
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| 120 |
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| 121 |
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Labbe, Steven G.
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1999
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p. 485-493
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