TY - JOUR
T1 - Analysis of fluid - Structure interactions using a time-marching technique
AU - Jadic, I.
AU - So, R. M C
AU - Mignolet, Marc
N1 - Funding Information:
Contract support given to R.M.C.So during his tenure at Arizona State University by the Naval Surface Warfare Center, Carderock Division, Department of the Navy, Bethesda, MD 20084, U.S.A., is gratefully acknowledged. The contract was monitored by Dr W. Tang. R.M.C.So would further like to acknowledge the support given to him by the Hong Kong Polytechnic University for the completion of the project and the preparation of this paper.
PY - 1998/8
Y1 - 1998/8
N2 - Fluid-structure interaction problems arise in many different areas of engineering where the system considered or some of its components are directly in contact with a fluid. Examples are aircraft, jet engines, ships, pipelines, nuclear and chemical reactors, offshore structures, bridges, etc. In these cases, the fluid often plays an important role in determining the behavior of the structure of interest. For example, flutter could have disastrous consequences on aircraft, and resonances resulting from flow-induced vibrations could provoke structural failures in nuclear reactors, bridges and other structures subjected to a cross-flow. To prevent these potential dramatic and expensive accidents, it is necessary to seek a reliable technique for the determination of the characteristics, in particular natural frequencies, damping levels and fatigue life, of the structure in the presence of the fluid. This computation has often been accomplished in the past by relying on either a total or substantial decoupling of the fluid and structural problems, but the ever increasing emphasis on reliability, efficiency, and weight motivates the use of precise strategies for the determination of the fluid and structural behaviour. Recent efforts in this area indicate that a time-marching solution for the combined fluid and structure governing equations is computationally feasible and may provide the necessary accuracy. The present investigation essentially verifies this approach and makes available a time-marching technique that fully resolves the fluid-structure interactions. As an illustration, the single airfoil flutter problem is first analysed in detail. This is followed by an investigation of the nonlinearity in the response of the airfoil. New insights thus obtained are presented and discussed.
AB - Fluid-structure interaction problems arise in many different areas of engineering where the system considered or some of its components are directly in contact with a fluid. Examples are aircraft, jet engines, ships, pipelines, nuclear and chemical reactors, offshore structures, bridges, etc. In these cases, the fluid often plays an important role in determining the behavior of the structure of interest. For example, flutter could have disastrous consequences on aircraft, and resonances resulting from flow-induced vibrations could provoke structural failures in nuclear reactors, bridges and other structures subjected to a cross-flow. To prevent these potential dramatic and expensive accidents, it is necessary to seek a reliable technique for the determination of the characteristics, in particular natural frequencies, damping levels and fatigue life, of the structure in the presence of the fluid. This computation has often been accomplished in the past by relying on either a total or substantial decoupling of the fluid and structural problems, but the ever increasing emphasis on reliability, efficiency, and weight motivates the use of precise strategies for the determination of the fluid and structural behaviour. Recent efforts in this area indicate that a time-marching solution for the combined fluid and structure governing equations is computationally feasible and may provide the necessary accuracy. The present investigation essentially verifies this approach and makes available a time-marching technique that fully resolves the fluid-structure interactions. As an illustration, the single airfoil flutter problem is first analysed in detail. This is followed by an investigation of the nonlinearity in the response of the airfoil. New insights thus obtained are presented and discussed.
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U2 - 10.1006/jfls.1998.0163
DO - 10.1006/jfls.1998.0163
M3 - Article
AN - SCOPUS:0000438448
SN - 0889-9746
VL - 12
SP - 631
EP - 654
JO - Journal of Fluids and Structures
JF - Journal of Fluids and Structures
IS - 6
ER -