A nonlinear model of a turbine blade by asymptotic analysis
International Journal of Applied Mathematics and Computer Science, Tome 12 (2002) no. 1, pp. 101-113
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In this paper we obtain a limit model for a turbine blade fixed to a 3D solid. This model is a three-dimensional linear elasticity problem in the 3D part of the piece (the rotor) and a two-dimensional problem (the nonlinear shallow shell equations) in the 2D part (the turbine blade), with junction conditions in the part of the turbine blade fixed to the rotor. To obtain this model, we perform an asymptotic analysis, starting with the nonlinear three-dimensional elasticity equations on all the pieces and taking as a small parameter the thickness of the blade.
Keywords:
asymptotic analysis, nonlinear elasticity, junctions, shallow shells, multistructures
Mots-clés : matematyka
Mots-clés : matematyka
@article{IJAMCS_2002_12_1_a9,
author = {Rodriguez, J. M.},
title = {A nonlinear model of a turbine blade by asymptotic analysis},
journal = {International Journal of Applied Mathematics and Computer Science},
pages = {101--113},
publisher = {mathdoc},
volume = {12},
number = {1},
year = {2002},
language = {en},
url = {http://geodesic.mathdoc.fr/item/IJAMCS_2002_12_1_a9/}
}
TY - JOUR AU - Rodriguez, J. M. TI - A nonlinear model of a turbine blade by asymptotic analysis JO - International Journal of Applied Mathematics and Computer Science PY - 2002 SP - 101 EP - 113 VL - 12 IS - 1 PB - mathdoc UR - http://geodesic.mathdoc.fr/item/IJAMCS_2002_12_1_a9/ LA - en ID - IJAMCS_2002_12_1_a9 ER -
Rodriguez, J. M. A nonlinear model of a turbine blade by asymptotic analysis. International Journal of Applied Mathematics and Computer Science, Tome 12 (2002) no. 1, pp. 101-113. http://geodesic.mathdoc.fr/item/IJAMCS_2002_12_1_a9/