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NASA NTRS · 19930094760

Dynamic testing of airplane shock-absorbing struts

Abstract

Measurement of perpendicular impacts of a landing gear with different shock-absorbing struts against the drum testing stand. Tests were made with pneumatic shock absorbers having various degrees of damping, liquid shock absorbers, steel-spring shock absorbers and rigid struts. Falling tests and rolling tests. Maximum impact and gradual reduction of the impacts in number and time in the falling tests. Maximum impact and number of weaker impacts in rolling tests.

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BibTeXRIS

Langer, P, Thome, W. 1932-01-01. Dynamic testing of airplane shock-absorbing struts. https://ntrs.nasa.gov/citations/19930094760

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