Add to ORKGThe calculation of wing spars of constant cross-section and load has been thoroughly treated by a large number of authors. Such is not the case,however, regarding the calculation of wing spars whose section and linear load diminish toward the ends, as in wings of trapezoidal contour and decreasing section
Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-momen...
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with...
For computing the critical flutter velocity of a wing among the data required are the position of th...
The present paper treats less of the effect of the union (of spars and ribs, namely, the reduction o...
The calculation of wing spars of constant cross-section and load has been thoroughly treated by a la...
In the present report the computation is actually carried through for the case of parallel spars of ...
The purpose of this treatise is, first of all, the determination of the effect of variously loaded s...
A method is presented for approximate static calculation, which is based on the customary assumption...
This investigation has a double object: 1) the calculation of the general characteristics of certain...
The significance attaching to "column effect" in airplane wing spars has been increasingly realized ...
A method is shown by which the symmetric span loading for a certain class of wings can be simply fou...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
After a brief discussion of the work done up to now on an unwarped wing of constant chord spanning a...
Tables are given for determining the load distribution of tapered wings with partial-span flaps plac...
Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-momen...
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with...
For computing the critical flutter velocity of a wing among the data required are the position of th...
The present paper treats less of the effect of the union (of spars and ribs, namely, the reduction o...
The calculation of wing spars of constant cross-section and load has been thoroughly treated by a la...
In the present report the computation is actually carried through for the case of parallel spars of ...
The purpose of this treatise is, first of all, the determination of the effect of variously loaded s...
A method is presented for approximate static calculation, which is based on the customary assumption...
This investigation has a double object: 1) the calculation of the general characteristics of certain...
The significance attaching to "column effect" in airplane wing spars has been increasingly realized ...
A method is shown by which the symmetric span loading for a certain class of wings can be simply fou...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
After a brief discussion of the work done up to now on an unwarped wing of constant chord spanning a...
Tables are given for determining the load distribution of tapered wings with partial-span flaps plac...
Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-momen...
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with...
For computing the critical flutter velocity of a wing among the data required are the position of th...