Zobrazeno 1 - 6
of 6
pro vyhledávání: '"N. C. Mahendra Babu"'
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811605499
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e9b146736a72a4c096a8fa61e59a23f
https://doi.org/10.1007/978-981-16-0550-5_38
https://doi.org/10.1007/978-981-16-0550-5_38
Autor:
N. C. Mahendra Babu, A. R. Aditya
Publikováno v:
AIP Conference Proceedings.
Curved stiffeners offer certain advantages over conventional isogrid stiffeners in GSS. Recent developments in composite materials manufacturing process like Automatic fiber placement technique have made fabrication of curved GSS easier. The present
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58c94ea312e2f40adde3496d4aaf7c88
https://doi.org/10.1063/1.5141564
https://doi.org/10.1063/1.5141564
Publikováno v:
Indian Journal of Science and Technology. 10:1-6
Exhaust manifold of an IC engine typically experiences cyclic thermal and mechanical loading and are prone to TMF failure. Thermo-mechanical fatigue resistance needs to be ensured for exhaust manifold to meet the requirement of durability in order to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::148b368fa5dcb542d6aeed2dd451377a
https://doi.org/10.17485/ijst/2017/v10i12/105559
https://doi.org/10.17485/ijst/2017/v10i12/105559
Publikováno v:
AIP Conference Proceedings.
Designing and analyzing grid stiffened panel to understand the effect of stiffeners on stiffness of the panel is crucial in designing grid stiffened cylinder for fuselage application. Traditionally only straight stiffeners were used due to limited ma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::963b1734e8d3ac0f88e9b4442ad5d06d
https://doi.org/10.1063/1.5029582
https://doi.org/10.1063/1.5029582
Publikováno v:
Advances in Structural Integrity ISBN: 9789811071966
Fracture mechanics provides a methodology for prediction, prevention and control of fracture in materials, components, and structures. Fracture mechanics analysis is the backbone of damage tolerant design. Objectives of fracture mechanics analysis ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d8d9a888cfa30f9fbc5a0bdfd0ee44c7
https://doi.org/10.1007/978-981-10-7197-3_2
https://doi.org/10.1007/978-981-10-7197-3_2
Publikováno v:
International Journal of Vehicle Structures and Systems. 6
Ring frames, stringers and skin panels are the main parts of aircraft fuselage structure. Circumferential joint is formed by joining skin panels in circumferential direction using doubler plates and adhesive bonding. In this paper finite element (FE)
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e62838a399353cd0c432170b28186b9f
https://doi.org/10.4273/ijvss.6.4.03
https://doi.org/10.4273/ijvss.6.4.03