Absorption of energy exploitation during impact of aircraft

Žiliukas, Antanas; Fiodorova, Nina

Use this URL to cite this publication: https://hdl.handle.net/20.500.14911/120305

Absorption of energy exploitation during impact of aircraft

Details

Publication Type (CRIS)

Straipsnis kitoje duomenų bazėje / Article in other database (S4)

Publication Type (eLABa)

Straipsnis kitoje DB / Article in other DB (S3)

Author(s)

Author	Affiliation
Žiliukas, Antanas	Kauno technologijos universitetas	Aeronautikos inžinerijos katedra / Department of Aeronautical Engineering (0842)
Fiodorova, Nina	Antano Gustaičio aviacijos institutas / Antanas Gustaitis' Aviation Institute (08)

Title

Absorption of energy exploitation during impact of aircraft

[en]

A. Žiliukas, N. Fiodorova

Is part of

Aviation : research Journal of Vilnius Gediminas Technical University

Published In

Year	Volume	Issue	Start Page	End Page
2004	8	2	3	8

Publisher

Vilnius : Technika

Referenced in Database(s)(DBs)

Compendex

Extent

p. 3-8

URI

URI
https://hdl.handle.net/20.500.14911/120305

Cited references

Science / Art Area

Technologijos mokslai / Technological sciences (T)

Field of Science / Art

Mechanikos inžinerija / Mechanical Engineering (T009)

Keywords (en)

Abstract (en)

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 distances are not. Minimum stopping distance is achieved with a rectangular pulse, and hence it is the most desired pulse shape from a consideration of deceleration from maximum velocity at a given deceleration level in the shortest possible distance.