-
1
-
-
2942529210
-
-
DLR-Mitt. 93-09, DLR, Braunschweig, Germany
-
Splettstoesser, W. R. et. al., "The HELINOISE Aeroacoustic Rotor Test in the DNW - Test Documentation and Representative Results", DLR-Mitt. 93-09, DLR, Braunschweig, Germany, 1993.
-
(1993)
The HELINOISE Aeroacoustic Rotor Test in the DNW - Test Documentation and Representative Results
-
-
Splettstoesser, W.R.1
-
2
-
-
33746648927
-
-
1999, Structural Component having Means for Actively Varying its Stiffness to Control Vibrations, U.S. Patent No. 5,973,440. European Patent: EP-996570-B1
-
Nitzsche, F., Grewal, A. and Zimcik, D. G., 1999, Structural Component having Means for Actively Varying its Stiffness to Control Vibrations, U.S. Patent No. 5,973,440. European Patent: EP-996570-B1, 2001.
-
(2001)
-
-
Nitzsche, F.1
Grewal, A.2
Zimcik, D.G.3
-
3
-
-
1242306809
-
Control laws for an active tunable vibration absorber designed for aeroelastic damping augmentation
-
Nitzsche, F., Zimcik, D., Wickramasinghe, V. and Yong, C., "Control Laws for an Active Tunable Vibration Absorber Designed for Aeroelastic Damping Augmentation," The Aeronautical Journal, Vol. 108, No. 1079, 2004, pp. 35-42.
-
(2004)
The Aeronautical Journal
, vol.108
, Issue.1079
, pp. 35-42
-
-
Nitzsche, F.1
Zimcik, D.2
Wickramasinghe, V.3
Yong, C.4
-
4
-
-
0842333777
-
Alleviation of airfoil dynamic stall moments via trailing edge flap flow control
-
January
-
Feszty, D., Gillies, E. A., Vezza, M., "Alleviation of Airfoil Dynamic Stall Moments via Trailing Edge Flap Flow Control", AIAA Journal, Vol. 42, no.1, pp 17-25, January 2004.
-
(2004)
AIAA Journal
, vol.42
, Issue.1
, pp. 17-25
-
-
Feszty, D.1
Gillies, E.A.2
Vezza, M.3
-
5
-
-
0037897034
-
Calculation of rotor blade-vortex interaction noise using parallel super computer
-
Paper 81, The Royal Aeronautical Society
-
nd European Rotorcraft Forum, The Royal Aeronautical Society, Vol. 2, 1996.
-
(1996)
nd European Rotorcraft Forum
, vol.2
-
-
Aoyama, T.1
-
6
-
-
0004090333
-
Nonlinear equation for the elastic bending and torsion of twisted non-uniform rotor blades
-
Hodges, D. H., and DowelI, E. H., "Nonlinear Equation for the Elastic Bending and Torsion of Twisted Non-uniform Rotor Blades," NASA TN D-7818, 1974.
-
(1974)
NASA TN
, vol.D-7818
-
-
Hodges, D.H.1
Doweli, E.H.2
-
7
-
-
2942616925
-
Stability of elastic bending and torsion of uniform cantilever rotor blades in Hover with variable structural coupling
-
Hodges, D. H. and Ormiston R. A., "Stability of Elastic Bending and Torsion of Uniform Cantilever Rotor Blades in Hover with Variable Structural Coupling," NASA TN D-8192, 1976.
-
(1976)
NASA TN
, vol.D-8192
-
-
Hodges, D.H.1
Ormiston, R.A.2
-
8
-
-
0003222470
-
General theory of aerodynamic instability and the mechanism of flutter
-
Theodorsen, T., "General Theory of Aerodynamic Instability and the Mechanism of Flutter", NACA Report 496, 1935.
-
(1935)
NACA Report
, vol.496
-
-
Theodorsen, T.1
-
9
-
-
13444266683
-
Airfoil in sinusoidal motion in a pulsating stream
-
Greenberg, J. M., "Airfoil in Sinusoidal Motion in a Pulsating Stream," NACA TN-1326, 1947.
