The future development of aerial navigation is closely connected with the condition of obtaining airplanes of great stability and sufficient strength. Different construction materials such as wood, aluminum, iron, and alloys are examined to determine which materials or combination of materials provides a greater coefficient of safety
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
The D.H. 66, constructed at Stag Lane Works of the De Haviland Aircraft Company built for Imperial A...
It has long been thought that metal construction of airplanes would involve an increase in weight as...
The present state of the problem of materials in airplane construction is studied on the basis of da...
In this report we will consider, as the dominating characteristic, either the load carried, the spee...
Different methods of constructing light airplanes are presented with a view toward increasing produc...
An airship frame may be regarded as a rigid girder subjected to a number of forces which, according ...
Since lightness is desirable in airplane construction, greater stresses must be tolerated than in ot...
This article is based on the experience of the Schute-Lanz Airship Company in light construction. Th...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
The use of duralumin by French airplane designers is presented, the results they have obtained, and ...
The first part of this report shows the differences between commercial and war airships and then goe...
Various details of design or arrangement of the parts of airplane structures are shown and discussed...
A comparison of the relative economy of airplane construction shows that monoplanes are cheaper than...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
The D.H. 66, constructed at Stag Lane Works of the De Haviland Aircraft Company built for Imperial A...
It has long been thought that metal construction of airplanes would involve an increase in weight as...
The present state of the problem of materials in airplane construction is studied on the basis of da...
In this report we will consider, as the dominating characteristic, either the load carried, the spee...
Different methods of constructing light airplanes are presented with a view toward increasing produc...
An airship frame may be regarded as a rigid girder subjected to a number of forces which, according ...
Since lightness is desirable in airplane construction, greater stresses must be tolerated than in ot...
This article is based on the experience of the Schute-Lanz Airship Company in light construction. Th...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
The use of duralumin by French airplane designers is presented, the results they have obtained, and ...
The first part of this report shows the differences between commercial and war airships and then goe...
Various details of design or arrangement of the parts of airplane structures are shown and discussed...
A comparison of the relative economy of airplane construction shows that monoplanes are cheaper than...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
The D.H. 66, constructed at Stag Lane Works of the De Haviland Aircraft Company built for Imperial A...