Every strength calculation, including those on airplanes, must be preceded by a determination of the forces to be taken into account. In the following discussion, it will be assumed that the magnitudes of these forces are known and that it is only a question of how, on the basis of these known forces, to meet the prescribed conditions on the one hand and the practical requirements on the other.
Strength calculations on airplanes
1925-12-01
Miscellaneous
No indication
English
Strength calculations on airplanes
Engineering Index Backfile | 1925
|Loads and calculations of army airplanes
NTRS | 1921
|Tail Load Calculations for Light Airplanes
Online Contents | 1994
|Tail load calculations for light airplanes
AIAA | 1994
|PRACTICAL AEROELASTIC CALCULATIONS FOR LIGHT AIRPLANES
British Library Conference Proceedings | 2008
|