TY - GEN
T1 - Development of an integrated BEM for hot fluid-structure interaction
AU - Dargush, G. F.
AU - Banerjee, P. K.
N1 - Publisher Copyright:
Copyright © 1989 by ASME.
PY - 1989
Y1 - 1989
N2 - A boundary element approach is developed for problems of hot fluid-structure interaction. The structure is idealized as a thermoelastic solid, and a time-domain, boundary-only integral formulation is described. Meanwhile, several approaches are discussed for the hot fluid. Integral equations are developed for both compressible and incompressible thermoviscous flow. Due to the presence of non-linear convective terms in the governing differential equations, domain discretization is generally required. However, with the introduction of reference velocities, volume modeling often can be confined to regions near obstacles and walls. All formulations are implemented for two-dimensional problems in GP-BEST, a general purpose boundary element computer program. An overview of this numerical implementation is provided, along with several illustrative examples. The present fluid formulations are appropriate in the low to medium Reynolds number ranges, however, some enhancements required for higher speed simulations are noted.
AB - A boundary element approach is developed for problems of hot fluid-structure interaction. The structure is idealized as a thermoelastic solid, and a time-domain, boundary-only integral formulation is described. Meanwhile, several approaches are discussed for the hot fluid. Integral equations are developed for both compressible and incompressible thermoviscous flow. Due to the presence of non-linear convective terms in the governing differential equations, domain discretization is generally required. However, with the introduction of reference velocities, volume modeling often can be confined to regions near obstacles and walls. All formulations are implemented for two-dimensional problems in GP-BEST, a general purpose boundary element computer program. An overview of this numerical implementation is provided, along with several illustrative examples. The present fluid formulations are appropriate in the low to medium Reynolds number ranges, however, some enhancements required for higher speed simulations are noted.
UR - https://www.scopus.com/pages/publications/84938926554
U2 - 10.1115/89-GT-128
DO - 10.1115/89-GT-128
M3 - Conference contribution
AN - SCOPUS:84938926554
T3 - Proceedings of the ASME Turbo Expo
BT - Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition, GT 1989
Y2 - 4 June 1989 through 8 June 1989
ER -