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 in order 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 translated abstract in Metallurgist (Supp. to Engineer), Apr. 26, 1929, pp. 52-53)
Dynamic Strength of Airplane Parts
Dynamische Festigkeit von Flugzeug-Konstruktionsteilen
V.D.I. Zeitschrift ; 72 , n 51
1928
6 pages
24 Figs.
Article (Journal)
German
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