Numerical Simulation for Strength Increase on Flat Plate Impacted By Bird Using ANSYS-AUTODYN
Аннотация
Bird strike term indicates the collision between an aircraft and bird as occurred during flight can lead to structural damage of an aircraft. This work leads to improvement in aircraft structure by improving its strength and will be able to satisfy the FAR requirements. First of all considering a square flat plate and impacting the impactor at a velocity of 90 m/s performing analysis in ANSYS-AUTODYN software. Results validate with the results given in literature. Ribs are provided in the section increasing its strength, leading to improved design efficiency and safety. Keywords: Lagrangian, ALE, SPH, strength, ribs Cite this Article Karishma Advani, Ahmed Sayyed. Numerical Simulation for Strength Increase on Flat Plate Impacted by Bird Using ANSYS-AUTODYN. Journal of Aerospace Engineering and Technology (JoAET). 2015; 5(3): 38–43p.Опубликован
Выпуск
Раздел
Лицензия
Declaration and Copyright Transfer Form
(to be completed by authors)
I/ We, the undersigned author(s) of the submitted manuscript, hereby declare, that the above manuscript which is submitted for publication in the STM Journals(s), is not published already in part or whole (except in the form of abstract) in any journal or magazine for private or public circulation, and, is not under consideration of publication elsewhere.
· I/We will not withdraw the manuscript after 1 week of submission as I have read the Author Guidelines and will adhere to the guidelines.
· I/We Author(s ) have niether given nor will give this manuscript elsewhere for publishing after submitting in STM Journal(s).
· I/ We have read the original version of the manuscript and am/ are responsible for the thought contents embodied in it. The work dealt in the manuscript is my/ our own, and my/ our individual contribution to this work is significant enough to qualify for authorship.
· I/We also agree to the authorship of the article in the following order:
Author’s name
1. ________________
2. ________________
3. ________________
_______________
We Author(s) tick this box and would request you to consider it as our signature as we agree to the terms of this Copyright Notice, which will apply to this submission if and when it is published by this journal. |