<abstract xml:lang="en" xmlns="http://www.w3.org/1999/xhtml"><p>This paper describes the problem of searching for the causes of damage in the form of rupture of a strength member of the main landing gear. There have been two incidents noted which both occurred during hangar storage. It should be pointed out that the two occurrences mentioned concern a particular aircraft currently in operation, and that these incidents occurred a few days after the last flight.</p><p>This article presents part of the investigation process needed to determine the causes of cracks in the test item. The crack growth analysis of the pull rod was performed using the NASGRO software. In order to perform the calculations, the information was gathered during previously conducted material studies and flight tests.</p></abstract>

This paper describes the problem of searching for the causes of damage in the form of rupture of a strength member of the main landing gear. There have been two incidents noted which both occurred during hangar storage. It should be pointed out that the two occurrences mentioned concern a particular aircraft currently in operation, and that these incidents occurred a few days after the last flight.This article presents part of the investigation process needed to determine the causes of cracks in the test item. The crack growth analysis of the pull rod was performed using the NASGRO software. In order to perform the calculations, the information was gathered during previously conducted material studies and flight tests.

Crack Growth Analysis of the Landing Gear Pull Rod of the Fighter Jet Aircraft

Air Force Institute of Technology, Warsaw, Poland

Fatigue of Aircraft Structures

{"article-title":"Crack Growth Analysis of the Landing Gear Pull Rod of the Fighter Jet Aircraft"}

This paper describes the problem of searching for the causes of damage in the form of rupture of a strength member of the main landing gear. There have been...

Crack Growth Analysis of the Landing Gear Pull Rod of the Fighter Jet Aircraft

Pubblicato online: 25 ago 2011

Pagine: 64 - 73

DOI: https://doi.org/10.2478/v10164-010-0039-1

Parole chiave
crack growth, fatigue, flight tests, landing gear

This content is open access.

Crack Growth Analysis of the Landing Gear Pull Rod of the Fighter Jet Aircraft

Pubblicato online: 25 ago 2011

Pagine: 64 - 73

DOI: https://doi.org/10.2478/v10164-010-0039-1

Parole chiavecrack growth, fatigue, flight tests, landing gear

This content is open access.

Parole chiave
crack growth, fatigue, flight tests, landing gear