Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance /
Saved in:
Author / Creator: | Bamber, Millard J., author. |
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Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1934. |
Description: | 1 online resource (8 pages, 3 unnumbered pages) : illustrations. |
Language: | English |
Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 493 Technical note (United States. National Advisory Committee for Aeronautics) ; 493. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12321605 |
Other authors / contributors: | United States. National Advisory Committee for Aeronautics, issuing body. |
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Notes: | "March 1934" No Federal Depository Library Program (FDLP) item number Includes bibliographical references (page 8) Description based on online resource, PDF version; title from title page (TRAIL, viewed June 12, 2020) |
Other form: | Print version: Bamber, Millard J., Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance |
GPO item no.: | 9999 (online) |
Govt.docs classification: | Y 3.N 21/5:6/493 |
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