Identification of helicopter mass flexibility characteristics

Authors

  • Лe Тхе Шон Національний авіаційний університет
  • А. Н. Клипа Національний авіаційний університет

DOI:

https://doi.org/10.18372/2306-1472.3.9375

Abstract

Considered is the problem of identification of helicopter mass flexibility characteristics, in par­ticular, that of the rotor. Differential equation of blade free oscillations in centrifugal force field is used as a mathematical model of flexible oscillations. The solution of the problem is made on the ba­sis of coordination of experimental and rated proper forms of elastic oscillations

References

Штейнберг Ш.Е. Идентификация в системах управления- М.: Энергоатомиздат, 1987 - С.21-30. .

Миль М.Л. Вертолеты. Расчет и проектирование. 42. Колебания и динамическая прочность. - М.: Машиностроение, 1967. - С.23-24.

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How to Cite

Шон, Л. Т., & Клипа, А. Н. (1999). Identification of helicopter mass flexibility characteristics. Proceedings of National Aviation University, 3(2), 77–82. https://doi.org/10.18372/2306-1472.3.9375

Issue

Vol. 3 No. 2 (1999)

Section

MODERN AVIATION AND SPACE TEHNOLOGY

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