Add to ORKGThe present investigation relates to a box-type fuselage with sides consisting of thin smooth sheet metal, stiffened by longitudinal members riveted to the flanged channel-section bulkheads or transverse frames and to the semicircular corrugated corner stiffenings. The results obtained in this particular case can be applied to a great number of similar structures
Previous investigations on the strength characteristics and structure of wood in construction are an...
A monocoque box beam consisting of a 24S-T aluminum-alloy sheet reinforced by four bulkheads and by ...
Two full-scale wing boxes with different types of butt joints were investigated under pure bending l...
The present investigation relates to a box-type fuselage with sides consisting of thin smooth sheet ...
This note is on an investigation made to obtain information on the strength of thin curved sheets of...
In the calculation of the dimensions of modern machines and building constructions, account is taken...
In this study, the effect of hole reinforcement on the buckling behaviour of thin-walled structures ...
In this study, the effect of hole reinforcement on the buckling behaviour of thin-walled structures ...
In practice the actual maximum stress is greater than the stress determined by the simple girder the...
A full-scale section of a transport aircraft wing box was designed, analyzed, fabricated, and tested...
Bending tests with transverse loads and with pure bending were undertaken on a double-web monocoque ...
This report is a compilation of previously published articles on formulas and methods of calculation...
Compression tests were conducted on 247 panels with Z-section stiffeners and 304 panels with hat-sec...
The monocoque form of airplane construction has introduced a number of new problems to the stress ca...
Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diago...
Previous investigations on the strength characteristics and structure of wood in construction are an...
A monocoque box beam consisting of a 24S-T aluminum-alloy sheet reinforced by four bulkheads and by ...
Two full-scale wing boxes with different types of butt joints were investigated under pure bending l...
The present investigation relates to a box-type fuselage with sides consisting of thin smooth sheet ...
This note is on an investigation made to obtain information on the strength of thin curved sheets of...
In the calculation of the dimensions of modern machines and building constructions, account is taken...
In this study, the effect of hole reinforcement on the buckling behaviour of thin-walled structures ...
In this study, the effect of hole reinforcement on the buckling behaviour of thin-walled structures ...
In practice the actual maximum stress is greater than the stress determined by the simple girder the...
A full-scale section of a transport aircraft wing box was designed, analyzed, fabricated, and tested...
Bending tests with transverse loads and with pure bending were undertaken on a double-web monocoque ...
This report is a compilation of previously published articles on formulas and methods of calculation...
Compression tests were conducted on 247 panels with Z-section stiffeners and 304 panels with hat-sec...
The monocoque form of airplane construction has introduced a number of new problems to the stress ca...
Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diago...
Previous investigations on the strength characteristics and structure of wood in construction are an...
A monocoque box beam consisting of a 24S-T aluminum-alloy sheet reinforced by four bulkheads and by ...
Two full-scale wing boxes with different types of butt joints were investigated under pure bending l...