论文信息 - Frictionless contact of aircraft tires

Frictionless contact of aircraft tires

A computational procedure for the solution of frictionless contact problems of spacecraft tires was developed using a two-dimensional laminated anisotropic shell theory incorporating the effects of variations in material and geometric parameters, transverse shear deformation, and geometric nonlinearities to model the nose-gear tire of a space shuttle. Numerical results are presented for the case when the nose-gear tire is subjected to inflation pressure and pressed against a rigid pavement. The results are compared with experimental results obtained at NASA Langley, demonstrating a high accuracy of the model and the effectiveness of the computational procedure.

Ahmed K. Noor | J. A. Tanner | John A. Tanner | A. Noor | Kyun O. Kim

[1] Peter Wriggers,et al. Algorithms for non-linear contact constraints with application to stability problems of rods and shells , 1987 .

[2] Walter Wunderlich,et al. Application of ring elements in the nonlinear analysis of shells of revolution under nonaxisymmetric loading , 1985 .

[3] L. Adams. m-Step Preconditioned Conjugate Gradient Methods , 1985 .

[4] Ahmed K. Noor,et al. Mixed finite element formulation for frictionless contact problems , 1989 .

[5] H. G. Schaeffer,et al. Nonlinear deflections of asymmetrically loaded shells of revolution. , 1968 .

[6] A. K. Noor,et al. Nonlinear analysis of anisotropic panels , 1986 .

[7] J. C. Simo,et al. A perturbed Lagrangian formulation for the finite element solution of contact problems , 1985 .

[8] Bernard Budiansky,et al. Notes on nonlinear shell theory. , 1968 .

[9] Ahmed K. Noor,et al. Modeling and analysis of the space shuttle nose-gear tire with semianalytic finite elements , 1990 .

[10] Ahmed K. Noor,et al. On making large nonlinear problems small , 1982 .

[11] Ahmed K. Noor. Reduction method for the non‐linear analysis of symmetric anisotropic panels , 1986 .

[12] J. L. Sanders,et al. NONLINEAR THEORIES FOR THIN SHELLS , 1963 .