This paper is published in Volume-3, Issue-1, 2017
Area
Aerospace
Author
Vishal Tiwari
Co-authors
Harikant, Pandey A. K.
Org/Univ
Feroze Gandhi Institute of Engineering and Technology, Uttar Pradesh, India
Pub. Date
28 February, 2017
Paper ID
V3I1-1384
Publisher
Keywords
Equilibrium, Inclination, Force-Deflection, Spring-Mass System, Shock Absorption.

Citationsacebook

IEEE
Vishal Tiwari, Harikant, Pandey A. K.. Inclined Lander for Shock Alleviation, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.

APA
Vishal Tiwari, Harikant, Pandey A. K. (2017). Inclined Lander for Shock Alleviation. International Journal of Advance Research, Ideas and Innovations in Technology, 3(1) www.IJARIIT.com.

MLA
Vishal Tiwari, Harikant, Pandey A. K.. "Inclined Lander for Shock Alleviation." International Journal of Advance Research, Ideas and Innovations in Technology 3.1 (2017). www.IJARIIT.com.

Abstract

Paper gives a theoretical solution of shock absorption and represents behavior of inclined Lander during the process of impact landing. It shows a clever mechanical design for shock alleviation and also decreases the chances of accidents during the landing impact. For a long period of time, landing gear or Lander is an important area of research. This paper use theoretical force deflection method for shock alleviation and an analysis of equilibrium of Lander (with help of mass spring damper system at a constant damping) when landed on finite degree inclined. The Inclination of landing gear and effect of wheel spin-up loads is characteristics of dynamic force deflection.
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