Computational Analysis of Fighter Aircraft Wing under Mach...

Computational Analysis of Fighter Aircraft Wing under Mach Number 0.7 for Small Sweep Angles

Srinivas, G., Potti, Srinivasa Rao
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Volume:
592-594
Language:
english
Journal:
Applied Mechanics and Materials
DOI:
10.4028/www.scientific.net/amm.592-594.1020
Date:
July, 2014
File:
PDF, 498 KB
english, 2014
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