| no |
title |
author |
magazine |
year |
volume |
issue |
page(s) |
type |
| 1 |
Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraft
|
Cavcar, Aydan
|
|
2004
|
8 |
6 |
p. 557-567
11 p.
|
article
|
| 2 |
Drag/thrust analysis of jet-propelled transonic transport aircraft; Definition of physical drag components
|
Destarac, D.
|
|
2004
|
8 |
6 |
p. 545-556
12 p.
|
article
|
| 3 |
Editorial Board
|
|
|
2004
|
8 |
6 |
p. IFC-
1 p.
|
article
|
| 4 |
Enhanced eigenstructure assignment for aeroelastic control application
|
Merkel, Maximilian
|
|
2004
|
8 |
6 |
p. 533-543
11 p.
|
article
|
| 5 |
Facilitated Airplane – project and preliminary in-flight experiments
|
Tomczyk, Andrzej
|
|
2004
|
8 |
6 |
p. 469-477
9 p.
|
article
|
| 6 |
Flow structure in the region of three shock wave interaction
|
Szwaba, Ryszard
|
|
2004
|
8 |
6 |
p. 499-508
10 p.
|
article
|
| 7 |
Frequency and time domain flutter computations of a wing with oscillating control surface including shock interference effects
|
Kwon, Hyuk-Jun
|
|
2004
|
8 |
6 |
p. 519-532
14 p.
|
article
|
| 8 |
Identification of dynamic derivatives with a controlled wind tunnel model of the spaceplane-configuration PHOENIX
|
Kirschstein, S.
|
|
2004
|
8 |
6 |
p. 509-518
10 p.
|
article
|
| 9 |
Investigation of integral surface formulations for acoustic post-processing of unsteady aerodynamic jet simulations
|
Rahier, Gilles
|
|
2004
|
8 |
6 |
p. 453-467
15 p.
|
article
|
| 10 |
On the physics and kinematics of vortex motion in the downstream of a high aspect ratio wing with high-lift devices
|
Das, A.
|
|
2004
|
8 |
6 |
p. 489-498
10 p.
|
article
|
| 11 |
Study on the relative motion of parafoil-load-systems
|
Strickert, Gordon
|
|
2004
|
8 |
6 |
p. 479-488
10 p.
|
article
|
Journal description