Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps / James C. Sivells, and Stanley H. Spooner.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Sivells, James C.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Spooner, Stanley H.
Other title:	Technical report archive and image library.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1579.
Subjects:	Aerofoils. Flaps (Airplanes) Lift (Aerodynamics) Wind tunnel testing.

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Call Number:	Y 3.N 21/5:6/1579
Y 3.N 21/5:6/1579	Available Place a Hold