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- W2915371632 abstract "Wind tunnel tests were conducted to determine the low speed, two dimensional aerodynamic characteristics of a 13percent thick medium speed airfoil designed for general aviation applications. The results were compared with data for the 13 percent thick low speed airfoil. The tests were conducted over a Mach number range from 0.10 to 0.32, a chord Reynolds number range from 2.0 x 10 to the 6th power to 12.0 x 10 to the 6th power, and an angle of attack frange from about -8 deg to 10 deg. The objective of retaining good high-lift low speed characteristics for an airfoil designed to have good medium speed cruise performance was achieved." @default.
- W2915371632 created "2019-03-02" @default.
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- W2915371632 date "1979-08-01" @default.
- W2915371632 modified "2023-09-27" @default.
- W2915371632 title "Low-speed aerodynamic characteristics of a 13 percent thick medium speed airfoil designed for general aviation applications" @default.
- W2915371632 hasPublicationYear "1979" @default.
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