Design of an Attachment Scheme of a Vehicle to a Typical Fighter Aircraft
| Autor: | Arindam Sarkar, P. S. R. Anjaneyulu, P. C. Jain, Hemant Kumar |
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| Rok vydání: | 2018 |
| Předmět: |
Scheme (programming language)
0209 industrial biotechnology Art design Computer science business.industry 020209 energy Mechanical Engineering Flight vehicle Aerospace Engineering Structural integrity ComputerApplications_COMPUTERSINOTHERSYSTEMS Ocean Engineering 02 engineering and technology Laboratory testing Industrial and Manufacturing Engineering 020901 industrial engineering & automation Flight envelope 0202 electrical engineering electronic engineering information engineering Launch lug Aerospace engineering business computer computer.programming_language |
| Zdroj: | Journal of The Institution of Engineers (India): Series C. 100:239-248 |
| ISSN: | 2250-0553 2250-0545 |
| DOI: | 10.1007/s40032-017-0432-4 |
| Popis: | Design of an attachment scheme of a flight vehicle to a fighter aircraft is a critical task. Here, flight vehicle is a cylindrical body and it is attached to fighter aircraft with the help of a component called launch lug. Loads experienced by the flight vehicle in captive condition have been estimated by using aircraft parameters obtained during previous missions of similar kind of vehicles. This paper provides state of the art design consideration of the attachment scheme (launch lug and shell assembly) of the flight vehicle to the fighter aircraft. The structural integrity of the flight vehicle and its attachments scheme to the fighter aircraft has been verified at various aircraft manoeuvring conditions in its flight envelope through analysis. Design is verified using laboratory testing and in field trials. Finally this flight vehicle with the attachment scheme was used in flight trials. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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