| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Advanced modelling of bird strike on high lift devices using hybrid Eulerian–Lagrangian formulation
|
Smojver, I.
|
|
2012
|
23 |
1 |
p. 224-232
9 p.
|
artikel
|
| 2 |
Aerodynamic and aerothermodynamic design of Future Launchers Preparatory Program concepts
|
Pezzella, Giuseppe
|
|
2012
|
23 |
1 |
p. 233-249
17 p.
|
artikel
|
| 3 |
Aerodynamic design prediction using surrogate-based modeling in genetic algorithm architecture
|
Pehlivanoglu, Y. Volkan
|
|
2012
|
23 |
1 |
p. 479-491
13 p.
|
artikel
|
| 4 |
Aid tool for the design of process and aircraft assembly lines
|
Anselmetti, Bernard
|
|
2012
|
23 |
1 |
p. 387-398
12 p.
|
artikel
|
| 5 |
Airborne GMTI experiment based on multi-channel synthetic aperture radar using space time adaptive processing
|
Yang, Zhiwei
|
|
2012
|
23 |
1 |
p. 179-186
8 p.
|
artikel
|
| 6 |
A modelling framework for the calculation of structural loads for fatigue life prediction of helicopter airframe components
|
van der Ven, H.
|
|
2012
|
23 |
1 |
p. 26-33
8 p.
|
artikel
|
| 7 |
An accelerated BEM for simulation of noise control in the aircraft cabin
|
Mallardo, V.
|
|
2012
|
23 |
1 |
p. 418-428
11 p.
|
artikel
|
| 8 |
Analysis of zenith pass problem and tracking strategy design for roll–pitch seeker
|
Jiang, Huhai
|
|
2012
|
23 |
1 |
p. 345-351
7 p.
|
artikel
|
| 9 |
An innovative scheme for SINS/GPS ultra-tight integration system with low-grade IMU
|
Wang, Xin-long
|
|
2012
|
23 |
1 |
p. 452-460
9 p.
|
artikel
|
| 10 |
An interpolation tool for aerodynamic mesh deformation problems based on octree decomposition
|
Cordero-Gracia, M.
|
|
2012
|
23 |
1 |
p. 93-107
15 p.
|
artikel
|
| 11 |
An investigation of a tactical cargo aircraft aft body drag reduction based on CFD analysis and wind tunnel tests
|
Mirzaei, Masoud
|
|
2012
|
23 |
1 |
p. 263-269
7 p.
|
artikel
|
| 12 |
Application of parameter plane method to pilot-induced oscillations
|
Perng, Jau-Woei
|
|
2012
|
23 |
1 |
p. 140-145
6 p.
|
artikel
|
| 13 |
A study of the supersonic ejector–diffuser system with an inlet orifice
|
Lijo, Vincent
|
|
2012
|
23 |
1 |
p. 321-329
9 p.
|
artikel
|
| 14 |
Comprehensive approach for noise reduction in helicopter cabins
|
Caillet, Julien
|
|
2012
|
23 |
1 |
p. 17-25
9 p.
|
artikel
|
| 15 |
Contrail microphysics in the near wake of a realistic wing through RANS simulations
|
Guignery, F.
|
|
2012
|
23 |
1 |
p. 399-408
10 p.
|
artikel
|
| 16 |
Design and performance characterization of a sub-Newton N2O monopropellant thruster
|
Cai, Guobiao
|
|
2012
|
23 |
1 |
p. 439-451
13 p.
|
artikel
|
| 17 |
Design and simulation of fault tolerant flight control based on a physical approach
|
Lombaerts, T.J.J.
|
|
2012
|
23 |
1 |
p. 151-171
21 p.
|
artikel
|
| 18 |
Design methodology for under-slung store structure of air-borne Time Domain Electromagnetic (TDEM) system
|
Lahiri, S.K.
|
|
2012
|
23 |
1 |
p. 120-131
12 p.
|
artikel
|
| 19 |
Determining load distribution between the different rows of fasteners of a hybrid load transfer bolted joint assembly
|
Andriamampianina, José
|
|
2012
|
23 |
1 |
p. 312-320
9 p.
|
artikel
|
| 20 |
Development of a low cost star tracker for the SHEFEX mission
|
Samaan, Malak
|
|
2012
|
23 |
1 |
p. 469-478
10 p.
|
artikel
|
| 21 |
Development of EC 135 turbulence models via system identification
|
Seher-Weiss, S.
|
|
2012
|
23 |
1 |
p. 43-52
10 p.
|
artikel
|
| 22 |
Editorial Board
|
|
|
2012
|
23 |
1 |
p. IFC-
1 p.
|
artikel
|
| 23 |
Effects of geometric imperfections on the aeroelastic behavior of functionally graded wings in supersonic flow
|
Ghadimi, M.
|
|
2012
|
23 |
1 |
p. 492-504
13 p.
|
artikel
|
| 24 |
Efficient rotorcraft trajectory optimization using comprehensive models by improved shooting methods
|
Bottasso, Carlo L.
|
|
2012
|
23 |
1 |
p. 34-42
9 p.
|
artikel
|
| 25 |
Flow structure over the yawed nonslender diamond wing
|
Sahin, B.
|
|
2012
|
23 |
1 |
p. 108-119
12 p.
|
artikel
|
| 26 |
High-fidelity optimization framework for helicopter rotors
|
Imiela, Manfred
|
|
2012
|
23 |
1 |
p. 2-16
15 p.
