| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Aeroelastic stability of composite hingeless rotor blades in hover—Part II: Results
|
Fulton, M.V.
|
|
1993
|
18 |
3-4 |
p. 19-35
17 p.
|
artikel
|
| 2 |
Aeroelastic stability of composite hingeless rotor blades in hover—Part I: Theory
|
Fulton, M.V.
|
|
1993
|
18 |
3-4 |
p. 1-17
17 p.
|
artikel
|
| 3 |
An integrated finite-state model for rotor deformation, nonlinear airloads, inflow and trim
|
Stumpf, W.M.
|
|
1993
|
18 |
3-4 |
p. 115-129
15 p.
|
artikel
|
| 4 |
Coupled rotor-fuselage vibration reduction using open-loop blade pitch control
|
Papavassiliou, I.
|
|
1993
|
18 |
3-4 |
p. 131-156
26 p.
|
artikel
|
| 5 |
Fully integrated aerodynamic/dynamic optimization of helicopter rotor blades
|
Walsh, J.L.
|
|
1993
|
18 |
3-4 |
p. 53-72
20 p.
|
artikel
|
| 6 |
Nonlinear aeroelasticity in rotorcraft
|
Tang, D.M.
|
|
1993
|
18 |
3-4 |
p. 157-184
28 p.
|
artikel
|
| 7 |
Optimum rotor interdisciplinary design with a finite state aeroelastic system
|
He, C.-J.
|
|
1993
|
18 |
3-4 |
p. 37-51
15 p.
|
artikel
|
| 8 |
Preface
|
Peters, David A.
|
|
1993
|
18 |
3-4 |
p. xi-
1 p.
|
artikel
|
| 9 |
Rotor wake interaction with separated flow
|
Komerath, N.M
|
|
1993
|
18 |
3-4 |
p. 73-87
15 p.
|
artikel
|
| 10 |
Structural optimization of high speed prop rotors including aeroelastic stability constraints
|
Chattopadhyay, A.
|
|
1993
|
18 |
3-4 |
p. 101-113
13 p.
|
artikel
|
| 11 |
Synthesis of a helicopter nonlinear flight controller using approximate model inversion
|
Prasad, J.V.R.
|
|
1993
|
18 |
3-4 |
p. 89-100
12 p.
|
artikel
|
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