Compressibility effects investigated from pressure distributions obtained at various airfoil angles of attack and aileron angles for Mach numbers from 0.25 to approximately 0.76; wind tunnel data indicated reduction in stick force and improvement in stick force characteristics at high diving speeds.
Effect of compressibility on section characteristics of airfoil with round-nose slotted Frise Aileron
Nat Advisory Committee Aeronautics -- Tech Note
1946
17 pages
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English
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Effect of compressibility on pressure distribution over airfoil with slotted frise aileron
Engineering Index Backfile | 1944
|TIBKAT | 1952
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