Add to ORKGRecent accidents, which were the result of structural failure in flight, revealed the necessity of a closer examination of the conditions under which the resistance of airplane structures may be calculated
This report presents test results of experiments on the vibration-response characteristics of airpla...
Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diago...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
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...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This report presents several hypotheses regarding airplane safety, mainly concerning the nondimensio...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
The historical development of the rules for structural strength of aircraft in the leading countries...
For the calculation of the parasite resistance of an airplane, a knowledge of the resistance of the ...
The physical resistance of passengers in establishing an upper limit to the strength of airplane cel...
Simple flight tests were made on ten conventional airplanes for the purpose of determining their act...
This report presents general formulas for the determination of all major airplane performance charac...
Load factors and loading conditions are presented for German aircraft. Loading conditions under vari...
On the wing structures of modern high speed aircraft, in particular, the comparatively high-service ...
This report presents test results of experiments on the vibration-response characteristics of airpla...
Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diago...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
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...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This report presents several hypotheses regarding airplane safety, mainly concerning the nondimensio...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
The historical development of the rules for structural strength of aircraft in the leading countries...
For the calculation of the parasite resistance of an airplane, a knowledge of the resistance of the ...
The physical resistance of passengers in establishing an upper limit to the strength of airplane cel...
Simple flight tests were made on ten conventional airplanes for the purpose of determining their act...
This report presents general formulas for the determination of all major airplane performance charac...
Load factors and loading conditions are presented for German aircraft. Loading conditions under vari...
On the wing structures of modern high speed aircraft, in particular, the comparatively high-service ...
This report presents test results of experiments on the vibration-response characteristics of airpla...
Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diago...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...