Dynamic Fatigue Tests Of Landing Gears

References

[1] Jachimowicz, J., Kowalski, W. and Wołejsza, Z., 1999, Metodyka określania resursu podwozi lotniczych na podstawie badań i eksploatacji, Transactions of the Institute of Aviation, 159(4), pp. 23-29.
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[2] Currey, N.S., Aircraft Landing Gear Design Principles and Practices, Washington AIAA 1988.10.2514/4.861468
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[3] Kowalski, W., et al., (2005), State of the art in landing gear shock absorbers. Transactions of the Institute of Aviation, 181(2), pp. 1-65.
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[4] Skorupka, Z. and Paprzycki, I., (2014), Laboratoryjne badania podwozi lotniczych, Transport przemysłowy i maszyny robocze, ISSN 1899-5489.
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[5] MIL-A-8867C(AS), Airplane Strength and Rigidity, Ground Tests
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[6] Normal, Utility, Aerobatic and Commuter Aeroplanes, CS-23, European Aviation Safety Agency (EASA)
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[7] Wikipedia, the free encyclopedia, (2020, May), Landing gear, from https://en.wikipedia.org/wiki/Landing_gear#/media/File:Antonov_An-124._Basic_chassis.jpg.
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