-
1
-
-
85007685430
-
A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows
-
E. Albano and W.P. Rodden. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows. Journal of Aircraft, 7(2):279-285, 1969.
-
(1969)
Journal of Aircraft
, vol.7
, Issue.2
, pp. 279-285
-
-
Albano, E.1
Rodden, W.P.2
-
5
-
-
0017635267
-
Floating reference frames for flexible spacecraft
-
December
-
J. R. Canavin and P. W. Likins. Floating reference frames for flexible spacecraft. Journal of Spacecraft and Rockets, 14(12):724-732, December 1977.
-
(1977)
Journal of Spacecraft and Rockets
, vol.14
, Issue.12
, pp. 724-732
-
-
Canavin, J.R.1
Likins, P.W.2
-
6
-
-
0017676054
-
Hamilton's principle: Finite-element methods and flexible body dynamics
-
September
-
R. K. Cavin and A. R. Dusto. Hamilton's principle: Finite-element methods and flexible body dynamics. AIAA Journal, 15(12):1684-1690, September 1977.
-
(1977)
AIAA Journal
, vol.15
, Issue.12
, pp. 1684-1690
-
-
Cavin, R.K.1
Dusto, A.R.2
-
8
-
-
29344442100
-
Berechnung dynamischer lasten bei elastischen strukturen
-
Universität Stuttgart
-
C.Reschke. Berechnung dynamischer lasten bei elastischen strukturen. Technical Report Diplomarbeit, Universität Stuttgart, 2003.
-
(2003)
Technical Report Diplomarbeit
-
-
Reschke, C.1
-
9
-
-
2342644111
-
Mode acceleration based random gust stresses in aeroservoelastic optimization
-
F. Engelsen and E. Livne. Mode acceleration based random gust stresses in aeroservoelastic optimization. Journal of Aircraft, 41(2):335-347, 2004.
-
(2004)
Journal of Aircraft
, vol.41
, Issue.2
, pp. 335-347
-
-
Engelsen, F.1
Livne, E.2
-
15
-
-
0008429855
-
Development of an integrated aeroservoelastic analysis program and correlation with test data
-
M.J.Brenner K.K.Gupta and L.S.Voelker. Development of an integrated aeroservoelastic analysis program and correlation with test data. Technical report, 1991.
-
(1991)
Technical Report
-
-
Brenner, M.J.1
Gupta, K.K.2
Voelker, L.S.3
-
18
-
-
0026222917
-
Hybrid state equations of motion for flexible bodies in terms of quasi-coordinates
-
L. Meirovitch. Hybrid state equations of motion for flexible bodies in terms of quasi-coordinates. Journal of Guidance, 14(5):1008-1013, 1988.
-
(1988)
Journal of Guidance
, vol.14
, Issue.5
, pp. 1008-1013
-
-
Meirovitch, L.1
-
19
-
-
4944223842
-
Time simulation of the response of maneuvering flexible aircraft
-
September-October
-
L. Meirovitch and I. Tuzcu. Time simulation of the response of maneuvering flexible aircraft. Jounal of Guidance, Control and Dynamics, 27(5):814-828, September-October 2004.
-
(2004)
Jounal of Guidance, Control and Dynamics
, vol.27
, Issue.5
, pp. 814-828
-
-
Meirovitch, L.1
Tuzcu, I.2
-
20
-
-
0032715079
-
Reduced-order models for integrated aeroservoelastic optimization
-
M.Karpel. Reduced-order models for integrated aeroservoelastic optimization. Journal of Aircraft, 36(1):146-155, 1999.
-
(1999)
Journal of Aircraft
, vol.36
, Issue.1
, pp. 146-155
-
-
Karpel, M.1
-
21
-
-
0022695242
-
New and existing techniques for dynamic loads analysis of flexible airplanes
-
A. S. Pototzky. New and existing techniques for dynamic loads analysis of flexible airplanes. Journal of Aircraft, 23(4):340-347, 1985.
-
(1985)
Journal of Aircraft
, vol.23
, Issue.4
, pp. 340-347
-
-
Pototzky, A.S.1
-
22
-
-
0017685541
-
Airplane math modeling methods for active control design
-
number AGARD/CP-226. AGARD, April
-
K. L. Roger. Airplane math modeling methods for active control design. In AGARD Structures and Materials Panel, number AGARD/CP-226, pages 4-1-4-11. AGARD, April 1977.
-
(1977)
AGARD Structures and Materials Panel
, pp. 41-411
-
-
Roger, K.L.1
-
24
-
-
0024019482
-
Flight dynamics of aeroelastic vehicles
-
M. R. Waszak and D. K. Schmidt. Flight dynamics of aeroelastic vehicles. Journal of Aircraft, 25(6):563-571, 1988.
-
(1988)
Journal of Aircraft
, vol.25
, Issue.6
, pp. 563-571
-
-
Waszak, M.R.1
Schmidt, D.K.2
|