| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Accurate reduced-order models for a simple rotor blade model using nonlinear normal modes
|
Pesheck, E.
|
|
2001
|
33 |
10-11 |
p. 1085-1097
13 p.
|
artikel
|
| 2 |
Application of the mixed finite-element method to rotor blade modal reduction
|
Ruzicka, G.C.
|
|
2001
|
33 |
10-11 |
p. 1177-1202
26 p.
|
artikel
|
| 3 |
Assessment of beam modeling methods for rotor blade applications
|
Volovoi, V.V.
|
|
2001
|
33 |
10-11 |
p. 1099-1112
14 p.
|
artikel
|
| 4 |
Coupled rotor/fuselage vibration analysis using detailed 3-D airframe models
|
Yeo, Hyeonsoo
|
|
2001
|
33 |
10-11 |
p. 1035-1054
20 p.
|
artikel
|
| 5 |
Influence of blade-to-blade dissimilarity on alleviation of helicopter blade-vortex interactions
|
Tauszig, L.
|
|
2001
|
33 |
10-11 |
p. 1139-1154
16 p.
|
artikel
|
| 6 |
Magnetostrictively actuated control flaps for vibration reduction in helicopter rotors—design considerations for implementation
|
Friedmann, P.P.
|
|
2001
|
33 |
10-11 |
p. 1203-1217
15 p.
|
artikel
|
| 7 |
Modeling rotorcraft dynamics with finite element multibody procedures
|
Bauchau, O.A.
|
|
2001
|
33 |
10-11 |
p. 1113-1137
25 p.
|
artikel
|
| 8 |
New developments in vibration reduction with actively controlled trailing edge flaps
|
Friedmann, P.P.
|
|
2001
|
33 |
10-11 |
p. 1055-1083
29 p.
|
artikel
|
| 9 |
Parallel fast-floquet analysis of trim and stability for large helicopter models
|
Subramanian, S.
|
|
2001
|
33 |
10-11 |
p. 1155-1176
22 p.
|
artikel
|
| 10 |
Preface
|
Peters, David A.
|
|
2001
|
33 |
10-11 |
p. xiii-
1 p.
|
artikel
|
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