Add to ORKGIn practice the actual maximum stress is greater than the stress determined by the simple girder theory, which overestimates the bearing or supporting capacity of the flange. The fact is that the assumptions of the simple girder theory no longer hold true, since normal transverse and shearing stresses are engendered in the plane of the flange
In order to simplify the calculation of beams continuous over three supports, a series of charts hav...
The calculation of wing spars of constant cross-section and load has been thoroughly treated by a la...
This paper calls attention to the desirability of expanding airplane building regulations to include...
In practice the actual maximum stress is greater than the stress determined by the simple girder the...
In this paper the behavior of straight, centrally loaded compression struts is discussed and values ...
The use of different forms of wide-flange, thin-wall steel beams is becoming increasingly widespread...
This report examines the stipulation contained in the 1918 BLV, that a girder subjected to longitudi...
This report analyzes the action of a cantilever T beam with a tension flange so thin it can only car...
The maximum compressive stress carried by a hinged flange is computed from a deformation theory of p...
This report discusses the fundamental action of shear deformation of the flanges on the basis of sim...
Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diago...
Airplane wing trusses are generally designed to contain redundant members (stagger wires and externa...
The present investigation relates to a box-type fuselage with sides consisting of thin smooth sheet ...
Bending tests with transverse loads and with pure bending were undertaken on a double-web monocoque ...
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
In order to simplify the calculation of beams continuous over three supports, a series of charts hav...
The calculation of wing spars of constant cross-section and load has been thoroughly treated by a la...
This paper calls attention to the desirability of expanding airplane building regulations to include...
In practice the actual maximum stress is greater than the stress determined by the simple girder the...
In this paper the behavior of straight, centrally loaded compression struts is discussed and values ...
The use of different forms of wide-flange, thin-wall steel beams is becoming increasingly widespread...
This report examines the stipulation contained in the 1918 BLV, that a girder subjected to longitudi...
This report analyzes the action of a cantilever T beam with a tension flange so thin it can only car...
The maximum compressive stress carried by a hinged flange is computed from a deformation theory of p...
This report discusses the fundamental action of shear deformation of the flanges on the basis of sim...
Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diago...
Airplane wing trusses are generally designed to contain redundant members (stagger wires and externa...
The present investigation relates to a box-type fuselage with sides consisting of thin smooth sheet ...
Bending tests with transverse loads and with pure bending were undertaken on a double-web monocoque ...
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
In order to simplify the calculation of beams continuous over three supports, a series of charts hav...
The calculation of wing spars of constant cross-section and load has been thoroughly treated by a la...
This paper calls attention to the desirability of expanding airplane building regulations to include...