Absorption of energy exploitation during impact of aircraft
The article shows the variation of stopping distance as a function of deceleration and velocity change derived from the standard Newtonian equations for assumed constant acceleration. Note that the time to stop is equal for all three triangular deceleration‐time pulses but that the stopping distance...
Main Authors: | Antanas Žiliukas, Nina Fiodorova |
---|---|
Format: | Article |
Language: | English |
Published: |
Vilnius Gediminas Technical University
2004-06-01
|
Series: | Aviation |
Subjects: | |
Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/7463 |
Similar Items
-
Interlaminar and intralaminar damage mechanisms of impact resistant aircraft materials under low‐energy impact
by: Neringa Keršienė, et al.
Published: (2006-09-01) -
Numerical simulation of impact of aircraft and engine into concrete wall
by: Kazuma HIROSAKA, et al.
Published: (2016-06-01) -
Design of the Sabot-Stopping System for a Single-Stage Light-Gas Gun for High-Velocity Impacts
by: Leonardo Barilaro, et al.
Published: (2023-06-01) -
The crash energy absorption of the vehicles front structures
by: P. Griškevičius, et al.
Published: (2003-04-01) -
Theoretical Optimal Trajectories for Reducing the Environmental Impact of Commercial Aircraft Operations
by: Cesar Celis, et al.
Published: (2014-02-01)