Discussion of various factors which may give rise to alternating or fatigue stresses in airplane; main causes are aerodynamic and engine effects; parts most affected by engine vibration are engine bearers, radiator and fuel piping and controls; fundamentals of fatigue failure; examples; recommendations as to procedure inorder to ensure that all aircraft members shall have sufficient strength against alternating stresses. Dynamic stresses and vibrations in airplanes; fatigue strength of alloys and metals used in airplane construction; examples from aviation practice illustrating failure by fatigue; methods of insuring dynamic strength in airplane construction. (See also vol. 72 no. 51, Dec. 22, 1928 pp. 24 figs)
Dynamic Strength of Airplane Parts
Dynamische festigkeit von flugzeug-konstruktionsteilen
1929
2 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Dynamic breaking tests of airplane parts
Engineering Index Backfile | 1933
|Dynamic destructive tests on airplane parts
Engineering Index Backfile | 1931
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1942
|Phenolic fibre in airplane parts
Engineering Index Backfile | 1945
|