-
(1947)
NACA TN-1326
-
-
Greenberg, J.M.1
-
10
-
-
0039644938
-
A theory of airflow through rotors and its application to some helicopter problems
-
Drees, J. M., "A Theory of Airflow Through Rotors and Its Application to Some Helicopter Problems," Journal of the Helicopter Association of Great Britain, Vol. 3, No. 2, pp. 79-104, 1949.
-
(1949)
Journal of the Helicopter Association of Great Britain
, vol.3
, Issue.2
, pp. 79-104
-
-
Drees, J.M.1
-
11
-
-
33746596863
-
Aeroelastic modeling and vibratory load analysis of helicopters
-
Madeira, Portugal, July
-
Gennaretti, M., and Carvai, A., "Aeroelastic Modeling and Vibratory Load Analysis of Helicopters," International Conference on Computational and Experimental Engineering and Science, Madeira, Portugal, July 2004.
-
(2004)
International Conference on Computational and Experimental Engineering and Science
-
-
Gennaretti, M.1
Carvai, A.2
-
14
-
-
85067322124
-
Helicopter vibration reduction using discrete controllable-stiffness devices at the rotor hub
-
AIAA Paper 2001-1438, Seattle, Washington
-
Gandhi, F., and Anusonti-Intra, P., "Helicopter Vibration Reduction using Discrete Controllable-Stiffness Devices at the Rotor Hub," AIAA Paper 2001-1438, Proceedings of the 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference, Seattle, Washington, 2001.
-
(2001)
Proceedings of the 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference
-
-
Gandhi, F.1
Anusonti-Intra, P.2
-
15
-
-
33746630068
-
Acoustic validation of a new code using particle wake aerodynamics and geometrically exact beam structural dynamics
-
Paper No. 11, 16-18 September, Friedrichshafen, Germany
-
Opoku, D. and Nitzsche, F., "Acoustic Validation of a New Code Using Particle Wake Aerodynamics and Geometrically Exact Beam Structural Dynamics," Paper No. 11, Proceedings: 29th European Rotorcraft Forum, 16-18 September 2003, Friedrichshafen, Germany.
-
(2003)
Proceedings: 29th European Rotorcraft Forum
-
-
Opoku, D.1
Nitzsche, F.2
-
16
-
-
27844552834
-
Development of a maximum energy extraction control for the smart spring
-
accepted for publication
-
Nitzsche, F., Harold, T., Wickramasinghe, V. K., Young, C. and Zimcik, D. G., "Development of a Maximum Energy Extraction Control for the Smart Spring," Journal of Intelligent Material Systems and Structures (accepted for publication, 2005).
-
(2005)
Journal of Intelligent Material Systems and Structures
-
-
Nitzsche, F.1
Harold, T.2
Wickramasinghe, V.K.3
Young, C.4
Zimcik, D.G.5
-
18
-
-
33746635396
-
-
Aerodynamics Laboratory, Department of Mechanical Engineering, National Technical University of Athens, Greece
-
"NTUA Internal Report on the GAST code", Aerodynamics Laboratory, Department of Mechanical Engineering, National Technical University of Athens, Greece, 2005.
-
(2005)
NTUA Internal Report on the GAST Code
-
-
-
19
-
-
0343228755
-
Elements of computational fluid dynamics on block structured grids using implicit solvers
-
Badcock, K.J., Richards, B.E. and Woodgate, M.A. "Elements of Computational Fluid Dynamics on Block Structured Grids Using Implicit Solvers", Progress in Aerospace Sciences, vol 36, pp 351-392, 2000.
-
(2000)
Progress in Aerospace Sciences
, vol.36
, pp. 351-392
-
-
Badcock, K.J.1
Richards, B.E.2
Woodgate, M.A.3
-
21
-
-
33746606277
-
-
Personal Communication, Carleton University
-
Wierach P., Personal Communication, Carleton University, 2004.
-
(2004)
-
-
Wierach, P.1
-
22
-
-
28844468529
-
Output-only approach for finite element model updating of AB-204 helicopter blade
-
18-22/Apr., Austin, TX, USA, paper No. AIAA-2005-2249
-
th AIAA/SDM Conference, 18-22/Apr./2005, Austin, TX, USA, paper No. AIAA-2005-2249.
