Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds /

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Bibliographic Details
Author / Creator:	Daley, Bernard N., author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1955.
Description:	1 online resource (57 pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 3424 Technical note (United States. National Advisory Committee for Aeronautics) ; 3424.
Subject:	Aerofoils -- Testing. Angle of attack (Aerodynamics) Aerofoils -- Testing. Angle of attack (Aerodynamics)
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12381208

Hidden Bibliographic Details
Varying Form of Title:	Aerodynamic characteristics of several six-percent-thick airfoils at angles of attack from zero degrees to twenty degrees at high subsonic speeds
Other authors / contributors:	Lord, Douglas T., author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"May 1955." "Supersedes recently declassified NACA RM L9E19. 1949"--Page 1. No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (page 10). Description based on online resource, PDF version; title from title page (TRAIL, viewed August 11, 2020).
Other form:	Paper version: Daley, Bernard N., Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/3424

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