Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180° /
Saved in:
Author / Creator: | Critzos, Chris C., author. |
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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 |
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 |
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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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