Add to ORKGThe historical development of the rules for structural strength of aircraft in the leading countries is traced from the beginning of flight to date. The term "factor of safety" is critically analyzed; its replacement by probability considerations has been considered desirable
In this report we will consider, as the dominating characteristic, either the load carried, the spee...
Aileron calculations have hitherto given greatly differing results according to different authors. I...
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...
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...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
This report presents several hypotheses regarding airplane safety, mainly concerning the nondimensio...
This report considers as the dominating characteristic, either the load carried, the speed, the radi...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
During the first few years after the war German air-plane activities were practically wiped out, whe...
Economic and design characteristics are examined in the design of airplanes and airships
In this report we will consider, as the dominating characteristic, either the load carried, the spee...
Aileron calculations have hitherto given greatly differing results according to different authors. I...
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...
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...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
This report presents several hypotheses regarding airplane safety, mainly concerning the nondimensio...
This report considers as the dominating characteristic, either the load carried, the speed, the radi...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
During the first few years after the war German air-plane activities were practically wiped out, whe...
Economic and design characteristics are examined in the design of airplanes and airships
In this report we will consider, as the dominating characteristic, either the load carried, the spee...
Aileron calculations have hitherto given greatly differing results according to different authors. I...
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...