Tests in variable℗-density wind tunnel of N. A. C. A. 23012 airfoil with plain and split flaps.

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Bibliographic Details
Online Access:	Full Text (via ProQuest)
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1938.
Subjects:	Aeronautics > Research. Airplanes. Wind. Weights and measures.

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Full Text (via ProQuest)

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Call Number:	Y3.N21_5..5_661
Y3.N21_5..5_661	Available