-
(2005)
th AIAA/SDM Conference
-
-
Balis Crema, L.1
Coppotelli, G.2
-
23
-
-
28844492471
-
Modal identification from ambient responses using frequency domain decomposition
-
07-10/Feb., San Antonio (TX) - USA
-
Brincker, Zhang, R. L., and Andersen, P. "Modal Identification from Ambient Responses Using Frequency Domain Decomposition", XVIII IMAC, 07-10/Feb., San Antonio (TX) - USA, 2000.
-
(2000)
XVIII IMAC
-
-
Brincker1
Zhang, R.L.2
Andersen, P.3
-
24
-
-
19944401017
-
Why output-only modal testing is a desirable tool for a wide range of practical applications
-
3-6/Feb., Orlando (FL) - USA
-
Brincker, R., Ventura, C. E. and Andersen, P., "Why Output-Only Modal Testing is a Desirable Tool for a Wide Range of Practical Applications," XXI IMAC, 3-6/Feb., Orlando (FL) - USA, (2003), pp. 265-272.
-
(2003)
XXI IMAC
, pp. 265-272
-
-
Brincker, R.1
Ventura, C.E.2
Andersen, P.3
-
25
-
-
13344277312
-
On modal parameters estimates from ambient vibration tests
-
Leuven, Belgium
-
Agneni, A., Brincker, R., Coppotelli, G., "On Modal Parameters Estimates from Ambient Vibration Tests," in Proceedings of International Seminar on Modal Analysis, Leuven, Belgium, 2004.
-
(2004)
Proceedings of International Seminar on Modal Analysis
-
-
Agneni, A.1
Brincker, R.2
Coppotelli, G.3
-
26
-
-
84896858409
-
Design and testing of a double X-frame piezoelectric actuator
-
Hall, S. R., Tzianetopoulou, T., "Design and testing of a double X-frame piezoelectric actuator," Smart Structures and Materials 2000: Smart Structures and Integrated Systems, Vol. 3985, 2000.
-
(2000)
Smart Structures and Materials 2000: Smart Structures and Integrated Systems
, vol.3985
-
-
Hall, S.R.1
Tzianetopoulou, T.2
-
27
-
-
0035311611
-
Analysis of an actively twisted rotor by multibody global modelling
-
April
-
Ghiringhelli, G. L., Masarati, P., and Mantegazza, P., "Analysis of an Actively Twisted Rotor by Multibody Global Modelling," Composite Structures, April 2001, Vol. 52/1, pp. 113-122.
-
(2001)
Composite Structures
, vol.52
, Issue.1
, pp. 113-122
-
-
Ghiringhelli, G.L.1
Masarati, P.2
Mantegazza, P.3
-
28
-
-
0033640196
-
A multibody implementation of finite volume beams
-
January
-
Ghiringhelli, G. L., Masarati, P., and Mantegazza, P., "A Multibody Implementation of Finite Volume Beams," AIAA Journal, Vol. 38(1), January 2000, pp. 131-138.
-
(2000)
AIAA Journal
, vol.38
, Issue.1
, pp. 131-138
-
-
Ghiringhelli, G.L.1
Masarati, P.2
Mantegazza, P.3
-
29
-
-
0028460355
-
A survey of models, analysis tools and compensation methods for the control of machines with friction
-
Armstrong-H'elouvry, B., Dupont, P., and Canudas de Wit, C., "A survey of models, analysis tools and compensation methods for the control of machines with friction," Automatica, 30(7): 1083-1138, 1994.
-
(1994)
Automatica
, vol.30
, Issue.7
, pp. 1083-1138
-
-
Armstrong-H'Elouvry, B.1
Dupont, P.2
Canudas De Wit, C.3
-
30
-
-
0036576599
-
Single state elastoplastic friction models
-
May
-
Dupont, P., Hayward, V., Armstrong, B., and Altpeter, F., "Single state elastoplastic friction models," IEEE Transactions on Automatic Control, 47(5):787-792, May 2002
-
(2002)
IEEE Transactions on Automatic Control
, vol.47
, Issue.5
, pp. 787-792
-
-
Dupont, P.1
Hayward, V.2
Armstrong, B.3
Altpeter, F.4
|