We are here giving a summary of the rules established by the Theoretical Section of the Central Aerodynamic Institute of Moscow for the different calculation cases of an airplane. It appears the engineers of the Aerodynamic Institute considered only thick or medium profiles. For these profiles they have attempted to increase the safety when the center of pressure moves appreciably toward the trailing edge
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This paper calls attention to the desirability of expanding airplane building regulations to include...
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...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
The physical resistance of passengers in establishing an upper limit to the strength of airplane cel...
Load factors and loading conditions are presented for German aircraft. Loading conditions under vari...
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...
The static stresses of airplane parts, the magnitude of which can be determined with the aid of stat...
Since lightness is desirable in airplane construction, greater stresses must be tolerated than in ot...
This article describes a static strength test of a fuselage of a small aircraft. Tests were done acc...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This paper calls attention to the desirability of expanding airplane building regulations to include...
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...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
Every strength calculation, including those on airplanes, must be preceded by a determination of the...
The physical resistance of passengers in establishing an upper limit to the strength of airplane cel...
Load factors and loading conditions are presented for German aircraft. Loading conditions under vari...
The following load assumptions shall be taken as the basis of the strength calculations. Certain def...
The static stresses of airplane parts, the magnitude of which can be determined with the aid of stat...
Since lightness is desirable in airplane construction, greater stresses must be tolerated than in ot...
This article describes a static strength test of a fuselage of a small aircraft. Tests were done acc...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
The author gives a survey of the principles of stress analysis and design of airplane structures, an...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This paper calls attention to the desirability of expanding airplane building regulations to include...