Since lightness is desirable in airplane construction, greater stresses must be tolerated than in other kinds of construction. It is therefore necessary to have a more accurate knowledge of the greatest stresses that may occur and of the actual properties of the materials used. The Aeronautic Research Laboratories took the limit of elasticity as the basis of the strength calculations. Many tests were made of different steels, woods, aluminum alloys, and fabrics
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
The purpose of this investigation is to study the effect of repeated tensile stresses above the prop...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
The present state of the problem of materials in airplane construction is studied on the basis of da...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
It has long been thought that metal construction of airplanes would involve an increase in weight as...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
In the selection of materials for aircraft application, it is not enough to make the selection on a ...
The Impact Endurance Limit is evaluated for several materials used in aircraft construction. The Imp...
The aim of this article is to present, in broad outline, a scientific method for solving the problem...
Tamás Molnár, Péter Szuchy, Sándor Csikós, László Gogolák, István Bíró, József Sáros
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
Laboratory tests were made to obtain information on the load-resisting properties of X76S-T aluminum...
Column and plate compressive strengths of extruded 24S-T aluminum alloy were determined both within ...
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
The purpose of this investigation is to study the effect of repeated tensile stresses above the prop...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
The present state of the problem of materials in airplane construction is studied on the basis of da...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
It has long been thought that metal construction of airplanes would involve an increase in weight as...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
In the selection of materials for aircraft application, it is not enough to make the selection on a ...
The Impact Endurance Limit is evaluated for several materials used in aircraft construction. The Imp...
The aim of this article is to present, in broad outline, a scientific method for solving the problem...
Tamás Molnár, Péter Szuchy, Sándor Csikós, László Gogolák, István Bíró, József Sáros
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
Laboratory tests were made to obtain information on the load-resisting properties of X76S-T aluminum...
Column and plate compressive strengths of extruded 24S-T aluminum alloy were determined both within ...
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
The purpose of this investigation is to study the effect of repeated tensile stresses above the prop...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...