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Publikováno v:
Laakso, R, Kettunen, J & Lähteenmäki, J 2020, Hawk Mk 51/51A/66 Tailplane Full-Scale Fatigue Tests . in A Niepokolczycki & J Komorowski (eds), Structural Integrity in the Age of Additive Manufacturing : ICAF 2019 . Springer, Lecture Notes in Mechanical Engineering, pp. 801-815, 30th Symposium of the International Committee on Aeronautical Fatigue, ICAF 2019, Warsaw, Poland, 2/06/19 . https://doi.org/10.1007/978-3-030-21503-3_63
Until 2017, there was no certainty about the fatigue life of Hawk tailplanes in FINAF’s flight conditions. Then full-scale fatigue tests were performed to determine if the FINAF is required to procure more tailplanes, and to extract evidence, which
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=355e65625b88::1f51e53423aa14753779dd6e19929b2f
https://cris.vtt.fi/en/publications/e5012c7e-88d8-4ead-9cd1-8479b8cb6052
https://cris.vtt.fi/en/publications/e5012c7e-88d8-4ead-9cd1-8479b8cb6052