Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180° /

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Bibliographic Details
Author / Creator:Critzos, Chris C., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1955.
Description:1 online resource (21 pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 3361
Technical note (United States. National Advisory Committee for Aeronautics) ; 3361.
Subject:Aerofoils.
Angle of attack (Aerodynamics)
Lift (Aerodynamics)
Aerofoils.
Angle of attack (Aerodynamics)
Lift (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12381207
Hidden Bibliographic Details
Varying Form of Title:Aerodynamic characteristics of National Advisory Committee for Aeronautics 0012 airfoil section at angles of attack from 0 degrees to 180 degrees
Other authors / contributors:Heyson, Harry H., author.
Boswinkle, Robert W., author.
United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"January 1955."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (pages 11-12).
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 7, 2020).
Other form:Paper version: Critzos, Chris C., Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 to 180 degrees
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/3361
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