The following load assumptions shall be taken as the basis of the strength calculations. Certain definite load conditions (e.g. of flight, control, landing and transport) shall be assumed. The loads shall be assumed to be safe loads, constant or only slowly variable, and the inertia forces due to elastic deformation are accordingly disregarded. The external forces, the force of gravity and the inertia forces on the whole airplane shall produce a condition of equilibrium.
Load assumptions for calculating the strength of airplanes
1930-09-01
Miscellaneous
No indication
English
Load assumptions for calculating the strength of airplanes
Engineering Index Backfile | 1930
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Engineering Index Backfile | 1927
|Calculating maximum speed of airplanes
Engineering Index Backfile | 1931
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NTRS | 1925
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