| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A guidance law with finite time convergence accounting for autopilot lag
|
Sun, Sheng
|
|
2013
|
25 |
1 |
p. 132-137
6 p.
|
artikel
|
| 2 |
Analytical modeling of clamp band joint under external bending moment
|
Qin, Z.Y.
|
|
2013
|
25 |
1 |
p. 45-55
11 p.
|
artikel
|
| 3 |
Analytical solution to optimal relocation of satellite formation flying in arbitrary elliptic orbits
|
Cho, Hancheol
|
|
2013
|
25 |
1 |
p. 161-176
16 p.
|
artikel
|
| 4 |
An approach for space launch vehicle conceptual design and multi-attribute evaluation
|
Ullah, Rizwan
|
|
2013
|
25 |
1 |
p. 65-74
10 p.
|
artikel
|
| 5 |
An optimization of energy addition to suppress the coalescence of the shock waves
|
Volkan Pehlivanoglu, Y.
|
|
2013
|
25 |
1 |
p. 75-83
9 p.
|
artikel
|
| 6 |
Attitude control of magnetically actuated satellites with an uneven inertia distribution
|
Wood, Mark
|
|
2013
|
25 |
1 |
p. 29-39
11 p.
|
artikel
|
| 7 |
Chaotic motions of a two-dimensional airfoil with cubic nonlinearity in supersonic flow
|
Zhou, Liangqiang
|
|
2013
|
25 |
1 |
p. 138-144
7 p.
|
artikel
|
| 8 |
Characterization of the startup and pressure blowdown processes in rocket nozzles
|
Maicke, Brian A.
|
|
2013
|
25 |
1 |
p. 273-282
10 p.
|
artikel
|
| 9 |
Distribution of subjective assessments in a controlled aircraft environment
|
Baumann, Ingo
|
|
2013
|
25 |
1 |
p. 93-101
9 p.
|
artikel
|
| 10 |
Dynamic modeling of the airship with Matlab using geometrical aerodynamic parameters
|
Ashraf, M.Z.
|
|
2013
|
25 |
1 |
p. 56-64
9 p.
|
artikel
|
| 11 |
Editorial Board
|
|
|
2013
|
25 |
1 |
p. IFC-
1 p.
|
artikel
|
| 12 |
Effect of aerodynamic valve on backflow in pulsed detonation tube
|
Qiu, Hua
|
|
2013
|
25 |
1 |
p. 1-15
15 p.
|
artikel
|
| 13 |
Efficient computation of the POD manifold containing the information required to generate a multi-parameter aerodynamic database
|
Lorente, L.S.
|
|
2013
|
25 |
1 |
p. 152-160
9 p.
|
artikel
|
| 14 |
Flexibility of hybrid load transfer assemblies: Influence of tightening pre-stress
|
Alkatan, Feras
|
|
2013
|
25 |
1 |
p. 84-92
9 p.
|
artikel
|
| 15 |
Hypersonic environment assessment of the CIRA FTB-X re-entry vehicle
|
Pezzella, Giuseppe
|
|
2013
|
25 |
1 |
p. 190-202
13 p.
|
artikel
|
| 16 |
Hypersonic high altitude aerothermodynamics of a space re-entry vehicle
|
Votta, Raffaele
|
|
2013
|
25 |
1 |
p. 253-265
13 p.
|
artikel
|
| 17 |
Improved methodologies for the design of maneuver for stability and control simulations
|
Jirásek, Adam
|
|
2013
|
25 |
1 |
p. 203-223
21 p.
|
artikel
|
| 18 |
Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function
|
Han, Zhong-Hua
|
|
2013
|
25 |
1 |
p. 177-189
13 p.
|
artikel
|
| 19 |
Large amplitude oscillations of cruciform tailed missiles. Part 1: Catastrophic yaw fundamental analysis
|
Morote, J.
|
|
2013
|
25 |
1 |
p. 145-151
7 p.
|
artikel
|
| 20 |
Missile target accuracy estimation with importance splitting
|
Morio, Jérôme
|
|
2013
|
25 |
1 |
p. 40-44
5 p.
|
artikel
|
| 21 |
Multidisciplinary design optimization of blended-wing-body transport aircraft with distributed propulsion
|
Leifsson, L.
|
|
2013
|
25 |
1 |
p. 16-28
13 p.
|
artikel
|
| 22 |
Numerical investigation of unsteady wave phenomena for transonic airfoil flow
|
Hermes, V.
|
|
2013
|
25 |
1 |
p. 224-233
10 p.
|
artikel
|
| 23 |
Optimal design of hybrid rocket motor powered vehicle for suborbital flight
|
Cai, Guobiao
|
|
2013
|
25 |
1 |
p. 114-124
11 p.
|
artikel
|
| 24 |
Perforation of aero-engine fan casing by a single rotating blade
|
He, Qing
|
|
2013
|
25 |
1 |
p. 234-241
8 p.
|
artikel
|
| 25 |
Relative motion coupled control based on dual quaternion
|
Wang, Jian-Ying
|
|
2013
|
25 |
1 |
p. 102-113
12 p.
|
artikel
|
| 26 |
Robust aeroelastic instability suppression of an advanced wing with model uncertainty in subsonic compressible flow field
|
Song, Ji-Seok
|
|
2013
|
25 |
1 |
p. 242-252
11 p.
|
artikel
|
| 27 |
Robust control of a nonlinear non-minimum phase supersonic flight vehicle based on stable system center
|
Bahrami, Mohsen
|
|
2013
|
25 |
1 |
p. 283-291
9 p.
|
artikel
|
| 28 |
The design, development and test of one newton hydrogen peroxide monopropellant thruster
|
Amri, Redha
|
|
2013
|
25 |
1 |
p. 266-272
7 p.
|
artikel
|
| 29 |
The development of a design methodology for dynamic power distribution management on a civil transport all electric aircraft
|
Xia, Xiuxian
|
|
2013
|
25 |
1 |
p. 125-131
7 p.
|
artikel
|
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