Systematic, two dimensional tests on an NACA 23015 airfoil section with a plain flap and circulation control by suction through a cuspedslot entry (Aerodynamic report)
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Book Details
Author(s)
James L Stalter
ISBN / ASIN
B0007GS07M
ISBN-13
978B0007GS070
Marketplace
United Kingdom 🇬🇧