|
artikel
|
| 27 |
Identification of weak non-linearities within complex aerospace structures
|
Fuellekrug, Ulrich
|
|
2012
|
23 |
1 |
p. 53-62
10 p.
|
artikel
|
| 28 |
Intelligent proportional-derivative control for flexible spacecraft attitude stabilization with unknown input saturation
|
Hu, Qinglei
|
|
2012
|
23 |
1 |
p. 63-74
12 p.
|
artikel
|
| 29 |
Inverse identification of continuously distributed loads using strain data
|
Nakamura, Toshiya
|
|
2012
|
23 |
1 |
p. 75-84
10 p.
|
artikel
|
| 30 |
Mathematical modeling and rapid recognition of hypersonic inlet buzz
|
Chang, Juntao
|
|
2012
|
23 |
1 |
p. 172-178
7 p.
|
artikel
|
| 31 |
Measurement and control of aircraft landing gear broadband noise
|
Li, Yong
|
|
2012
|
23 |
1 |
p. 213-223
11 p.
|
artikel
|
| 32 |
Modified Newton, rank-1 Broyden update and rank-2 BFGS update methods in helicopter trim: A comparative study
|
Chandra Sekhar, D.
|
|
2012
|
23 |
1 |
p. 187-200
14 p.
|
artikel
|
| 33 |
Neural networks based airfoil generation for a given C p using Bezier–PARSEC parameterization
|
Kharal, Athar
|
|
2012
|
23 |
1 |
p. 330-344
15 p.
|
artikel
|
| 34 |
Novel approach to dynamic shock attenuation and its validation through computational analysis
|
Ivanchenko, Oleksandr
|
|
2012
|
23 |
1 |
p. 146-150
5 p.
|
artikel
|
| 35 |
Numerical simulation of ice accretions on an aircraft wing
|
Cao, Yihua
|
|
2012
|
23 |
1 |
p. 296-304
9 p.
|
artikel
|
| 36 |
Optimization of transition maneuvers through aerodynamic vectoring
|
Maqsood, Adnan
|
|
2012
|
23 |
1 |
p. 363-371
9 p.
|
artikel
|
| 37 |
Output feedback back-stepping control for a generic Hypersonic Vehicle via small-gain theorem
|
Zong, Qun
|
|
2012
|
23 |
1 |
p. 409-417
9 p.
|
artikel
|
| 38 |
Pattern transition in spacecraft formation flying using bifurcating potential fields
|
Bennet, Derek J.
|
|
2012
|
23 |
1 |
p. 250-262
13 p.
|
artikel
|
| 39 |
Perturbative effects of antenna radiation reaction on artificial satellite orbit
|
Heilmann, A.
|
|
2012
|
23 |
1 |
p. 352-357
6 p.
|
artikel
|
| 40 |
Prediction of flutter characteristics for a transport wing with wingtip devices
|
Cui, Peng
|
|
2012
|
23 |
1 |
p. 461-468
8 p.
|
artikel
|
| 41 |
Prediction of icing effects on the lateral/directional stability and control of light airplanes
|
Lampton, Amanda
|
|
2012
|
23 |
1 |
p. 305-311
7 p.
|
artikel
|
| 42 |
Real-time trajectory optimization of an underactuated rigid spacecraft using differential flatness
|
Zhuang, Yufei
|
|
2012
|
23 |
1 |
p. 132-139
8 p.
|
artikel
|
| 43 |
Reconfigurable automated behavior for UAS applications
|
Santamaria, Eduard
|
|
2012
|
23 |
1 |
p. 372-386
15 p.
|
artikel
|
| 44 |
Roll-pitch-yaw integrated μ-synthesis for high angle-of-attack missiles
|
Choi, Byunghun
|
|
2012
|
23 |
1 |
p. 270-279
10 p.
|
artikel
|
| 45 |
Simultaneous optimization of staging and trajectory of launch vehicles using two different approaches
|
Jamilnia, Reza
|
|
2012
|
23 |
1 |
p. 85-92
8 p.
|
artikel
|
| 46 |
Sonic boom propagation revisited: A nonlinear geometrical acoustic model
|
Berci, M.
|
|
2012
|
23 |
1 |
p. 280-295
16 p.
|
artikel
|
| 47 |
The design of optimal guidance law with multi-constraints using block pulse functions
|
Dou, Lei
|
|
2012
|
23 |
1 |
p. 201-205
5 p.
|
artikel
|
| 48 |
Theoretical and experimental study of a piezoelectric flapping wing rotor for micro aerial vehicle
|
Guo, Shijun
|
|
2012
|
23 |
1 |
p. 429-438
10 p.
|
artikel
|
| 49 |
35th ERF: Progress in Rotorcraft Research
|
Pahlke, Klausdieter
|
|
2012
|
23 |
1 |
p. 1-
1 p.
|
artikel
|
| 50 |
Thermodynamic performance analysis of turbofan engine with a pulse detonation duct heater
|
Chen, Wenjuan
|
|
2012
|
23 |
1 |
p. 206-212
7 p.
|
artikel
|
| 51 |
Thermodynamic state investigation of the hypersonic air plasma flow produced by the arc-jet facility SCIROCCO
|
Cipullo, A.
|
|
2012
|
23 |
1 |
p. 358-362
5 p.
|
artikel
|
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