Increase of only 20kg..? What exactly they are referring to here..? Increase in existing fuel tanks only..?Kartik wrote:LCA AF Mk2 variant - the most details that we've got so far, from ADA's 31st Annual Report for 2015-2016. Next year's report will reveal what has transpired with relation to the LCA AF Mk2 variant in 2017.
LCA AF Mk2
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The changes in NMG have resulted in drag reduction and increase in fuel content by about 20kg. These improvements are going to result in improved point and mission performance.
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Aerodynamics : A number of aerodynamics improvements have been carried out to reduce drag and improve performance:
• Drag reduction studies have been completed. Canopy reshaping, outer cowl modification, actuator fairing extension and supersonic pylons have resulted in approx 20 counts (8%) drag reduction in supersonic regimes.
• Wind Tunnel studies have been completed.
• Aero loads computations have been completed.
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Also, data point for LCA drag - 20 counts reduction ~ 8% >> baseline drag must be ~250 counts. But its not clear whether they are talking about only supersonic wave drag or total drag. I suppose its the former.
Another figure was mentioned in the Canopy optimization paper from one of the conferences.
http://www.nal.res.in/CFDsympo17/cfdful ... rcraft.pdf
50kg fuel increase and 12 count reduction (~6%) in supersonic wave drag due to canopy reshaping. Which means other 8 counts is due to other factors mentioned above. The 12 counts reduction had increased transonic acceleration by 20%, so total of 20 counts would increase it even further, may be by >30%.