The effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings /
Saved in:
Author / Creator: | Weick, Fred E., author. |
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Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933. |
Description: | 1 online resource (15 pages, 9 unnumbered pages) : illustrations. |
Language: | English |
Series: | Technical note / National Advisory Committee for Aeronautics ; No. 447 Technical note (United States. National Advisory Committee for Aeronautics) ; 447. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12695168 |
Other authors / contributors: | Scudder, Nathan F., author. United States. National Advisory Committee for Aeronautics, issuing body. |
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Notes: | "February, 1933." "Part I - Wind-tunnel tests showing effect on lift, drag, and autorotation, by Fred E. Weick"--Pages 3-6. "Part II - Flight tests showing effect on the spin and performance of the XN2Y-1 airplane, by Nathan F. Scudder"--Pages 6-11. No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (page 12). Description based on online resource, PDF version; title from title page (TRAIL, viewed January 11, 2021). |
Other form: | Print version: Weick, Fred E. Effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings |
GPO item no.: | 9999 (online) |
Govt.docs classification: | Y 3.N 21/5:6/447 |
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