Exact modal analysis of an idealized whole aircraft using symbolic computation

Aeronautical Journal

Volumn 104, Issue 1035, 2000, Pages 247-255

  Banerjee, J R ^a  

^a CITY UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DIFFERENTIAL EQUATIONS; MATHEMATICAL MODELS; MODAL ANALYSIS; OPTIMIZATION;

SOFTWARE PACKAGE REDUCE; SYMBOLIC COMPUTATION;

AIRCRAFT;

EID: 0034186750     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (12)

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9. BANERJEE, J. R. Coupled bending-torsional dynamic stiffness matrix for beam elements, Int J Numer Meth Eng, 1989, 28, pp 1283-1298.
10. DOCUMACI, E. An exact solution for coupled bending and torsion vibrations of uniform beams having single cross-sectional symmetry, J Sound Vibr, 1987, 119, pp 443-449.
11. HALLAUER, W. L. and LIU, R. Y. L. Beam bending-torsion dynamic stiffness method for calculation of exact vibration modes, J Sound Vibr, 1982, 85, pp 105-113.
12. BANERJEE J. R. Use and capability of CALFUN: A program for Calculation of Flutter Speed using Normal Modes, Proceedings of the International AMSE Conference on Modelling and Simulation, Athens, Greece, June 1984, pp 121-131.