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: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Vilnius Gediminas Technical University
2004-06-01
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| Series: | Aviation |
| Subjects: | |
| Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/7463 |
| _version_ | 1811191498367041536 |
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| author | Antanas Žiliukas Nina Fiodorova |
| author_facet | Antanas Žiliukas Nina Fiodorova |
| author_sort | Antanas Žiliukas |
| collection | DOAJ |
| description | 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.
First Published Online: 14 Oct 2010 |
| first_indexed | 2024-04-11T15:06:54Z |
| format | Article |
| id | doaj.art-1a04ea52a00e4cdbb4cc004ceae547cf |
| institution | Directory Open Access Journal |
| issn | 1648-7788 1822-4180 |
| language | English |
| last_indexed | 2024-04-11T15:06:54Z |
| publishDate | 2004-06-01 |
| publisher | Vilnius Gediminas Technical University |
| record_format | Article |
| series | Aviation |
| spelling | doaj.art-1a04ea52a00e4cdbb4cc004ceae547cf2022-12-22T04:16:47ZengVilnius Gediminas Technical UniversityAviation1648-77881822-41802004-06-018210.3846/16487788.2004.9635868Absorption of energy exploitation during impact of aircraftAntanas Žiliukas0Nina Fiodorova1VGTU Antanas Gustaitis Aviation Institute, LithuaniaVGTU Antanas Gustaitis Aviation Institute, LithuaniaThe 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. First Published Online: 14 Oct 2010https://journals.vgtu.lt/index.php/Aviation/article/view/7463aircraftimpactenergyvelocitystopping distance |
| spellingShingle | Antanas Žiliukas Nina Fiodorova Absorption of energy exploitation during impact of aircraft Aviation aircraft impact energy velocity stopping distance |
| title | Absorption of energy exploitation during impact of aircraft |
| title_full | Absorption of energy exploitation during impact of aircraft |
| title_fullStr | Absorption of energy exploitation during impact of aircraft |
| title_full_unstemmed | Absorption of energy exploitation during impact of aircraft |
| title_short | Absorption of energy exploitation during impact of aircraft |
| title_sort | absorption of energy exploitation during impact of aircraft |
| topic | aircraft impact energy velocity stopping distance |
| url | https://journals.vgtu.lt/index.php/Aviation/article/view/7463 |
| work_keys_str_mv | AT antanasziliukas absorptionofenergyexploitationduringimpactofaircraft AT ninafiodorova absorptionofenergyexploitationduringimpactofaircraft |