The Shock-Absorbed System of the Airplane Landing Gear
Description:
"A discussion is given of the behavior of the shock-absorbing system, consisting of elastic struts and tires, under landing, take-off, and taxying conditions, and a general formula derived for obtaining the minimum stroke required to satisfy the conditions imposed on the landing gear. Finally, the operation of some typical shock-absorbing systems are examined and the necessity brought out for taking into account, in dynamic landing-gear tests, the effect of the wing lift at the instant of conta…
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Date:
March 1940
Creator:
Callerio, Pietro
Partner:
UNT Libraries Government Documents Department