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Results: 1-11 |
Results: 11
Frequency equation and mode shape formulae for composite Timoshenko beams
Authors: Banerjee, JR
Citation: Jr. Banerjee, Frequency equation and mode shape formulae for composite Timoshenko beams, COMP STRUCT, 51(4), 2001, pp. 381-388
Dynamic stiffness formulation and free vibration analysis of centrifugallystiffened Timoshenko beams
Authors: Banerjee, JR
Citation: Jr. Banerjee, Dynamic stiffness formulation and free vibration analysis of centrifugallystiffened Timoshenko beams, J SOUND VIB, 247(1), 2001, pp. 97-115
Free vibration analysis of a twisted beam using the dynamic stiffness method
Authors: Banerjee, JR
Citation: Jr. Banerjee, Free vibration analysis of a twisted beam using the dynamic stiffness method, INT J SOL S, 38(38-39), 2001, pp. 6703-6722
Explicit analytical expressions for frequency equation and mode shapes of composite beams
Authors: Banerjee, JR
Citation: Jr. Banerjee, Explicit analytical expressions for frequency equation and mode shapes of composite beams, INT J SOL S, 38(14), 2001, pp. 2415-2426
Use of generalized mass in the interpretation of dynamic response of bending-torsion coupled beams
Authors: Eslimy-Isfahany, SHR Banerjee, JR
Citation: Shr. Eslimy-isfahany et Jr. Banerjee, Use of generalized mass in the interpretation of dynamic response of bending-torsion coupled beams, J SOUND VIB, 238(2), 2000, pp. 295-308
Free vibration of centrifugally stiffened uniform and tapered beams using the dynamic stiffness method
Authors: Banerjee, JR
Citation: Jr. Banerjee, Free vibration of centrifugally stiffened uniform and tapered beams using the dynamic stiffness method, J SOUND VIB, 233(5), 2000, pp. 857-875
Explicit modal analysis of an axially loaded Timoshenko beam with bending-torsion coupling
Authors: Banerjee, JR
Citation: Jr. Banerjee, Explicit modal analysis of an axially loaded Timoshenko beam with bending-torsion coupling, J APPL MECH, 67(2), 2000, pp. 307-313
Exact modal analysis of an idealised whole aircraft using symbolic computation
Authors: Banerjee, JR
Citation: Jr. Banerjee, Exact modal analysis of an idealised whole aircraft using symbolic computation, AERONAUT J, 104(1035), 2000, pp. 247-255
Ply angle optimization of nonuniform composite beams subject to aeroelastic constraints
Authors: Evrard, T Butler, R Hughes, SW Banerjee, JR
Citation: T. Evrard et al., Ply angle optimization of nonuniform composite beams subject to aeroelastic constraints, AIAA J, 38(10), 2000, pp. 1992-1994
Explicit frequency equation and mode shapes of a cantilever beam coupled in bending and torsion
Authors: Banerjee, JR
Citation: Jr. Banerjee, Explicit frequency equation and mode shapes of a cantilever beam coupled in bending and torsion, J SOUND VIB, 224(2), 1999, pp. 267-281
Sequential use of conceptual MDO and panel sizing methods for aircraft wing design
Authors: Butler, R Lillico, M Banerjee, JR Patel, MH Done, GTS
Citation: R. Butler et al., Sequential use of conceptual MDO and panel sizing methods for aircraft wing design, AERONAUT J, 103(1026), 1999, pp. 389-397
Risultati: 1-11 |