recent trends in fluid mechanics (vol1, issue1)
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Recent Trends in Fluid Mechanics
(RTFM)
Jan - April 2014
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Recent Trends in Fluid Mechanics
Recent Trends in Fluid Mechanics
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I take the privilege to present the print version for the Volume 1 Issue (1) of Recent Trends in Fluid
Mechanics. The intension of RTFM is to create an atmosphere that stimulates creativeness, research
and growth in the area of fluid mechanics and applications.
The development and growth of the mankind is the consequence of brilliant Research done by
eminent Scientists and Engineers in every field. RTFM provides an outlet for research findings and
reviews in areas of fluid mechanics technology found to be relevant for national and international
recent developments & research initiative.
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research in the domain of fluid mechanics research.
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I hope you will enjoy reading this issue and we welcome your feedback on any aspect of the Journal.
Dr. Archana Mehrotra
Director
STM Journals
Director's Desk
STM JOURNALS
1. Analysis of Flow through Main Engine Control Unit (MECU) of a New Aircraft Fuel Control System under Various Aircraft Acceleration Arun Kumar Sc 'E', Kamesh Goyal Sc 'G', Pradyumna Ghosh, Ankit Gopal Pandey 1
ContentsRecent Trends in Fluid Mechanics
RTFM (2014) © STM Journals 2014. All Rights Reserved
Recent Trends in Fluid Mechanics
Volume 1, Issue 1
www.stmjournals.com
Analysis of Flow through Main Engine Control Unit
(MECU) of a New Aircraft Fuel Control System under
Various Aircraft Acceleration
Arun Kumar Sc ‘E’1, Kamesh Goyal Sc ‘G’
1, Pradyumna Ghosh
2*, Ankit Gopal Pandey2
1Regional Centre for Military Airworthiness, CEMILAC, HAL P. O. Lucknow, UP, India
2Department of Mechanical Engineering, Indian Institute of Technology (BHU), Varanasi, UP, India
Abstract A fuel control system is being designed and developed for a new aero engine of a fighter
aircraft. But existing facility doesn’t support the full operational testing of the individual
components of aircraft fuel control system under various aircraft acceleration conditions. In this paper theoretical analysis has been done to check the flow distribution of one of the basic
systems, i.e., Main Engine Control Unit (MECU) under various aircraft accelerations. It has
been observed that, in normal mode upon application of vertical orientated acceleration, for the flow rate of 1572 gph from the pump, a maximum variation of 0.17% in the
combustion chamber flow rate has been observed. For this case a maximum variation of 3.3% in pressure (at Upstream MPV) was also observed. These variations are within permissible
limit of variations that can be sustained by MECU circuit. In case of manual mode there
is a large offset between experimental and simulation results (as large as 10 percent) but effect of possible ‘g’ effect is within 2 percent of the base results. Moreover, effect of
sustained acceleration effect of ‘5 g’ for 5 min has also been analyzed and both the configuration and performance parameters are almost the same as the regular aircraft
acceleration. It has also been analyzed that Emergency Spill Valve (ESV) and Pump Pressure
Relief Valve (PPRV) which are spring loaded will not be falsely activated under operational ‘g’ effect.
Keywords: Aircraft acceleration, falsely activated, Main Engine control unit (MECU),
Sustained acceleration