PRESSURE DROP TEST ON LCA FUEL SYSTEM LRU’s

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.

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      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: Proj.Doc/Technical Report (Project Report)
      Subjects: PHYSICS
      Division/Department: Propulsion Division, Propulsion Division, Propulsion Division, Propulsion Division
      Depositing User: THENNAVARAJAN S SUBRAMANIAN
      Date Deposited: 27 Apr 2011 11:56
      Last Modified: 27 Apr 2011 11:56
      URI: http://nal-ir.nal.res.in/id/eprint/9174

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