It is shown that the force distribution resulting from incomplete ribs in single spar wing structures may be determined with the aid of the shear field method by a statistically indeterminate computation. A numerical computation is given of the force distribution of a wing structure whose two neighboring incomplete ribs with web missing in half the section are torsionally loaded
Bending tests with transverse loads and with pure bending were undertaken on a double-web monocoque ...
Airplane wing trusses are generally designed to contain redundant members (stagger wires and externa...
Logical analysis of a box wing necessitates the allowance for the contribution of the drag spars to ...
A method is presented for approximate static calculation, which is based on the customary assumption...
This report deals with the analysis of 2-spar cantilever wings in torsion, taking cognizance of the ...
The purpose of this treatise is, first of all, the determination of the effect of variously loaded s...
The aim of the project is to develop a calculation process for the influence of the number of unifor...
This lecture concerns the combining effects in airplane wings so as to save some of the dead weight
This report describes a simple method for calculating the position of the elastic axis of a wing str...
The aim of the project is to develop a calculation process for the influence of the number of unifor...
The present paper treats less of the effect of the union (of spars and ribs, namely, the reduction o...
The stress relations to the fabric and the rib consequent upon a change of spacing between ribs in a...
The calculation of wing spars of constant cross-section and load has been thoroughly treated by a la...
The purpose of the study was to develop improvements in the current methods for the calculation of t...
The fleet structure consists of skin, ribs and sections of peace. The fox carries a flight load and ...
Bending tests with transverse loads and with pure bending were undertaken on a double-web monocoque ...
Airplane wing trusses are generally designed to contain redundant members (stagger wires and externa...
Logical analysis of a box wing necessitates the allowance for the contribution of the drag spars to ...
A method is presented for approximate static calculation, which is based on the customary assumption...
This report deals with the analysis of 2-spar cantilever wings in torsion, taking cognizance of the ...
The purpose of this treatise is, first of all, the determination of the effect of variously loaded s...
The aim of the project is to develop a calculation process for the influence of the number of unifor...
This lecture concerns the combining effects in airplane wings so as to save some of the dead weight
This report describes a simple method for calculating the position of the elastic axis of a wing str...
The aim of the project is to develop a calculation process for the influence of the number of unifor...
The present paper treats less of the effect of the union (of spars and ribs, namely, the reduction o...
The stress relations to the fabric and the rib consequent upon a change of spacing between ribs in a...
The calculation of wing spars of constant cross-section and load has been thoroughly treated by a la...
The purpose of the study was to develop improvements in the current methods for the calculation of t...
The fleet structure consists of skin, ribs and sections of peace. The fox carries a flight load and ...
Bending tests with transverse loads and with pure bending were undertaken on a double-web monocoque ...
Airplane wing trusses are generally designed to contain redundant members (stagger wires and externa...
Logical analysis of a box wing necessitates the allowance for the contribution of the drag spars to ...