NASA Technical Reports Server (NTRS) 19930094835: Load assumptions for calculating the strength of airplanes
Book details
- Title
- NASA Technical Reports Server (NTRS) 19930094835: Load assumptions for calculating the strength of airplanes
- Publication year listed
- 1930
- Format
- Public domain eBook
- Reading access
- Free online reader; no registration required
- Source record
- View on Archive.org
About this book
NASA Technical Reports Server (NTRS) 19930094835: Load assumptions for calculating the strength of airplanes
Author: NASA Technical Reports Server (NTRS)
Year: 1930
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.
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