Symmetric finite element matrix formulations for compressible and incompressible hydroelasticity are developed on the basis of Toupin's complementary formulation of classical mechanics. Results of implementation of the new technique in the NASTRAN structural analysis program are presented which demonstrate accuracy and efficiency
An accurate and efficient numerical solution algorithm is established for solution of the high Reyno...
summary:The subject of this paper is the numerical simulation of aeroelastic problems. The interacti...
This paper presents a procedure for computing the aeroelasticity of wing-body configurations on mult...
A finite element hydroelastic analysis formulation is developed on the basis of Toupin's complementa...
The implementation of a general three-dimensional hydroelastic capability in the NASTRAN computer pr...
The method used to formulate the fluid/structure equations is described in the updates to the NASTRA...
A finite element solution algorithm is established for the two-dimensional Navier-Stokes equations g...
The general application of finite element methodology and the specific application of NASTRAN to a w...
This paper is interested in solution of two-dimensional aeroelastic problems. Two mathematical model...
The general application of finite element methodology and the specific application of NASTRAN to a w...
Formulations and algorithms implemented in the MHOST finite element program are discussed. The code ...
The objective of this research is to develop computationally efficient methods for solving fluid-str...
Recent work has shown that the use of separable symmetric functions of the principal stretches can a...
Cover title.Includes bibliographical references (p. 91).Mode of access: Internet
Vita.The objective of this research is to present a symmetric stiffness matrix for incompressible hy...
An accurate and efficient numerical solution algorithm is established for solution of the high Reyno...
summary:The subject of this paper is the numerical simulation of aeroelastic problems. The interacti...
This paper presents a procedure for computing the aeroelasticity of wing-body configurations on mult...
A finite element hydroelastic analysis formulation is developed on the basis of Toupin's complementa...
The implementation of a general three-dimensional hydroelastic capability in the NASTRAN computer pr...
The method used to formulate the fluid/structure equations is described in the updates to the NASTRA...
A finite element solution algorithm is established for the two-dimensional Navier-Stokes equations g...
The general application of finite element methodology and the specific application of NASTRAN to a w...
This paper is interested in solution of two-dimensional aeroelastic problems. Two mathematical model...
The general application of finite element methodology and the specific application of NASTRAN to a w...
Formulations and algorithms implemented in the MHOST finite element program are discussed. The code ...
The objective of this research is to develop computationally efficient methods for solving fluid-str...
Recent work has shown that the use of separable symmetric functions of the principal stretches can a...
Cover title.Includes bibliographical references (p. 91).Mode of access: Internet
Vita.The objective of this research is to present a symmetric stiffness matrix for incompressible hy...
An accurate and efficient numerical solution algorithm is established for solution of the high Reyno...
summary:The subject of this paper is the numerical simulation of aeroelastic problems. The interacti...
This paper presents a procedure for computing the aeroelasticity of wing-body configurations on mult...