| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active twist rotor blade modelling using particle-wake aerodynamics and geometrically exact beam structural dynamics
|
Cesnik, C.E.S.
|
|
2004
|
19 |
5 |
p. 651-668
18 p.
|
artikel
|
| 2 |
Aeroelastic analysis of hypersonic vehicles
|
Friedmann, P.P.
|
|
2004
|
19 |
5 |
p. 681-712
32 p.
|
artikel
|
| 3 |
Aeroelastic scaling for rotary-wing aircraft with applications
|
Friedmann, P.P
|
|
2004
|
19 |
5 |
p. 635-650
16 p.
|
artikel
|
| 4 |
Comparison of experiments and reduced-order models for turbomachinery high-incidence flutter
|
Copeland, G.S.
|
|
2004
|
19 |
5 |
p. 713-727
15 p.
|
artikel
|
| 5 |
Equivalent linear modal parameter estimation for a nonlinear aeroelastic system
|
Marsden, C.C
|
|
2004
|
19 |
5 |
p. 607-619
13 p.
|
artikel
|
| 6 |
Nonlinear mode interactions and period-tripling flutter in transonic flow
|
Bendiksen, O.O
|
|
2004
|
19 |
5 |
p. 591-606
16 p.
|
artikel
|
| 7 |
Preface
|
Cesnik, C.E.S
|
|
2004
|
19 |
5 |
p. 573-
1 p.
|
artikel
|
| 8 |
Reduced-order modelling of limit-cycle oscillation for aeroelastic systems
|
Beran, P.S
|
|
2004
|
19 |
5 |
p. 575-590
16 p.
|
artikel
|
| 9 |
Transient response study on rolling effectiveness of multiple control surfaces
|
Tang, D
|
|
2004
|
19 |
5 |
p. 621-634
14 p.
|
artikel
|
| 10 |
Vortex-induced vibration of a heavy-lift launch vehicle during transonic flight
|
Dotson, K.W
|
|
2004
|
19 |
5 |
p. 669-680
12 p.
|
artikel
|
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