The effect of longitudinal moment of inertia upon dynamic stability /
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Author / Creator: | Norton, F. H. (Frederick Harwood), 1896-1992, author. |
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Imprint: | [Washington, D.C.] : National Advisory Committee for Aeronautics, 1922. |
Description: | 1 online resource (3 pages, 1 unnumbered page) : illustration. |
Language: | English |
Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 115 Technical note (United States. National Advisory Committee for Aeronautics) ; 115. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12092491 |
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100 | 1 | |a Norton, F. H. |q (Frederick Harwood), |d 1896-1992, |e author. |0 http://id.loc.gov/authorities/names/n84804590 |1 http://viaf.org/viaf/33415817 | |
245 | 1 | 4 | |a The effect of longitudinal moment of inertia upon dynamic stability / |c by F.H. Norton and T. Carroll. |
264 | 1 | |a [Washington, D.C.] : |b National Advisory Committee for Aeronautics, |c 1922. | |
300 | |a 1 online resource (3 pages, 1 unnumbered page) : |b illustration. | ||
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. 115 | |
588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed March 25, 2020). | ||
500 | |a "October, 1922." | ||
500 | |a No Federal Depository Library Program (FDLP) item number. | ||
504 | |a Includes bibliographical reference (page 1). | ||
650 | 0 | |a Stability of airplanes. |0 http://id.loc.gov/authorities/subjects/sh85127186 | |
650 | 0 | |a Stability of airplanes, Longitudinal. |0 http://id.loc.gov/authorities/subjects/sh85127188 | |
650 | 0 | |a Moments of inertia. |0 http://id.loc.gov/authorities/subjects/sh85086657 | |
650 | 7 | |a Moments of inertia. |2 fast |0 (OCoLC)fst01025015 | |
650 | 7 | |a Stability of airplanes. |2 fast |0 (OCoLC)fst01131210 | |
650 | 7 | |a Stability of airplanes, Longitudinal. |2 fast |0 (OCoLC)fst01131217 | |
700 | 1 | |a Carroll, Thomas, |e author. |0 http://id.loc.gov/authorities/names/n2015035611 |1 http://viaf.org/viaf/195120086 | |
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 Norton, F. H. |t Effect of longitudinal moment of inertia upon dynamic stability |w (OCoLC)639555648 |
830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 115. | |
856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo134194 |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/gpo134194 |z Government Publishing Office |g ebooks |i 11652268 |