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- W47364043 abstract "A 12% thick NLF airfoil is designed for an unmanned aircraft for reconnaissance and target acguision role. This airfoil is compared with NACA 64/, -612 airfoil of same thickness. NAL airfoil, designated as NAL-NLF-1 2Qr has given better performance than NACA airfoil at the design conditions. For that matter in the entire range 0.4lt;CLlt; 0.8 NAL airfoil performs better than the NACA airfoil." @default.
- W47364043 created "2016-06-24" @default.
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- W47364043 date "1990-03-01" @default.
- W47364043 modified "2023-09-24" @default.
- W47364043 title "Design of a natural laminar flow airfoil for an unmanned aircraft" @default.
- W47364043 hasPublicationYear "1990" @default.
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