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- W288264029 abstract "The data obtained on the NACA M-12 airfoil, tested at twenty atmosphere density in the NACA variable density wind tunnel, have been extended by additional tests at one and at twenty atmospheres under improved conditions. The results of these tests are given. Considerable scale effect was found." @default.
- W288264029 created "2016-06-24" @default.
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- W288264029 date "1926-08-01" @default.
- W288264029 modified "2023-09-27" @default.
- W288264029 title "The characteristics of the NACA M-12 airfoil section" @default.
- W288264029 hasPublicationYear "1926" @default.
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