| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Aerodynamic study of theater ballistic missile target
|
Zhang, Wen-dian
|
|
2013
|
24 |
1 |
p. 221-225
5 p.
|
artikel
|
| 2 |
A multiobjective optimization approach to determine the parameters of stepped frequency pulse train
|
Sahoo, Ajit Kumar
|
|
2013
|
24 |
1 |
p. 101-110
10 p.
|
artikel
|
| 3 |
Analysis of the effect of stiffener profile on buckling strength in composite isogrid stiffened shell under axial loading
|
Rahimi, G.H.
|
|
2013
|
24 |
1 |
p. 198-203
6 p.
|
artikel
|
| 4 |
A refined trigonometric shear deformation theory for thermoelastic bending of functionally graded sandwich plates
|
Tounsi, Abdelouahed
|
|
2013
|
24 |
1 |
p. 209-220
12 p.
|
artikel
|
| 5 |
Attitude and orbit control systems for the LISA Pathfinder mission
|
Giulicchi, Luisella
|
|
2013
|
24 |
1 |
p. 283-294
12 p.
|
artikel
|
| 6 |
Detached-Eddy Simulation of the vortical flow field about the VFE-2 delta wing
|
Cummings, Russell M.
|
|
2013
|
24 |
1 |
p. 66-76
11 p.
|
artikel
|
| 7 |
Direct calculation of the average local Mach number in converging–diverging nozzles
|
Majdalani, Joseph
|
|
2013
|
24 |
1 |
p. 111-115
5 p.
|
artikel
|
| 8 |
Editorial Board
|
|
|
2013
|
24 |
1 |
p. IFC-
1 p.
|
artikel
|
| 9 |
Enabling leg-based guidance on top of waypoint-based autopilots for UAS
|
Prats, Xavier
|
|
2013
|
24 |
1 |
p. 95-100
6 p.
|
artikel
|
| 10 |
Evaluation on novel architecture for harmonizing manual and automatic flight controls under atmospheric turbulence
|
Itoh, Eri
|
|
2013
|
24 |
1 |
p. 241-254
14 p.
|
artikel
|
| 11 |
Guidance law implementation with performance recovery using an extended high-gain observer
|
Ma, Kemao
|
|
2013
|
24 |
1 |
p. 177-186
10 p.
|
artikel
|
| 12 |
Hybrid life support systems with integrated fuel cells and photobioreactors for a lunar base
|
Belz, S.
|
|
2013
|
24 |
1 |
p. 169-176
8 p.
|
artikel
|
| 13 |
Initial experiments and analysis of blunt-edge vortex flows for VFE-2 configurations at NASA Langley, USA
|
Luckring, James M.
|
|
2013
|
24 |
1 |
p. 10-21
12 p.
|
artikel
|
| 14 |
Limit cycle oscillation control of wing with static output feedback control method
|
Dardel, Morteza
|
|
2013
|
24 |
1 |
p. 147-160
14 p.
|
artikel
|
| 15 |
Mistuned bladed disk forced vibration analysis based on standing wave formulation
|
Lee, Il
|
|
2013
|
24 |
1 |
p. 275-282
8 p.
|
artikel
|
| 16 |
Numerical analysis of regenerative cooling in liquid propellant rocket engines
|
Ulas, A.
|
|
2013
|
24 |
1 |
p. 187-197
11 p.
|
artikel
|
| 17 |
Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code
|
Schütte, Andreas
|
|
2013
|
24 |
1 |
p. 56-65
10 p.
|
artikel
|
| 18 |
Numerical simulation of the peculiar subsonic flow-field about the VFE-2 delta wing with rounded leading edge
|
Fritz, Willy
|
|
2013
|
24 |
1 |
p. 45-55
11 p.
|
artikel
|
| 19 |
Optimal filtering for systems with finite-step autocorrelated noises and multiple packet dropouts
|
Li, Fan
|
|
2013
|
24 |
1 |
p. 255-263
9 p.
|
artikel
|
| 20 |
Optimal generator matrix G
|
Harun, Harlisya
|
|
2013
|
24 |
1 |
p. 136-140
5 p.
|
artikel
|
| 21 |
Optimal thickness distributions of aeroelastic flapping shells
|
Stanford, Bret
|
|
2013
|
24 |
1 |
p. 116-127
12 p.
|
artikel
|
| 22 |
Optimal trends in Manoeuvre Load Control at subsonic and supersonic flight points for tailless delta wing aircraft
|
Suresh, P.S.
|
|
2013
|
24 |
1 |
p. 128-135
8 p.
|
artikel
|
| 23 |
Prediction of transient responses of a folding wing during the morphing process
|
Zhao, Yonghui
|
|
2013
|
24 |
1 |
p. 89-94
6 p.
|
artikel
|
| 24 |
PSP and PIV investigations on the VFE-2 configuration in sub- and transonic flow
|
Konrath, Robert
|
|
2013
|
24 |
1 |
p. 22-31
10 p.
|
artikel
|
| 25 |
Robust reliable control for autonomous spacecraft rendezvous with limited-thrust
|
Yang, Xuebo
|
|
2013
|
24 |
1 |
p. 161-168
8 p.
|
artikel
|
| 26 |
Scale effect of fuel regression rate in hybrid rocket motor
|
Cai, Guobiao
|
|
2013
|
24 |
1 |
p. 141-146
6 p.
|
artikel
|
| 27 |
Stability, flying qualities and longitudinal parameter estimation of a twin-engine CS-23 certified light aircraft
|
Nicolosi, Fabrizio
|
|
2013
|
24 |
1 |
p. 226-240
15 p.
|
artikel
|
| 28 |
Temporal evolution of the RCS of aircraft wake vortices
|
Wang, Xuesong
|
|
2013
|
24 |
1 |
p. 204-208
5 p.
|
artikel
|
| 29 |
The International Vortex Flow Experiment 2 (VFE-2): Background, objectives and organization
|
Hummel, Dietrich J.
|
|
2013
|
24 |
1 |
p. 1-9
9 p.
|
artikel
|
| 30 |
Thermochemical exploration of hydrogen combustion in generic scramjet combustor
|
Dharavath, Malsur
|
|
2013
|
24 |
1 |
p. 264-274
11 p.
|
artikel
|
| 31 |
Turbulent and unsteady flow characteristics of delta wing vortex systems
|
Furman, Andrej
|
|
2013
|
24 |
1 |
p. 32-44
13 p.
|
artikel
|
| 32 |
What was learned from the new VFE-2 experiments
|
Luckring, James M.
|
|
2013
|
24 |
1 |
p. 77-88
12 p.
|
artikel
|
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