REVISTA

MATHEMATICAL AND COMPUTER MODELLING

ISSN: 0895-7177 Frecuencia: 12 Formato: Impresa

Tablas de contenido

9 artículos asociados

Volumen 33 Número 10-11 Parte 0 Año 2001

Coupled rotor/fuselage vibration analysis using detailed 3-D airframe models	Solicitud
Yeo, H.
Pág. 1035 - 1054

New developments in vibration reduction with actively controlled trailing edge flaps	Solicitud
Friedmann, P. P. de Terlizzi, M.
Pág. 1055 - 1083

Accurate reduced-order models for a simple rotor blade model using nonlinear normal modes	Solicitud
Pesheck, E. Pierre, C.
Pág. 1085 - 1097

Assessment of beam modeling methods for rotor blade applications	Solicitud
Volovoi, V. V. Hodges, D. H.
Pág. 1099 - 1112

Modeling rotorcraft dynamics with finite element multibody procedures	Solicitud
Bauchau, O. A.
Pág. 1113 - 1137

Influence of blade-to-blade dissimilarity on alleviation of helicopter blade-vortex interactions	Solicitud
Tauszig, L. Gandhi, F.
Pág. 1139 - 1154

Parallel fast-floquet analysis of trim and stability for large helicopter models	Solicitud
Subramanian, S. Venkataratnam, S. Gaonkar, G. H.
Pág. 1155 - 1176

Application of the mixed finite-element method to rotor blade modal reduction	Solicitud
Ruzicka, G. C.
Pág. 1177 - 1202

Magnetostrictively actuated control flaps for vibration reduction in helicopter rotors-design considerations for implementation	Solicitud
Friedmann, P. P.
Pág. 1203 - 1217