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PRESSURE DROP TEST ON LCA FUEL SYSTEM LRU’s

IR@NAL: CSIR-National Aerospace Laboratories, Bangalore

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Title PRESSURE DROP TEST ON LCA FUEL SYSTEM LRU’s
 
Creator Thennavarajan, S
Ramamurthy, S
Janaki Rami Reddy, S
Pandian, K
 
Subject PHYSICS
 
Description 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.
 
Publisher NAL
 
Type Proj.Doc/Technical Report
NonPeerReviewed
 
Format application/msword
application/pdf
 
Identifier http://nal-ir.nal.res.in/9174/1/BACK_COVER_PAGE.docx
http://nal-ir.nal.res.in/9174/2/BACK_COVER_PAGE.pdf
Thennavarajan, S and Ramamurthy, S and Janaki Rami Reddy, S and Pandian, K PRESSURE DROP TEST ON LCA FUEL SYSTEM LRU’s. Project Report. NAL, NAL.
 
Relation http://nal-ir.nal.res.in/9174/