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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)

Author James L Stalter
Publisher University of Wichita, School of Engineering
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Book Details
ISBN / ASINB0007GS07M
ISBN-13978B0007GS070
MarketplaceIndia 🇮🇳