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

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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