By comparing airplanes of known strength that have resisted all the usual and even extreme air loads with those that under like conditions were found to be insufficiently strong, the researchers, aided by scientific investigations, developed standards which are satisfactory for the calculation of airplane structures. Given here are standards applicable to loads on wing trusses, load factors for use in stress analysis, load factors required in sand testing, loads on control surfaces, loads on wing ribs, loads on landing gear, and rigidity of materials.
Loads and calculations of army airplanes
1921-02-01
Sonstige
Keine Angabe
Englisch
SAE Technical Papers | 1937
|Engineering Index Backfile | 1937
|Engineering Index Backfile | 1937
|“MAINTENANCE PROBLEMS OF ARMY AIRPLANES”
SAE Technical Papers | 1937
|Engineering Index Backfile | 1929