Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 /
Saved in:
Author / Creator: | Turner, M. J., author. |
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Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1950. |
Description: | 1 online resource (46 pages) : illustrations. |
Language: | English |
Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 2213 Technical note (United States. National Advisory Committee for Aeronautics) ; 2213. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12678724 |
Other authors / contributors: | Rabinowitz, S., author. United States. National Advisory Committee for Aeronautics, issuing body. |
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Notes: | "October 1950" No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (page 19). Description based on online resource, PDF version; title from title page (TRAIL, viewed July 16, 2020). |
Other form: | Print version: Turner, M. J., Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 |
GPO item no.: | 9999 (online) |
Govt.docs classification: | Y 3.N 21/5:6/2213 |
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