The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals /
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Author / Creator: | Munk, Max M. (Max Michael), 1890- author. |
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Imprint: | [Washington, D.C.] : National Advisory Committee for Aeronautics, 1923. |
Description: | 1 online resource (9 pages, 2 unnumbered pages) : illustrations. |
Language: | English |
Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 122 Technical note (United States. National Advisory Committee for Aeronautics) ; 122. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12285007 |
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100 | 1 | |a Munk, Max M. |q (Max Michael), |d 1890- |e author. |0 http://id.loc.gov/authorities/names/no2008043810 |1 http://viaf.org/viaf/47157480 | |
245 | 1 | 4 | |a The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals / |c by Max M. Munk. |
264 | 1 | |a [Washington, D.C.] : |b National Advisory Committee for Aeronautics, |c 1923. | |
300 | |a 1 online resource (9 pages, 2 unnumbered pages) : |b illustrations. | ||
336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
337 | |a computer |b c |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/c | ||
338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
490 | 1 | |a Technical notes / National Advisory Committee for Aeronautics ; |v No. 122 | |
588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed March 26, 2020). | ||
500 | |a "January, 1923." | ||
500 | |a No Federal Depository Library Program (FDLP) item number. | ||
504 | |a Includes bibliographical references (page 1). | ||
650 | 0 | |a Lift (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85076855 | |
650 | 0 | |a Angle of attack (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh95010977 | |
650 | 0 | |a Aerofoils. |0 http://id.loc.gov/authorities/subjects/sh85001301 | |
650 | 0 | |a Camber (Aerofoils) |0 http://id.loc.gov/authorities/subjects/sh85019077 | |
650 | 7 | |a Aerofoils. |2 fast |0 (OCoLC)fst00798241 | |
650 | 7 | |a Angle of attack (Aerodynamics) |2 fast |0 (OCoLC)fst00808866 | |
650 | 7 | |a Camber (Aerofoils) |2 fast |0 (OCoLC)fst00844649 | |
650 | 7 | |a Lift (Aerodynamics) |2 fast |0 (OCoLC)fst00998431 | |
710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://viaf.org/viaf/136563305 | |
776 | 0 | 8 | |i Print version: |a Munk, Max M. |t Determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals |w (OCoLC)639573931 |
830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 122. | |
856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo134268 |y Government Publishing Office |
903 | |a HeVa | ||
929 | |a eresource | ||
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928 | |t Library of Congress classification |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/gpo134268 |z Government Publishing Office |g ebooks |i 11846177 |