Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section /
Saved in:
Author / Creator: | Smith, Hamilton A., author. |
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Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1950. |
Description: | 1 online resource (18 pages) : illustrations. |
Language: | English |
Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 2074 Technical note (United States. National Advisory Committee for Aeronautics) ; 2074. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12346599 |
Varying Form of Title: | Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the National Advisory Committee for Aeronautics 0012 airfoil section |
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Other authors / contributors: | Schaefer, Raymond F., author. United States. National Advisory Committee for Aeronautics, issuing body. |
Notes: | "April 1950." No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (page 9). Description based on online resource, PDF version; title from title page (TRAIL, viewed July 15, 2020). |
Other form: | Paper version: Smith, Hamilton A., Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section |
GPO item no.: | 9999 (online) |
Govt.docs classification: | Y 3.N 21/5:6/2074 |
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