A FORTRAN 4 digital computer program is presented for the initial postbuckling and imperfection sensitivity analysis of bifurcation buckling modes for ring-stiffened orthotropic multilayered shells of revolution. The boundary value problem for the second-order contribution to the buckled state was solved by the forward integration technique using the Runge-Kutta method. The effects of nonlinear prebuckling states and live pressure loadings are included."NASA CR-1801.""October 1971."Cover title.Includes bibliographical references (p. 179)A FORTRAN 4 digital computer program is presented for the initial postbuckling and imperfection sensitivity analysis of bifurcation buckling modes for ring-stiffened orthotropic multilayered shells of revolu...
The information necessary for application of the STARS-2P (shell theory automated for rotational str...
This report investigates an analytical evaluation of buckling modes of shell configurations to deter...
A procedure for the structural analysis of stiffened shells of revolution is presented. A digital co...
A study of the buckling of thin shells was conducted using a digital computer program for the geomet...
Computer program performs stability analyses for a wide class of shells without unduly restrictive a...
A study of the buckling of thin shells was conducted using a digital computer program for the geomet...
The modified structure method, which is based on Koiter's theory of imperfections, was used to calcu...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
The theoretical analysis background for the STARS-2P nonlinear inelastic program is discussed. The t...
The purpose of this report's analysis is to develop a numerical method and computer program for the ...
The equations and method of solution for a series of five compatible computer programs for structura...
A user manual and related program documentation is presented for six compatible computer programs fo...
Thin-walled structures are capable of carrying loads very efficiently. However, they are prone to bu...
Computer program on axisymmetric response of shells with other meridional geometries and response of...
Nonlinear problems are treated which involve geometrical nonlinearities occurring because of geometr...
The information necessary for application of the STARS-2P (shell theory automated for rotational str...
This report investigates an analytical evaluation of buckling modes of shell configurations to deter...
A procedure for the structural analysis of stiffened shells of revolution is presented. A digital co...
A study of the buckling of thin shells was conducted using a digital computer program for the geomet...
Computer program performs stability analyses for a wide class of shells without unduly restrictive a...
A study of the buckling of thin shells was conducted using a digital computer program for the geomet...
The modified structure method, which is based on Koiter's theory of imperfections, was used to calcu...
The buckling modes of four optimized Mars entry aeroshell configurations at angle-of-attack loadings...
The theoretical analysis background for the STARS-2P nonlinear inelastic program is discussed. The t...
The purpose of this report's analysis is to develop a numerical method and computer program for the ...
The equations and method of solution for a series of five compatible computer programs for structura...
A user manual and related program documentation is presented for six compatible computer programs fo...
Thin-walled structures are capable of carrying loads very efficiently. However, they are prone to bu...
Computer program on axisymmetric response of shells with other meridional geometries and response of...
Nonlinear problems are treated which involve geometrical nonlinearities occurring because of geometr...
The information necessary for application of the STARS-2P (shell theory automated for rotational str...
This report investigates an analytical evaluation of buckling modes of shell configurations to deter...
A procedure for the structural analysis of stiffened shells of revolution is presented. A digital co...