Zobrazeno 1 - 5
of 5
pro vyhledávání: '"K. E Girish"'
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 1091:012065
In a transport aircraft, there are normally two spars to withstand bending loads. A large part of this bending moment is drawn from the main spar. The main spar in large transport wings is an integrally machined part that is physically connected to t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0fbd4b3b8c0c501892ce73a55f0d8e45
https://doi.org/10.1088/1757-899x/1091/1/012065
https://doi.org/10.1088/1757-899x/1091/1/012065
Publikováno v:
International Journal of Research in Engineering and Technology. :347-354
Integrity of the airframe structure is achieved through rigorous design calculations, stress analysis and structural testing. Finite element method (FEM) is widely used for stress analysis of structural components. Each component in the airframe beco
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a91c664d919163fcf86d921e2c676d6d
https://doi.org/10.15623/ijret.2015.0407056
https://doi.org/10.15623/ijret.2015.0407056
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::9d3b22df3b2f9ba55f92bac0ed5ec24e
https://ijasre.net/index.php/ijasre/article/view/390
https://ijasre.net/index.php/ijasre/article/view/390
Publikováno v:
National Conference on Challenges in Research & Technology in the Coming Decades (CRT 2013).
Aircraft is a mechanical structure which can fly in air. Civil Aircraft is used for transportation and fighter aircraft for defense purpose. It is a challenge in front of the aircraft structural designer to bring out a safest structure with minimum w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6aa3526f9d3081ad77e583ec83748122
https://doi.org/10.1049/cp.2013.2563
https://doi.org/10.1049/cp.2013.2563
Publikováno v:
National Conference on Challenges in Research & Technology in the Coming Decades (CRT 2013).
Transport aircraft typically have two spars in their wings which carry the major bending loads coming on the wings. Sometimes an auxiliary spar is employed for the landing gear attachment. The aerodynamic lift load acting on the top and bottom surfac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6f36001d0be19f21392dfb960dadb073
https://doi.org/10.1049/cp.2013.2560
https://doi.org/10.1049/cp.2013.2560