Add to ORKGLoad factors and loading conditions are presented for German aircraft. Loading conditions under various stress factors are presented along with a breakdown of individual aircraft components such as landing gear, wings, etc
Aileron calculations have hitherto given greatly differing results according to different authors. I...
The information obtained from flight tests in 1927-1928 covers chiefly the effect of the structural ...
In the calculation of the dimensions of modern machines and building constructions, account is taken...
The historical development of the rules for structural strength of aircraft in the leading countries...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
During the first few years after the war German air-plane activities were practically wiped out, whe...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
The author, who was a captain of the Reserves in the Technical Department of the Aviation Division (...
On the wing structures of modern high speed aircraft, in particular, the comparatively high-service ...
The ultimate test of a load factor formula is experience. The chief advantages of a semi rational fo...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
This paper calls attention to the desirability of expanding airplane building regulations to include...
This report presents a review of German light airplane construction. Some of the topics discussed in...
Aileron calculations have hitherto given greatly differing results according to different authors. I...
The information obtained from flight tests in 1927-1928 covers chiefly the effect of the structural ...
In the calculation of the dimensions of modern machines and building constructions, account is taken...
The historical development of the rules for structural strength of aircraft in the leading countries...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
During the first few years after the war German air-plane activities were practically wiped out, whe...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
The author, who was a captain of the Reserves in the Technical Department of the Aviation Division (...
On the wing structures of modern high speed aircraft, in particular, the comparatively high-service ...
The ultimate test of a load factor formula is experience. The chief advantages of a semi rational fo...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
This paper calls attention to the desirability of expanding airplane building regulations to include...
This report presents a review of German light airplane construction. Some of the topics discussed in...
Aileron calculations have hitherto given greatly differing results according to different authors. I...
The information obtained from flight tests in 1927-1928 covers chiefly the effect of the structural ...
In the calculation of the dimensions of modern machines and building constructions, account is taken...