PRESSURE DROP TEST ON LCA FUEL SYSTEM LRU’s

Thennavarajan, S and Ramamurthy, S and Janaki Rami Reddy, M and Pandian, K PRESSURE DROP TEST ON LCA FUEL SYSTEM LRU’s. Project Report. NAL, NAL.

[img] Microsoft Word (PROJECT DOCUMENT)
BACK_COVER_PAGE.docx - Published Version
Restricted to Registered users only
Download (20kB) | Request a copy
[img] PDF
BACK_COVER_PAGE.pdf
Restricted to Registered users only
Download (42kB) | Request a copy

Abstract

Abstract This report deals with the testing of LRU’s used in fuel system for LCA/TEJAS aircraft. The test facility was made to test the LRU’s. The instrumentation and data acquisition software were incorporated in the test rig. The venting characteristics of the LRU’s were experimentally evaluated for various LRU’s pressures. It was observed that the mass flow increases with increase in pressure loss across the valves.

Item Type: Monograph (Project Report)
Subjects: PHYSICS
Depositing User: Mr THENNAVARAJAN SUBRAMANIAN
Date Deposited: 27 Apr 2011 06:26
Last Modified: 13 Aug 2015 07:33
URI: http://nal-ir.nal.res.in/id/eprint/9174

Actions (login required)

View Item View Item
nalir is powered by EPrints 3 which is developed by the School of Electronics and Computer Science at the University of Southampton. More information and software credits.