Every strength calculation, including those on airplanes, must be preceded by a determination of the forces to be taken into account. In the following discussion, it will be assumed that the magnitudes of these forces are known and that it is only a question of how, on the basis of these known forces, to meet the prescribed conditions on the one hand and the practical requirements on the other
Various details of design or arrangement of the parts of airplane structures are shown and discussed...
We are here giving a summary of the rules established by the Theoretical Section of the Central Aero...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...
Load factors and loading conditions are presented for German aircraft. Loading conditions under vari...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
Since lightness is desirable in airplane construction, greater stresses must be tolerated than in ot...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
The most essential phenomena of aircraft should be classified according to their origin and then mea...
The ultimate test of a load factor formula is experience. The chief advantages of a semi rational fo...
The historical development of the rules for structural strength of aircraft in the leading countries...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
In the calculation of the dimensions of modern machines and building constructions, account is taken...
Aileron calculations have hitherto given greatly differing results according to different authors. I...
Various details of design or arrangement of the parts of airplane structures are shown and discussed...
We are here giving a summary of the rules established by the Theoretical Section of the Central Aero...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...
Load factors and loading conditions are presented for German aircraft. Loading conditions under vari...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
Since lightness is desirable in airplane construction, greater stresses must be tolerated than in ot...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
The most essential phenomena of aircraft should be classified according to their origin and then mea...
The ultimate test of a load factor formula is experience. The chief advantages of a semi rational fo...
The historical development of the rules for structural strength of aircraft in the leading countries...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
In the calculation of the dimensions of modern machines and building constructions, account is taken...
Aileron calculations have hitherto given greatly differing results according to different authors. I...
Various details of design or arrangement of the parts of airplane structures are shown and discussed...
We are here giving a summary of the rules established by the Theoretical Section of the Central Aero...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...