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Paper
Title

DESIGN AND ANALYSIS OF AIRCRAFT GASPER SYSTEM

Year: 1389
COI: NIVHC02_042
Language: EnglishView: 2,347
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Authors

Mohammad Hadi Esteki - Air Distribution System Expert, Aeronautical Design Center of Iran Aircraft Manufacturing Industries Co
Sayed Mohammad Reza Afghari - Air Condition System Expert, Aeronautical Design Center of Iran Aircraft Manufacturing Industries Co
Sattar Shahbaz - Life Support Systems Dep. Manager, Aeronautical Design Center of Iran Aircraft Manufacturing Industries Co.

Abstract:

In this paper, aircraft air distribution system has been analyzed. To achieve that, ducting pressure loss and air flow throw gaspers calculations has been done for cabin ducts in according to exact location of individual air distribution system in the cabin. Then the length of gasper air flow was compared with the distance between gasper outlet and passengers seats. Finally the results show good agreement between air flow throw gaspers and gasper to passenger distance that make comfortable air feeling conditions. Therefore adding of gasper system to available distribution system must be designed in according to least modifications, suitable location and good air flow throw gaspers.

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Paper COI Code

This Paper COI Code is NIVHC02_042. Also You can use the following address to link to this article. This link is permanent and is used as an article registration confirmation in the Civilica reference:

https://civilica.com/doc/110167/

How to Cite to This Paper:

If you want to refer to this Paper in your research work, you can simply use the following phrase in the resources section:
Esteki, Mohammad Hadi and Afghari, Sayed Mohammad Reza and Shahbaz, Sattar,1389,DESIGN AND ANALYSIS OF AIRCRAFT GASPER SYSTEM,2nd national Industrial Ventilation & Hygeine Conference,Tehran,https://civilica.com/doc/110167

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  • Fax, R. W., Mc. Donald, A.T. "Introduction to FIuid Mechanics", ...
  • Aircraft Maintenance manual & Flight Manual. ...
  • "Aero thermodynamic Systems Engineering and Design", SAE AIR1168/3, 1990-0)9-05. ...
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