The STRESS ANALYSIS AND FATIGUE DAMAGE ESTIMATION FOR SEAT SUPPORT ATTACHMENT

Autor: Veeresh C Panshetty, Dr. Manjunath L H, K. E. Girish

Publikováno v: I. J. of Advances in Scientific Research and Engineering-IJASRE (ISSN: 2454-8006); Vol. 3 No. 5 (2017): Volume 3, Issue 5 June (2017); 118-125

Aircraft structure is the most obvious example where structural efficiency results in light weight and high operating stresses. Airframe experiences variable loading in service. The paper presents the response of fuselage seat attachment due to cabin

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https://ijasre.net/index.php/ijasre/article/view/390